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040
Friday, December 8th, 2017
Fortune Global Forum 2017
Guangzhou, China
8:00 AMâ9:20 AM
SMART MANUFACTURING AND THE INTERNET OF THINGS
Around the world, factory floors and assembly lines are becoming highly automated, combining human ingenuity with data and technology to revolutionize product and productivity outcomes. As the notion of a âfactory of the futureâ continues to evolve, how are companies incorporating âsmartâ and connected products into their manufacturing process? From sensors and robots to 3D printing and green technology, global companies are experimenting with a variety of methods to streamline, scale, and sustain their business. Here in China, manufacturers have been asked to deliver on the nationâs âMade in China 2025â strategy and are aggressively pursuing their own strategies to become smarter, greener, and more efficient. As these changes take hold, what are the implications for those doing business in China and for supply chains worldwide? And how are companies redeploying and reeducating their workforces as traditional factory jobs become automated and the need for technically proficient talent increases?
Hosted by The City of Guangzhou
Börje Ekholm, President and CEO, Ericsson Group
Till Reuter, Chief Executive Officer, KUKA
Tony Tan, Partner, Shanghai Office, McKinsey & Company
Wang Wenyin, Chairman, Amer International Group
Shoei Yamana, President and CEO, Konica Minolta
Zhang Jing, Founder and Chairman, Cedar Holdings Group
Moderator: Adam Lashinsky, Fortune
Photograph by Vivek Prakash/Fortune
Part of modding your car is making it look good, and looks weren't really a concern when the engineers were designing your ride. It's easy to see that when you open up the hood and it easily looks like a rat's nest. Password knows that looks on the outside don't mean squat if you can't show off what's under the hood. The Password:JDM dry carbon fiber fuse box over-cover for the 2013+ Subaru BRZ / Scion FR-S adheres to your stock fuse box cover and will help clean up the look of your engine bay making your engine stand out, while adding a much needed accent to the scene. Like all of our dry carbon fiber parts that we manufacture, this piece has been precision crafted for a perfect fit and requires no tools or modifications to install. We also use a fade-resistant resin during the manufacturing process which ensures that the part will look as fresh as it did and function as well as the day you bought it.
Note:The Password:JDM Dry Carbon Fiber Fuse Box Over Cover fits over the factory part and is adhered with double side tape.
Features include:
- Perfect dry carbon fitment with structural integrity
- high-heat, fade resistant resin fabrication process
- Extreme lightweight to strength ratio
- Made in the USA
- Badass looks for your BRZ or FR-S engine bay!
During the production of an Extrusion Die, several manufacturing processes are applied, from CAD to CAM from FEA to ERP. Due to the open interface structure, ExtrusionPower supports the achievement of a complete Product Life Cycle. Different applications can be integrated with ExtrusionPower.
Winter logging, 1920s
Wood manufacturing in Maryland began with hundreds of small sawmills that often used streams and water wheels to power they belt-driven machinery. Modern milling technology uses computers to scan logs and determine how best to maximize wood recovery and optimize grade and quality. Modern wood-producing mills make use of every part of a tree in a very efficient manufacturing process.
The Maryland Forest and Park services were founded in 1906. These photos were archived in celebration of their centennial in 2006.
EXHIBITION
100 Best Posters 14
GERMANY, AUSTRIA, SWITZERLAND
MI, MO 11/11/2015, 03/28/2016
MAK Art Print Hall
Already for the tenth time, the MAK in the exhibition 100 Best Posters 14. Germany Austria Switzerland shows the hundred most compelling design concepts in the probably hottest medium of visual everyday culture: the poster. The current winning projects of the popular graphic design competition are characterized by an enigmatic pictural humor, explosive colors as well as precise designs and demonstrate impressively that a poster can be more than just an banal advertising space. Many of the award-winning works furthermore also rely on a subtle play with typography. Innovative ideas can also be found in the manufacturing process: This year's competition shows that you can readily knit posters in high-tech process or use a thermo-insulating space blanket as carrier material for screen printing.
Hardly any medium is such clocked on the consumption and nevertheless sets trends at the cutting edge. "[...] The poster designer challenges himself repeatedly and enjoys himself at gained symbols." Says Götz Gramlich, President of the association 100 Best Posters eV, and he postulats. "A good poster unfolds in the mind of the beholder."
From over 1 800 submitted individual posters, composed of contract work, self-initiated posters/self-promotion as well as student project orders from Germany, Austria and Switzerland, awarded the international jury, consisting of Richard van der Laken (Amsterdam, Chairman), Christof Nardin (Wien), Jiri Oplatek (Basel), Nicolaus Ott (Berlin) and Ariane Spanier (Berlin), the 100 winning posters of the year 2014.
In the competition participated 575 submitters (men and women), of which 48 are from Austria, 128 from Switzerland and 399 from Germany. The leader among the winning 100 best is Switzerland with 51 winning projects, followed by 44 German and 5 Austrian contributions.
The by sensomatic design (Christine Zmölnig and Florian Koch, Vienna) designed catalog offers in addition to the illustrations of all the winning posters and the contacts with the designers also this year a captivating essay by Thomas Friedrich: On the dialectics of image and text in the poster today. In a concise way, he looks at the contextuality of posters and explains the theme facetiously and pictorially based on a poster for a bullfight. Read more in the catalog!
For the corporate design of this year's competition and the new Web Visuals also sensomatic design, Vienna, is responsible. Since June 2014, the new online archive on the homepage of the 100 Best Posters Registered Association offers a comprehensive overview of all award-winning works from the years 2001-2014.
The exhibition takes place in cooperation with 100 Best Posters e. V.
100-beste-plakate.de
Curator Peter Klinger, Deputy Head of the MAK Library and Works on Paper Collection
AUSSTELLUNG
100 Beste Plakate 14
DEUTSCHLAND ÖSTERREICH SCHWEIZ
MI, 11.11.2015–MO, 28.03.2016
MAK-KUNSTBLÄTTERSAAL
Bereits zum zehnten Mal zeigt das MAK in der Ausstellung 100 BESTE PLAKATE 14. Deutschland Österreich Schweiz die einhundert überzeugendsten Gestaltungskonzepte im wohl heißesten Medium der visuellen Alltagskultur: dem Plakat. Die aktuellen Siegerprojekte des beliebten Grafikdesignwettbewerbs bestechen mit hintergründigem Bildwitz, explosiver Farbgebung sowie exakten Ausführungen und demonstrieren eindrücklich, dass ein Plakat mehr als nur banale Werbefläche sein kann. Viele der prämierten Arbeiten setzen außerdem auf ein subtiles Spiel mit Typografie. Innovative Ideen finden sich auch im Herstellungsprozess: Der diesjährige Wettbewerb zeigt, dass man Plakate ohne Weiteres im Hightech-Verfahren stricken oder eine thermo-isolierende Rettungsdecke als Trägermaterial für einen Siebdruck verwenden kann.
Kaum ein Medium ist derart auf den Verbrauch hin getaktet und setzt dennoch Trends am Puls der Zeit. „[…] der Plakatgestalter fordert sich immer wieder selbst heraus und erfreut sich an gewonnenen Sinnbildern.“ so Götz Gramlich, Präsident des Vereins 100 Beste Plakate e. V., und er postuliert: „Ein gutes Plakat entfaltet sich im Kopf des Betrachters.“
Aus über 1 800 eingereichten Einzelplakaten, zusammengesetzt aus Auftragsarbeiten, selbst initiierten Plakaten/Eigenwerbungen sowie studentischen Projektaufträgen aus Deutschland, Österreich und der Schweiz, prämierte die international besetzte Fachjury, bestehend aus Richard van der Laken (Amsterdam, Vorsitz), Christof Nardin (Wien), Jiri Oplatek (Basel), Nicolaus Ott (Berlin) und Ariane Spanier (Berlin), die 100 Siegerplakate des Jahres 2014.
Am Wettbewerb hatten sich 575 EinreicherInnen beteiligt, davon 48 aus Österreich, 128 aus der Schweiz und 399 aus Deutschland. Spitzenreiter unter den prämierten 100 Besten ist die Schweiz mit 51 Siegerprojekten, gefolgt von 44 deutschen und 5 österreichischen Beiträgen.
Der von sensomatic design (Christine Zmölnig und Florian Koch, Wien) gestaltete Katalog bietet neben den Abbildungen aller Siegerplakate und den Kontakten zu den GestalterInnen auch dieses Jahr einen bestechenden Aufsatz von Thomas Friedrich: Zur Dialektik von Bild und Text im Plakat heute. In pointierter Form geht er auf die Kontextualität von Plakaten ein und erklärt das Thema witzig und bildhaft anhand eines Plakats für einen Stierkampf. Mehr dazu im Katalog!
Für das Corporate Design des diesjährigen Wettbewerbs und die neuen Web-Visuals zeichnet ebenfalls sensomatic design, Wien, verantwortlich. Seit Juni 2014 bietet das neue Online-Archiv auf der Homepage der 100 Beste Plakate e. V. einen umfassenden Überblick aller prämierten Arbeiten aus den Jahren 2001 bis 2014.
Die Ausstellung findet in Kooperation mit 100 Beste Plakate e. V. statt.
100-beste-plakate.de
Kurator: Peter Klinger, Stellvertretende Leitung MAK-Bibliothek und Kunstblättersammlung
A quality manufacturing process uses ultraviolet resistant polycarbonate lenses and a high diode count. This results in stop, trim, turn and tail lamps that make vehicles easier to see. TRP LED lighting products will not fade or change color over time.
SeaDek is a revolutionary product utilized not only by the top boat builders in the marine industry, but also in the aftermarket by boat owners seeking custom products. Made from closed cell PE/EVA foam, SeaDek products offer safe and comfortable alternatives to marine traction products currently on the market. Easy to install and customizable, SeaDek replaces the need for molded in non skid, saving OEMs time and money during the manufacturing process.
SeaDek can be tailored to fit endless applications on nearly any type of boat. Some of the other benefits SeaDek offers include:
Exceptional traction, even when wet
Unparalleled comfort when standing, walking, or leaning on boat surfaces
Shock absorption, which decreases fatigue
Protection for boat surfaces against scratches, chips, and dents
Noise reduction characteristics - ideal for fishermen
If you have a boat, you have a place for SeaDek!
Learn more at www.seadek.com/
Want custom SeaDek for your boat? Find a Certified Fabricator or Installer near you! www.seadek.com/seadek-certified
Part of modding your car is making it look good, and looks weren't really a concern when the engineers were designing your ride. It's easy to see that when you open up the hood and it easily looks like a rat's nest. Password knows that looks on the outside don't mean squat if you can't show off what's under the hood. The Password:JDM dry carbon fiber fuse box over-cover for the 2013+ Subaru BRZ / Scion FR-S adheres to your stock fuse box cover and will help clean up the look of your engine bay making your engine stand out, while adding a much needed accent to the scene. Like all of our dry carbon fiber parts that we manufacture, this piece has been precision crafted for a perfect fit and requires no tools or modifications to install. We also use a fade-resistant resin during the manufacturing process which ensures that the part will look as fresh as it did and function as well as the day you bought it.
Note:The Password:JDM Dry Carbon Fiber Fuse Box Over Cover fits over the factory part and is adhered with double side tape.
Features include:
- Perfect dry carbon fitment with structural integrity
- high-heat, fade resistant resin fabrication process
- Extreme lightweight to strength ratio
- Made in the USA
- Badass looks for your BRZ or FR-S engine bay!
Old model watches in the museum at Prim.
On September 26, 2008 my family and I were privileged to spend the day in the beautiful town of Nové Mesto nad Metují in the east of the Czech Republic, close to the Polish border. Our host was Mr. Jan Prokop, Marketing Director (and principal designer) at the ELTON hodinárská, a.s. - the manufacturers of fine bespoke Prim wristwatches.
Mr. Prokop collected us from our hotel in Prague, drove us to Nové Mesto nad Metují and back (a round trip of three hours), presented their current product range, guided us through their interesting museum, and led us on a tour of the full manufacturing operation at Prim. This was a fantastic opportunity, and we got to see everything from the manufacturing of cases, dials, hesatite crystals and hands through to the final assembly process. We also saw great examples of their bespoke manufacturing capability as well as their top class restoration service. Mr Prokop ended a fine day with a meal and good local beer in a restaurant on the old town square.
Six weeks after our visit I sent my prized Prim Sport "Igen" 38 (produced in the 60's and early-70's) to ELTON where it is currently being restored and modernised to my specification, as well as being personalised. I can't wait to get it back - my first bespoke wristwatch and an heirloom to pass on to my son!
Although obviously sensitive about certain parts of their operation, Mr. Prokop graciously allowed me to take many photographs during our visit, and here they are for your viewing pleasure. As you will see, these are truly hand-made watches that combine both leading edge design and manufacturing processes and age-old processes and technologies. It is this progressive traditionalism and craftsmanship that gives these unique timepieces their individual character...and I love them!
This silver steampunk butterfly necklace is created with a vintage recycled pocket watch movement and a jeweled neo Victorian pewter butterfly. The steampunk butterfly is adorned with iridescent Austrian crystals. A large gold watch gear glistens above the butterfly. The vintage pocket watch pendant from the 1920s has a speckled guilloche that creates a metallic holographic effect. A guilloche is the design that is engraved on many vintage and antique watches during the manufacturing process. The necklace is completed with silver tone chunky chain.
From raw forging to lathe turn to milled face to powder coating and beyond, StreetLegalTV.com walks you through the entire manufacturing process of a Forgeline one piece forged monoblock wheel. If you've been thinking about investing in the most advanced wheel available, then take a few minutes this weekend and get the scoop at: www.streetlegaltv.com/tech-stories/wheels-tires/faster-li...
#Forgeline #forged #monoblock #notjustanotherprettywheel #madeinUSA
(En) Founded in 1906, the Coking Plant of Anderlues was specialized in the production of coke for industrial use.
Coke was obtained by distillation of coal in furnaces and, thanks to its superior fuel coal properties, it was used afterwards to feed the blast furnaces in the steel manufacturing process.
Closed and abandoned since 2002, the site has since undergone many losses and damages, not including an important pollution. While some buildings have now been demolished, there are however still some important parts of the former coking plant.
Among them, the former coal tower, next to the imposing "battery" of 38 furnaces, where the coke was produced. Besides them, we still can see the administrative buildings, the power station with its cooling tower, and buildings for the by-products, which were obtained by recovering the tar and coal gas. There are also a gasometer north side, the coal tip east side and a settling basin south side.
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(Fr) Fondées en 1906, les Cokeries d'Anderlues étaient spécialisées dans la fabrication de coke à usage industriel.
Le coke était obtenu par distillation de la houille dans des fours et, grâce à ses propriétés combustibles supérieures au charbon, il servait par après à alimenter les hauts-fourneaux dans le processus de fabrication de l'acier.
Fermé et laissé à l'abandon depuis 2002, le site a depuis lors subi de nombreuses pertes et dégradations, sans compter la pollution qui y règne. Si certains bâtiments (comme l'ancien lavoir à charbon) ont aujourd'hui été démolis, on retrouve encore toutefois certaines parties importantes de cette ancienne cokerie.
Parmi celles-ci, l'ancienne tour à charbon suivie de près par l'imposante "batterie" de 38 fours, où était produit le coke. A côté d'eux, on découvre également les bâtiments administratifs, la centrale électrique avec sa tour de refroidissement, ainsi que les bâtiments des sous-produits, lesquels étaient obtenus par récupération du goudron et du gaz de houille. Et en périphérie, on retrouve un gazomètre côté nord, le terril à l'est et un bassin de décantation côté sud.
iPlay V1
Our design had to be cheap to manufacture, with minimal manufacture processes and a low overall cost. Keeping this in mind I sketched my basic idea and then rendered it. After exporting the DXF files I lasercut them and had my first prototype.
There is an everlasting debate amongst gamers as to which console and controller is the best. I found that the PS3 controller was the most popular second being Xbox 360. The PS3 controller is symettrical unlike the Xbox controller and is so ergonomoic you can often forget you are holding it.
I illustrated the PS3 controller outline to kickstart the CAD process. My design consists of 3 layers of 5mm acrylic creating an iphone cavity depth of 10mm (iPhone 4 has a thickness of 9.3mm) and an overall thickness of 15mm. The structure would be held together with tight fit acrylic rods. I need to carry out test pieces on 2.99+-0.1mm radii to decide what are the best dimensions to use for these slots bearing in mind the lasercutter burns away material.
The whole in the bottom layer is so the device can be pushed out from the case after use.
V2
I asked some students to test the V1 prototype. They liked the product especially its simplicity. There were points that I could develop and improve.
Not all iPhone games auto orientate, hence it was essential I adapted my design so the phone could be rotated 180 degress. This would be easy by simply duplicating the button slots.
In addition to this there was no camera hole. If I were to introduce a camera holeto the design it would have to be duplicated 180 degrees to ensure photos could be taken no matter what orientation the iPhone was.
Taking this on board I designed and manufactured iPlay V2. Although acrylic rod would create a tight fit, 4 drops of dichloromethane would chemically weld the components together for a long lasting permanent fit. After this I used a buffing wheel to create round edges making the product more ergonomic to hold.
V3
Once again I asked some students for feedback on my prototype. They were impressed with how I addressed the previous issues. The only negative point raised was that it would not fit in your pocket. This was the next challenge I faced.
I considered hinging the lower two arms and making them lock into the back of the case. However this would make the design more complex and increase cost and manufacturing processes.
I moved the top pair of holes further up to better distribute the stress. I decided to split the product in half. My V3 model has alternating layers this creates cavities that allow it to be locked together together when not in use as photographed. This would easily fit in you pocket.
The problem the alternating layers created is a less ergonomic shape. Secondly there was nothing holding the two half together when placed on the phone.
In my V4 model I introduced a rubber band which kept the two half together when on the phone. It would also prevent one half form being lost. This created a new problem; the top half of the rubber band would not always line up as there was nothing guiding it. This was my next problem to solve.
V4
My final model would be made from acrylic but I was not going to buff it as that would add a manufacture process and would siginificanty increase the manufacture time. Since I was already using the laser cutter for cutting my components I thought I may aswell engrave some sort of graphics onto the top layer. I decided to remove the gaps in between the layers to make it better to hold and to remodel the rubberband tracks.
V5
I solved the problem of the inconvenient rubber band with two more locating rods on the top. These extra rods would keep the rubber band guided along the correct track. I made a MDF prototype to test my idea and it worked successfully even with coffee stirrers replicating the acrylic rod.
Satisfied with my idea I finally created an acrylic version. This required a bit more thought than previously as I had to accomodate for the thick rubber band. I decided to use 3mm acrylic instead of 5mm to create a thinner profile. This meant I needed a total of 5 layers to accomodate an iPhone 4.
Since I was already using a lasercutter and I wanted the product to appeal to gamers I decided to engrave some patterns. I was going to use a translucent coloured acrylic for the bottom layer and adjust the design so that it covers the camera and flash. This way the case will act as a camera filter and the flash/torch will produce coloured light.
Now that the product was split into halfs the individual components were so small that cutting a single iPlay V5 uses less than an A4 sized amount of 3mm acrylic (the 2D Design screenshot has an A3 page layout). This also meant that it would fit both an iPhone 4 & 5 as the rubber can stretch to accomodate for an iPhone 5. Apart from the height of the iPhone 5 the dimensions are very similair to those of the 4.
I am very pleased with the final product and getting through to the next stage with KFDS. If I were to develop the product further I would find a way to lock the two halves together when not on the phone. This could be done like a jigsaw puzzle or by manipulating the rods into a dowel joint.
Io Aircraft - www.ioaircraft.com
Drew Blair
www.linkedin.com/in/drew-b-25485312/
io aircraft, phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air-Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, hypersonic plane, hypersonic aircraft, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, defense science, missile defense agency, aerospike,
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
follow me @sunnyholt www.twitter.com/sunnyholt for more news and photographs.
July 2014
Swedish born, but London based, interior designer Staffan Tollgard has a spacious showroom for products/brands he has sourced from all over the world. He is so passionate about what he does, and has visited all his suppliers in person, to understand their ethos, history and manufacturing processes, and to bring back the very best to London. Find furniture/furnishings/art from the US, Scandinavia (naturally!), Holland, Germany, Canada, and Israel, for example.
The space, in a brand new Chelsea development, with the river just a stone's throw away, has huge windows, and a double-height ceiling, from which hang spectacular lightfittings. There's a gallery of chairs, sofas, side tables, rugs and much more, with a fully-furnished "apartment" in a secret inner sanctum. This is a - as yet - lesser know design destination which is well worth a journey if you love interior design. Take the chance to explore the surroundings, with a mesmerising water feature that fills the air with its noise of a rushing torrent, and then a series of locks that lead directly into the river itself.
Grosvenor Waterside, Gatliff Road, SW1
A change-making, industry-shaking fabric, Revolution is a breakthrough in textile circularity.
The first fabric to be produced using Camira’s advanced textile recycling capability, iinouiio, Revolution uses waste wool yarn from our own manufacturing processes to create a fabric that is truly closing the loop, and opening the door to a new, exciting era of sustainability.
Woollen mill, now council offices. 1818 for Stanley and Stephen Clissold, extended to north and clock tower added by G F Bodley for S S Marling in 1862; restored for Stroud District Council 1987-90. Squared limestone; Welsh slate roofs, hipped to 1862 block and gabled to 1818 block; stone lateral and end stacks to 1818 range; projecting from west elevation of 1862 range is large stack with moulded base to tapered octagonal shaft with moulded capping. L-plan with long 1818 block to south of 1862 block which has boiler house to west. 1818 block of 4 storeys and 18 x 3 bays: segmental-arched doorways and 2-light segmental-arched windows each with central mullion; continuous roof dormers with canted roofs, much restored. 1862 block of 5 storeys and 6 x 6 bays: articulated by shallow pilasters which frame flat-arched windows and semi-circular arched top-floor windows; all windows of cast-iron with small panes. Projecting stair/clock tower in south west angle between blocks has steeply pitched French Gothic roof with iron cresting and weathervane. Low one-storey boiler house projects to north-east. Interior: includes timber floors supported by timber girding beams with inserted cast-iron columns for additional support; brick arches to ground floor mark sites of original culverts to water wheels. 1862 range has stone stair and lift shaft to south west angle. The site was bought by the Clissolds in 1799: the traditonal internal timber construction of the mill contrasts with the advanced construction of nearby Stanley Mill (q;v) which was built in brick around a cast iron frame. The 1818 block was powered by 5 water wheels; steam power was installed by 1862 for SS Marling who acquired the mill with his brother in 1840. Bodley designed nearby Selsley Church for Marling, its French Gothic style matching the tower at the mill. Including Greenaway Buildings to west of Ebley Mills: The detached western buildings of Eblley Mill, which together with the mill comprise the rare and important survival of a functionally-integrated early C19 woollen mill complex. The western group consists of two multi-storeyed buildings attached to the east and west sides of the remains of a single-storeyed shed. All in Cotswold limestone, with two and three-light mullioned windows. Early to mid C19. The east building, on a north-south axis, is of two storeys and ten bays, probably dating in part from circa 1825 or earlier. Three light windows and gabled slate roof. A wagon entrance in the east elevation and a former taking-in door in the south end suggest the main function was warehousing. A later two-storey tranverse building in brick, now forming the west side of the site entrance, replaced the original north end. The larger five-storeyed west building is of ten bays, with three-light windows and a gabled slate roof. Probably added in the mid C19, replacing a smaller building in the same position. Its large size, fenestration and absence of taking-in doors suggests it originally accommodated manufacturing processes... EH Listing
At Sau Hoai's Rice Noodle Factory near Can Tho on the Mekong Delta, you can see every step of the noodle manufacturing process. These noodles are all hand-made, via a method that has not changed in decades - if not centuries! You can try making a batch yourself. This family-run business also includes an open-air restaurant where you can taste freshly-made noodles: they were outstanding!
100118-F-0782R-014 Kabul- A Kabul Milli factory employee sews a boot together during the boot manufacturing process in Kabul, Afghanistan, Jan. 18, 2010. Members of CSTC-A and the Afghan National Army visited the boot factory to observe the boot manufacturing process and to initiate a process improvement program..
(U.S. Air Force Photo/Staff Sgt. Larry E. Reid Jr., Released)
Io Aircraft - www.ioaircraft.com
Drew Blair
www.linkedin.com/in/drew-b-25485312/
io aircraft, phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air-Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, hypersonic plane, hypersonic aircraft, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, defense science, missile defense agency, aerospike,
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
Founded in 1993 by two 25 year old engineers, Matthieu GOBBI and Jerome GIACOMONI, AEROPHILE S.A. reinvented the tethered gas balloon following an 80 year absence.
AEROPHILE S.A. has since become the world leader in tethered gas balloons through the development of three flagship products: the AERO30NG Aerophile 5500 model (30 passengers) since 1994, 50 balloons sold over 20 countries, the AERO2 model Aerophile 380 (2 passengers) since 2000, 4 systems sold and the AEROPHARE (12 passengers) since 2007, 1 system sold. Additionally AEROPHILE S.A. manufactures various types of systems, inflatables and small tethered balloons. AEROPHILE S.A. received the grand prize for innovation in 2000 and devotes a large part of its resources to research and development for the continued improvement of existing balloons and the creation of new products. Aerophile S.A. is the holder of several patents.
The tethered balloon is a highly specialist aerostat requiring strict manufacturing processes and rigorous operating practices. Not only the manufacturer, AEROPHILE S.A. is also a successful operator of their balloons in Paris, since 1999, the PanoraMagique in Disney Village since 2005, the Great Park Balloon in Irvine (California) since 2007 and in Evry2 (France) the first AEROPHARE in 2007.
AEROPHILE S.A.'s personnel comprises some thirty staff, including some fifteen pilots and technicians qualified to undertake installation, training and commissioning of all systems.
The Whitechapel Bell Foundry was famous for, well, casting church bells. However, it closed in 2017 after nearly 450 years of bell-making and 250 years at its Whitechapel site, with the final bell cast given to the Museum of London along with other artefacts used in the manufacturing process.
Io Aircraft - www.ioaircraft.com
Drew Blair
www.linkedin.com/in/drew-b-25485312/
io aircraft, phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air-Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, hypersonic plane, hypersonic aircraft, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, defense science, missile defense agency, aerospike,
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
040
Friday, December 8th, 2017
Fortune Global Forum 2017
Guangzhou, China
8:00 AMâ9:20 AM
SMART MANUFACTURING AND THE INTERNET OF THINGS
Around the world, factory floors and assembly lines are becoming highly automated, combining human ingenuity with data and technology to revolutionize product and productivity outcomes. As the notion of a âfactory of the futureâ continues to evolve, how are companies incorporating âsmartâ and connected products into their manufacturing process? From sensors and robots to 3D printing and green technology, global companies are experimenting with a variety of methods to streamline, scale, and sustain their business. Here in China, manufacturers have been asked to deliver on the nationâs âMade in China 2025â strategy and are aggressively pursuing their own strategies to become smarter, greener, and more efficient. As these changes take hold, what are the implications for those doing business in China and for supply chains worldwide? And how are companies redeploying and reeducating their workforces as traditional factory jobs become automated and the need for technically proficient talent increases?
Hosted by The City of Guangzhou
Börje Ekholm, President and CEO, Ericsson Group
Till Reuter, Chief Executive Officer, KUKA
Tony Tan, Partner, Shanghai Office, McKinsey & Company
Wang Wenyin, Chairman, Amer International Group
Shoei Yamana, President and CEO, Konica Minolta
Zhang Jing, Founder and Chairman, Cedar Holdings Group
Moderator: Adam Lashinsky, Fortune
Photograph by Vivek Prakash/Fortune
iPlay V1
Our design had to be cheap to manufacture, with minimal manufacture processes and a low overall cost. Keeping this in mind I sketched my basic idea and then rendered it. After exporting the DXF files I lasercut them and had my first prototype.
There is an everlasting debate amongst gamers as to which console and controller is the best. I found that the PS3 controller was the most popular second being Xbox 360. The PS3 controller is symettrical unlike the Xbox controller and is so ergonomoic you can often forget you are holding it.
I illustrated the PS3 controller outline to kickstart the CAD process. My design consists of 3 layers of 5mm acrylic creating an iphone cavity depth of 10mm (iPhone 4 has a thickness of 9.3mm) and an overall thickness of 15mm. The structure would be held together with tight fit acrylic rods. I need to carry out test pieces on 2.99+-0.1mm radii to decide what are the best dimensions to use for these slots bearing in mind the lasercutter burns away material.
The whole in the bottom layer is so the device can be pushed out from the case after use.
V2
I asked some students to test the V1 prototype. They liked the product especially its simplicity. There were points that I could develop and improve.
Not all iPhone games auto orientate, hence it was essential I adapted my design so the phone could be rotated 180 degress. This would be easy by simply duplicating the button slots.
In addition to this there was no camera hole. If I were to introduce a camera holeto the design it would have to be duplicated 180 degrees to ensure photos could be taken no matter what orientation the iPhone was.
Taking this on board I designed and manufactured iPlay V2. Although acrylic rod would create a tight fit, 4 drops of dichloromethane would chemically weld the components together for a long lasting permanent fit. After this I used a buffing wheel to create round edges making the product more ergonomic to hold.
V3
Once again I asked some students for feedback on my prototype. They were impressed with how I addressed the previous issues. The only negative point raised was that it would not fit in your pocket. This was the next challenge I faced.
I considered hinging the lower two arms and making them lock into the back of the case. However this would make the design more complex and increase cost and manufacturing processes.
I moved the top pair of holes further up to better distribute the stress. I decided to split the product in half. My V3 model has alternating layers this creates cavities that allow it to be locked together together when not in use as photographed. This would easily fit in you pocket.
The problem the alternating layers created is a less ergonomic shape. Secondly there was nothing holding the two half together when placed on the phone.
In my V4 model I introduced a rubber band which kept the two half together when on the phone. It would also prevent one half form being lost. This created a new problem; the top half of the rubber band would not always line up as there was nothing guiding it. This was my next problem to solve.
V4
My final model would be made from acrylic but I was not going to buff it as that would add a manufacture process and would siginificanty increase the manufacture time. Since I was already using the laser cutter for cutting my components I thought I may aswell engrave some sort of graphics onto the top layer. I decided to remove the gaps in between the layers to make it better to hold and to remodel the rubberband tracks.
V5
I solved the problem of the inconvenient rubber band with two more locating rods on the top. These extra rods would keep the rubber band guided along the correct track. I made a MDF prototype to test my idea and it worked successfully even with coffee stirrers replicating the acrylic rod.
Satisfied with my idea I finally created an acrylic version. This required a bit more thought than previously as I had to accomodate for the thick rubber band. I decided to use 3mm acrylic instead of 5mm to create a thinner profile. This meant I needed a total of 5 layers to accomodate an iPhone 4.
Since I was already using a lasercutter and I wanted the product to appeal to gamers I decided to engrave some patterns. I was going to use a translucent coloured acrylic for the bottom layer and adjust the design so that it covers the camera and flash. This way the case will act as a camera filter and the flash/torch will produce coloured light.
Now that the product was split into halfs the individual components were so small that cutting a single iPlay V5 uses less than an A4 sized amount of 3mm acrylic (the 2D Design screenshot has an A3 page layout). This also meant that it would fit both an iPhone 4 & 5 as the rubber can stretch to accomodate for an iPhone 5. Apart from the height of the iPhone 5 the dimensions are very similair to those of the 4.
I am very pleased with the final product and getting through to the next stage with KFDS. If I were to develop the product further I would find a way to lock the two halves together when not on the phone. This could be done like a jigsaw puzzle or by manipulating the rods into a dowel joint.
The existing Freeport Community Center & a historic Edward B. Mallett house has been joined by a spacious addition to provide new social services offices, thrift store, teen center, coffee bar & multi-funtion community room. Not only was there a goal to preserve history landmarks....but to obtain serious energy savings!
Hunter XCI Foil product is used in the construction of the renovation & addition of the Freeport Community Center.. XCI Foil is a high thermal, rigid building insulation composed of a closed cell polyiso foam core bonded on-line during the manufacturing process to an impermeable foil facing material. It is designed for use in commercial cavity wall applications to provide continuous insulation within the building envelope.
Hunter Xci polyiso products:
- Have the highest R-Value per inch of any insulation
- NFPA 285 TEST - Passed
- Energy Star approved
- Contribute toward LEED certification credits
- HCFC, CFC, zero ODP, and negligable GWP.
Construction by: Warren Construction
XCI Twitter: twitter.com/#!/HunterXCI
XCI Facebook: www.facebook.com/pages/Hunter-Xci-Exterior-Continuous-Ins...
View more: www.hunterxci.com/
040
Friday, December 8th, 2017
Fortune Global Forum 2017
Guangzhou, China
8:00 AMâ9:20 AM
SMART MANUFACTURING AND THE INTERNET OF THINGS
Around the world, factory floors and assembly lines are becoming highly automated, combining human ingenuity with data and technology to revolutionize product and productivity outcomes. As the notion of a âfactory of the futureâ continues to evolve, how are companies incorporating âsmartâ and connected products into their manufacturing process? From sensors and robots to 3D printing and green technology, global companies are experimenting with a variety of methods to streamline, scale, and sustain their business. Here in China, manufacturers have been asked to deliver on the nationâs âMade in China 2025â strategy and are aggressively pursuing their own strategies to become smarter, greener, and more efficient. As these changes take hold, what are the implications for those doing business in China and for supply chains worldwide? And how are companies redeploying and reeducating their workforces as traditional factory jobs become automated and the need for technically proficient talent increases?
Hosted by The City of Guangzhou
Börje Ekholm, President and CEO, Ericsson Group
Till Reuter, Chief Executive Officer, KUKA
Tony Tan, Partner, Shanghai Office, McKinsey & Company
Wang Wenyin, Chairman, Amer International Group
Shoei Yamana, President and CEO, Konica Minolta
Zhang Jing, Founder and Chairman, Cedar Holdings Group
Moderator: Adam Lashinsky, Fortune
Photograph by Vivek Prakash/Fortune
040
Friday, December 8th, 2017
Fortune Global Forum 2017
Guangzhou, China
8:00 AM–9:20 AM
SMART MANUFACTURING AND THE INTERNET OF THINGS
Around the world, factory floors and assembly lines are becoming highly automated, combining human ingenuity with data and technology to revolutionize product and productivity outcomes. As the notion of a “factory of the future” continues to evolve, how are companies incorporating “smart” and connected products into their manufacturing process? From sensors and robots to 3D printing and green technology, global companies are experimenting with a variety of methods to streamline, scale, and sustain their business. Here in China, manufacturers have been asked to deliver on the nation’s “Made in China 2025” strategy and are aggressively pursuing their own strategies to become smarter, greener, and more efficient. As these changes take hold, what are the implications for those doing business in China and for supply chains worldwide? And how are companies redeploying and reeducating their workforces as traditional factory jobs become automated and the need for technically proficient talent increases?
Hosted by The City of Guangzhou
Börje Ekholm, President and CEO, Ericsson Group
Till Reuter, Chief Executive Officer, KUKA
Tony Tan, Partner, Shanghai Office, McKinsey & Company
Wang Wenyin, Chairman, Amer International Group
Shoei Yamana, President and CEO, Konica Minolta
Zhang Jing, Founder and Chairman, Cedar Holdings Group
Moderator: Adam Lashinsky, Fortune
Photograph by Vivek Prakash/Fortune
Hafted Scraper - "PALEO TOOLS: The kinds of tools used by the Paleoindians can tell us much about their way of life. Most of the tools surviving today are made of stone. Spear points, knives, drills, and scrapers are typical Paleoindian artifacts. They were used for a variety of tasks, including hunting and butchering animals, processing plants, and working raw materials to make other tools. Archaeological sites of the Paleoindians contain mostly chipped stone tools and waste flakes left from the manufacturing process. However it is almost certain that these people made wide use of other raw materials including bone, wood, ivory, and antler. Objects made of these materials do not preserve as well as stone and have likely decayed over the past 10,000 years. Springs, sinkholes and deep river beds offer good conditions for preserving organic materials because of their high mineral content and lack of oxygen. Fragments of bone, wood, and other plant remains will give clues to future archaeologists who research the skills that Paleoindians needed to survive in Ice Age Florida. " ~ Display at the Florida Museum of Natural History. (Photo 091712-013.jpg) Paleoindians section of the Division of Historical Resources - Florida Museum of History - Where I used to work - September 17, 2012: A Walk Down Memory Lane - revisiting College Town - Tallahassee, Florida. (c) 2012 - photography by Leaf McGowan, Thomas Baurley, Eadaoin Bineid - technogypsie.com. To purchase this photo or to obtain permission to use, go to www.technogypsie.com/photography/
"PALEOINDIANS: The earliest people who inhabited North America are called Paleoindians. They came to Florida during the end of the last Ice Age, at least 12,000 years ago. Their way of life lasted for about 2,500 years. Archaeologists have found few Paleoindian sites. If, as it seems likely, these early people lived along the coast of Florida, their settlements have been covered by the rising sea level. Compared to later Florida Indian cultures, Paleoindians lived in small, widely dispersed groups. Their artifacts are often found around outcrops of a flint-like rock called chert. Pieces of chert were chipped, or knapped, to make stone tools. Paleoindian artifacts are also found in springs, sinkholes and rivers that were probably ancient waterholes. These were important sources of fresh water in an otherwise dry landscape.
PALEO TIMELINE: 12,000 B.P. to 9,500 B.P. (Before present) - EARLY PALEO PERIOD: 12,000-10,000 BP - Simpson point on mammoth ivory foreshaft (circa 11,500 BP) - First evidence of people on the Florida peninsula, Paleoindians live a semi-nomadic life, hunt big game like mastadon, climate was drier than today, and sea level is more than 100 feet lower than today. - Bison antiguns skull with embedded spearpoint, Wacissa River (circa 11,000 BP).
LATE PALEO PERIOD: 10,000 to 9500 BP - stone bola weight (circa 10,000 BP) had most big game animals extinct, wetter climate prevails, sea level rises gradually, several new styles of stone points appear, like the side notched bolan point. " ~ Display in the Florida Museum of Natural History.
For more information visit:
Paleoindians: www.technogypsie.com/science/?p=939 (expected publication December 2012)
Tallahassee: www.technogypsie.com/reviews/?p=5093 (Expected publication November 2012)
Florida: www.technogypsie.com/reviews/?p=5079 (Expected Publication December 2012)
For travel tales, visit:
Io Aircraft - www.ioaircraft.com
Drew Blair
www.linkedin.com/in/drew-b-25485312/
io aircraft, phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air-Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, hypersonic plane, hypersonic aircraft, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, defense science, missile defense agency, aerospike,
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
National Museum of Nuclear Science & History
Radiation Attenuating Gloves
International Biomedical, Inc., manufacturer of this Radiation Attenuating Surgical glove, noticed a need for protecting surgeon's hands while using radiation in treating patients. The surgeons were wearing leaded gowns and eyewear but nothing on their hands.
Why were they not protecting their hands? Unfortunately, the gloves they had at their disposal were not suited for surgical procedures because they were thick, bulky and very heavy. The surgeons could not operate with these large cumbersome gloves so they would simply not wear anything at all on their hands. The glove shown here is made of red lead oxide and a rubber product-Neoprene. Many of the standard surgical and examination gloves used today are made of Neoprene.
The red lead oxide is incorporated with the Neoprene in the manufacturing process and it is this lead that protects the surgeon by "reflecting" the radiation away from the glove. (The red lead oxide is what gives the glove the orange color.) There is no risk of lead poisoning from the lead because it is encapsulated by the Neoprene compound And because they are only .012" thick, the Radiation Attenuating Glove allows the surgeon the freedom of movement and dexterity needed to perform the delicate tasks associated with various surgical procedures while offering protection not afforded by standard surgical gloves
International Biomedical, Inc. is based in Austin, Texas, USA and may be contacted at 8508 Cross Park Drive, Austin, TX 78754-4532. Phone - 512.873.0033 Fax-512.873.9090 Web site: www.int-bio.com
The existing Freeport Community Center & a historic Edward B. Mallett house has been joined by a spacious addition to provide new social services offices, thrift store, teen center, coffee bar & multi-funtion community room. Not only was there a goal to preserve history landmarks....but to obtain serious energy savings!
Hunter XCI Foil product is used in the construction of the renovation & addition of the Freeport Community Center.. XCI Foil is a high thermal, rigid building insulation composed of a closed cell polyiso foam core bonded on-line during the manufacturing process to an impermeable foil facing material. It is designed for use in commercial cavity wall applications to provide continuous insulation within the building envelope.
Hunter Xci polyiso products:
- Have the highest R-Value per inch of any insulation
- NFPA 285 TEST - Passed
- Energy Star approved
- Contribute toward LEED certification credits
- HCFC, CFC, zero ODP, and negligable GWP.
Construction by: Warren Construction
XCI Twitter: twitter.com/#!/HunterXCI
XCI Facebook: www.facebook.com/pages/Hunter-Xci-Exterior-Continuous-Ins...
View more: www.hunterxci.com/
Io Aircraft - www.ioaircraft.com
Drew Blair
www.linkedin.com/in/drew-b-25485312/
io aircraft, phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air-Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, hypersonic plane, hypersonic aircraft, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, defense science, missile defense agency, aerospike,
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
Hunter XCI Foil product is used in the construction of the new commons building at University of Northwestern Ohio. XCI Foil is a high thermal, rigid building insulation composed of a closed cell polyiso foam core bonded on-line during the manufacturing process to an impermeable foil facing material. It is designed for use in commercial cavity wall applications to provide continuous insulation within the building envelope.
Hunter Xci polyiso products:
- Have the highest R-Value per inch of any insulation
- NFPA 285 TEST - Passed
- Energy Star approved
- Contribute toward LEED certification credits
- HCFC, CFC, zero ODP, and negligable GWP.
XCI Twitter: twitter.com/#!/HunterXCI
XCI Facebook: www.facebook.com/pages/Hunter-Xci-Exterior-Continuous-Ins...
View more: www.hunterxci.com/
Super-Hydrophobic Coatings
AquaShield develops a wide range of “next generation” durable waterproof/ water repellents, through the science of super hydrophobic nano-polymer coating technologies. Many of these formulations and coatings take the form of easy to use waterproofing sprays. They are strong enough for any manufacturing process or professional application, but easy enough to use that they are ideal to use as a household product.
All AquaShield products offer water repellent nano-coatings which can turn virtually any substrate from wood and concrete, to leather and wool into a super hydrophobic surface. The benefits of these innovative technologies are limitless… Imagine a rain coat made of wool, or an outdoor parking lot in a wet climate that requires 1/10th the maintenance.
Auto Body Care and Car Detailing Solutions
The AquaShield Car Care line of products is a complete solution for auto care. From hydrophobic ceramic coatings that far outperform the best car wax, to a high shine tire care product. There is even nano-coating engine oil additive for improved performance and fuel conservation.
While it’s true that there are many hydrophobic sprays available today, there are none that can match AquaShield’s results, while maintaining the ease of application, zero toxicity, and an eco-friendly status, at an affordable price. We provide durable , UV resistant and long lasting products that can handle extremely harsh conditions, sand and dust abrasion, plus frost and ice and snow. Super-Hydrophobic Ceramic & Waterproof Nano Coatings - Global Opportunities Available 866-285-105. Visit Us @www.aquashieldpro.com. #Aquashieldpro #nanocoatings
(En) Founded in 1906, the Coking Plant of Anderlues was specialized in the production of coke for industrial use.
Coke was obtained by distillation of coal in furnaces and, thanks to its superior fuel coal properties, it was used afterwards to feed the blast furnaces in the steel manufacturing process.
Closed and abandoned since 2002, the site has since undergone many losses and damages, not including an important pollution. While some buildings have now been demolished, there are however still some important parts of the former coking plant.
Among them, the former coal tower, next to the imposing "battery" of 38 furnaces, where the coke was produced. Besides them, we still can see the administrative buildings, the power station with its cooling tower, and buildings for the by-products, which were obtained by recovering the tar and coal gas. There are also a gasometer north side, the coal tip east side and a settling basin south side.
-----------
(Fr) Fondées en 1906, les Cokeries d'Anderlues étaient spécialisées dans la fabrication de coke à usage industriel.
Le coke était obtenu par distillation de la houille dans des fours et, grâce à ses propriétés combustibles supérieures au charbon, il servait par après à alimenter les hauts-fourneaux dans le processus de fabrication de l'acier.
Fermé et laissé à l'abandon depuis 2002, le site a depuis lors subi de nombreuses pertes et dégradations, sans compter la pollution qui y règne. Si certains bâtiments (comme l'ancien lavoir à charbon) ont aujourd'hui été démolis, on retrouve encore toutefois certaines parties importantes de cette ancienne cokerie.
Parmi celles-ci, l'ancienne tour à charbon suivie de près par l'imposante "batterie" de 38 fours, où était produit le coke. A côté d'eux, on découvre également les bâtiments administratifs, la centrale électrique avec sa tour de refroidissement, ainsi que les bâtiments des sous-produits, lesquels étaient obtenus par récupération du goudron et du gaz de houille. Et en périphérie, on retrouve un gazomètre côté nord, le terril à l'est et un bassin de décantation côté sud.
Io Aircraft - www.ioaircraft.com
Drew Blair
www.linkedin.com/in/drew-b-25485312/
io aircraft, phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air-Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, hypersonic plane, hypersonic aircraft, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, defense science, missile defense agency, aerospike,
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
Made in Romania!
Traditional bag from Romania, handcrafted using wool embroidery. You may daily use it to carry different stuff. Perfect for use as a school/student purse, a jewelry bag, or other valuables for a night out dancing.
Made from natural wool painted with natural colors by popular artists. Geometrical motives used, that give these bags some traditional decorative features. The manufacturing process for this type of tissue has been kept since the early ages of the Romanian history (approx. 700 A.D.). The object behind traditional clothes and accessories in Romanian culture, is the weaving loom.
There are thousands of ways in which the talented hands of our ancestors have been crafting true treasures of beauty. Handed down from generation to generation, but preserving the personality of Romanian people, these techniques are still being used during present times.
Size: 35 X 31 cm / 13.8 x 12.2 inch
Handle: 100 cm / 39.4 inch
Weight: 400 g
austin, texas
1977
motorola semiconductor plant
part of an archival project, featuring the photographs of nick dewolf
© the Nick DeWolf Foundation
Image-use requests are welcome via flickrmail or nickdewolfphotoarchive [at] gmail [dot] com
Io Aircraft - www.ioaircraft.com
Drew Blair
www.linkedin.com/in/drew-b-25485312/
io aircraft, phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air-Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, hypersonic plane, hypersonic aircraft, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, defense science, missile defense agency, aerospike,
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
The existing Freeport Community Center & a historic Edward B. Mallett house has been joined by a spacious addition to provide new social services offices, thrift store, teen center, coffee bar & multi-funtion community room. Not only was there a goal to preserve history landmarks....but to obtain serious energy savings!
Hunter XCI Foil product is used in the construction of the renovation & addition of the Freeport Community Center.. XCI Foil is a high thermal, rigid building insulation composed of a closed cell polyiso foam core bonded on-line during the manufacturing process to an impermeable foil facing material. It is designed for use in commercial cavity wall applications to provide continuous insulation within the building envelope.
Hunter Xci polyiso products:
- Have the highest R-Value per inch of any insulation
- NFPA 285 TEST - Passed
- Energy Star approved
- Contribute toward LEED certification credits
- HCFC, CFC, zero ODP, and negligable GWP.
Construction by: Warren Construction
XCI Twitter: twitter.com/#!/HunterXCI
XCI Facebook: www.facebook.com/pages/Hunter-Xci-Exterior-Continuous-Ins...
View more: www.hunterxci.com/
Thai silk is produced from the cocoons of Thai silkworms. Thai weavers, mainly from the Khorat Plateau in the northeast region of Thailand, raise the caterpillars on a steady diet of mulberry leaves. Khorat is the center of the silk industry in Thailand and a steady supplier of rose Thai silk for many generations.
Today, Thai silk is famous for its special qualities produced through unparalleled manufacturing processes, bearing unique patterns and colors.
3D computer simulations allow Ford engineers to evaluate manufacturing processes in a virtual environment.
JCC received a grant award through the Western New York Regional Economic Development Council’s Consolidated Funding Application to offer the Machinist Training Program which features classroom and hands-on training and consists of a mixture of college credit and non-credit classes spread over 12 months. Training for the manufacturing environment includes drafting, shop math, CNC machining, teamwork, and lean manufacturing processes.
St. Stevens Church, Birmingham, AL: Xci Class A is an exterior wall insulation panel composed of a Class A rigid polyisocyanurate foam core laminated during the manufacturing process to embossed foil facers.
Hunter Xci polyiso products:
- Have the highest R-Value per inch of any insulation
- NFPA 285 TEST - Passed
- Contribute toward LEED certification credits
- HCFC, CFC, zero ODP, and negligable GWP.
XCI Twitter: twitter.com/HunterXCI
XCI Facebook: www.facebook.com/pages/Hunter-Xci-Exterior-Continuous-Ins...
View more: www.hunterxci.com/
040
Friday, December 8th, 2017
Fortune Global Forum 2017
Guangzhou, China
8:00 AMâ9:20 AM
SMART MANUFACTURING AND THE INTERNET OF THINGS
Around the world, factory floors and assembly lines are becoming highly automated, combining human ingenuity with data and technology to revolutionize product and productivity outcomes. As the notion of a âfactory of the futureâ continues to evolve, how are companies incorporating âsmartâ and connected products into their manufacturing process? From sensors and robots to 3D printing and green technology, global companies are experimenting with a variety of methods to streamline, scale, and sustain their business. Here in China, manufacturers have been asked to deliver on the nationâs âMade in China 2025â strategy and are aggressively pursuing their own strategies to become smarter, greener, and more efficient. As these changes take hold, what are the implications for those doing business in China and for supply chains worldwide? And how are companies redeploying and reeducating their workforces as traditional factory jobs become automated and the need for technically proficient talent increases?
Hosted by The City of Guangzhou
Börje Ekholm, President and CEO, Ericsson Group
Till Reuter, Chief Executive Officer, KUKA
Tony Tan, Partner, Shanghai Office, McKinsey & Company
Wang Wenyin, Chairman, Amer International Group
Shoei Yamana, President and CEO, Konica Minolta
Zhang Jing, Founder and Chairman, Cedar Holdings Group
Moderator: Adam Lashinsky, Fortune
Photograph by Vivek Prakash/Fortune
040
Friday, December 8th, 2017
Fortune Global Forum 2017
Guangzhou, China
8:00 AMâ9:20 AM
SMART MANUFACTURING AND THE INTERNET OF THINGS
Around the world, factory floors and assembly lines are becoming highly automated, combining human ingenuity with data and technology to revolutionize product and productivity outcomes. As the notion of a âfactory of the futureâ continues to evolve, how are companies incorporating âsmartâ and connected products into their manufacturing process? From sensors and robots to 3D printing and green technology, global companies are experimenting with a variety of methods to streamline, scale, and sustain their business. Here in China, manufacturers have been asked to deliver on the nationâs âMade in China 2025â strategy and are aggressively pursuing their own strategies to become smarter, greener, and more efficient. As these changes take hold, what are the implications for those doing business in China and for supply chains worldwide? And how are companies redeploying and reeducating their workforces as traditional factory jobs become automated and the need for technically proficient talent increases?
Hosted by The City of Guangzhou
Börje Ekholm, President and CEO, Ericsson Group
Till Reuter, Chief Executive Officer, KUKA
Tony Tan, Partner, Shanghai Office, McKinsey & Company
Wang Wenyin, Chairman, Amer International Group
Shoei Yamana, President and CEO, Konica Minolta
Zhang Jing, Founder and Chairman, Cedar Holdings Group
Moderator: Adam Lashinsky, Fortune
Photograph by Vivek Prakash/Fortune