This is the famous "Hörder Fackel", over 80m high. The surplus gas from the steel manufacturing process was burned here. The torch was in use for some decades and was one of the towns landmarks. It was blown up in January 2004.

The pictures were taken on a freezing cold February morning in 2003. It was the last chance to catch this wonderful light composition of winter morning, cold air and low sun. The steelworks was taken down later that year.

Taken with my Canon T90, then scanned from slide.

www.route-industriekultur.de/routen/06/06_46.htm

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!

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.

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:

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- 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!

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.

Are you aware of the basic problems in the clothing manufacturing process? In the clothing manufacturing process, there are a few basic problems that new entrepreneurs often face. Garment production is a well-organized process that includes steps like laying, marking, cutting, sewing, inspecting, finishing, pressing, and packing. This is the transformation of raw materials into final goods. It will be difficult to keep the industry going if manufacturing isn’t up to standard and material preparation has not been done properly during the testing and development phase.

For details, www.beautifulcng.com/clothing-manufacturing-process-probl...

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!

www.tiannengglobal.com/products/lead-acid-battery/

Always making progress for lead acid battery to provide great reliability and excellent performance.

With more than 34 years' expertise in lead-acid battery industry, Tianneng Battery produces lead-acid cells that are reliable with their higher performances, including stronger power, extended mileage, and longer cycle life. With 1 million unit production capacity, you can find all kinds of lead-acid batteries in Tianneng Group, like the motive battery for electric vehicles, traction battery for forklifts, reserve batteries for data centers, lead-acid storage battery for solar systems, SLI battery for automobiles, etc. As a professional lead acid battery supplier, Tianneng Battery can provide you with high-quality lead-acid battery packs at competitive marketing prices. Feel free to contact us for more information.

DIFFERENT TYPES OF LEAD ACID BATTERIES FOR SALE

Motive Battery

High energy density of our deep cycle batteries ensures longer mileage

Extended cycle life promises outstanding service life

Continuous large current realizes great gradeability

Low and high temp can performance withstands harsh environments.

High-rate charge acceptance enables fast-charge requirement

Traction Battery

Instant discharge current ensures traction requirements

Continuous large current drives heavy-duty load

Extended cycle life promises outstanding service life

High temp. performance provides great temp. tolerance

High-rate charge acceptance enables fast-charge requirement

GEL Technology realizes maintenance-free requirements

Reserve Battery

Extended floating life promises outstanding service life

High-rate instant discharge capability meets the need of UPS/EPS

Remarkable temp. tolerance adapts to wide operating temp.

Excellent consistency allows flexible grouping

Front terminal type enables easy connection

AGM/GEL Technology realizes maintenance-free requirements

Energy Storage Battery

Outstanding conversion efficiency provides the highest energy efficiency

Extended cycle life promises outstanding service life

Unique PSOC performance overcomes partial statue of charge

Remarkable temp. tolerance adapts to wide operating temp.

Excellent consistency allows flexible grouping

AGM/GEL Technology realizes maintenance-free requirements

SLI Battery

High-rate instant discharge capability enables quick start

Remarkable CCA performance ensures low-temp. starting

Large reserve capacity fulfills the load consumption on-board

Lower water loss decreases the maintenance rate

Extended cycle life promises outstanding service life

Outstanding DCA performance adapts to frequent start

Start-stop design and technology

Manufacturing Advantages of Lead Acid Battery

Reliable Production Process

Patent technology and innovation for the rechargeable lead-acid battery.

Leading Quality Control

Strict quality control throughout the automation and intelligent manufacturing process of the lead accumulator cell.

Abundant Production Capacity

Tianneng Group can produce 1 million units of lead-acid batteries per day.

Uses of Lead-acid Battery

For starting, ignition, and lighting of various automobiles, tractors, and diesel engines. With the small internal resistance, the lead-acid storage battery is widely for vehicles that require large current discharge when starting.

Used in power plants, substations, communication, hospitals, etc. The lead-acid battery cell can also work as a backup power source for protection, automatic control, emergency lighting, communication, etc.;

Used for all kinds of battery cars, forklifts, forklifts, mine electric locomotives, etc. Capable of meeting the requirements of thick plate and large capacity, the lead storage cell can work as an electric traction battery and lighting power supply as well.

Lead-acid Battery Manufacturing Process

Tianneng has the first domestic motive battery automatic continuous casting, rolling, continuous punching, and continuous coating production demonstration line, the domestic first small-density power battery intelligent automatic assembly demonstration production line, and other digital production lines and a complete digital industry. The supply chain of our lead-acid accumulator cell has the leading advantages of high equipment utilization, relatively stable production capacity, high product quality, flexible operation, and great product adaptability.

Maintenance of Lead-Acid Accumulator

Prevent electrolytes from flowing out. At the time of charging, the lead-acid battery will generate hydrogen and oxygen, and since the lead accumulator cell is a relatively closed space, the internal pressure of the battery will then inevitably increase when charging. Under internal pressure, the electrolyte inside the battery may more or less flow out of the battery. Thus, it is of great significance to clean up the electrolyte on the surface of the lead storage battery and prevent the outflow of the electrolyte. Otherwise, it will accelerate the corrosion of electrode screws.

Keep the lead-acid storage cell and connecting wires dry and clean to avoid leakage. Regularly clean the battery surface and connecting wires with a dry cloth. Do not use organic solvents to wipe. If the appearance of the lead-acid accumulator cell is adversely affected, it should be replaced in time.

Check the terminals regularly and there should be no looseness. Remove oxides from the terminals and wire joints, and strictly prohibit metal debris and other debris from entering the lead-acid battery packs.

Try to avoid deep discharge and over-discharge, the charge is best when the discharge depth is about 70% (that is when the remaining power is about 30%).

The lead storage cells should use the original charger and the charger matched by the regular manufacturer. After the lead-acid accumulator cell is fully charged, it should not be charged for a long time to avoid overcharging and losing water. The charging process should avoid outdoor cold weather in winter and exposure to hot sun or other high-temperature scenes in summer.

When the lead-acid battery is in storage, the battery should be fully charged and stored, and periodically recharged every other month to avoid sulphation and capacity loss of the battery plate.

When the battery usage time is suddenly shortened sharply or the discharge performance is greatly reduced, it should be checked by professional maintenance staffs in time to check whether the charger, motor, battery, etc. are abnormal, and abnormalities are eliminated in time.

During the use of the lead accumulator cell, the maintenance of single charge and single discharge should be done every six months, so as to extend the service life of the lead-acid cell.

If you have any other questions regarding the maintenance of lead-acid accumulators, feel free to contact Tianneng Group, one of the professional lead acid battery suppliers in China, at any time!

FAQS OF LEAD ACID BATTERY

Q. Do lead-acid batteries need to be maintained with water?

A.Maintenance-free AGM/GEL technology is widely used in the production of our lead-acid batteries for sale. So there is no need to add water during normal application.

Q. What are the common causes of failure of lead-acid batteries?

A.Under normal use of the lead-acid cell, the main reason is that the battery performance is reduced due to the softening of anode lead paste and the increase of grid corrosion.

Q. What will happen if the lead-acid battery is not charged for a long time?

A.If the lead-acid battery pack is not charged and discharged for more than 6 months, it will lead to negative sulfation, resulting in a significant reduction in capacity, etc.

Q. What is the operating temperature range for lead acid battery?

A.Lead acid storage cell enjoys a wide range of operating temperature, from -20°C to 50°C, and it will have a higher ratio of discharge capacity than lithium battery.

Q. Do lead-acid batteries have any explosion risk?

A.Most lead-acid batteries for sale at Tianneng Group are valve-regulated lead-acid batteries, and this kind of rechargeable storage battery will automatically exhaust internal gas and release pressure, so there is no risk of explosion under normal application.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

Some background:

In the grand scope of World War 2 fighter aircraft there is a little-remembered French design designated the Arsenal "VG-33". The aircraft was born from a rather lengthy line of prototype developments put forth by the company in the years leading up to World War 2 and the VG-33 and its derivatives represented the culmination of this work before the German invasion rendered all further work moot.

The aircraft never saw combat action in the Battle of France. Its arrival was simply too late to have any effect on the outcome of the German plans. Therefore, with limited production and very limited combat service during the defence of Paris in May 1940, it largely fell into the pages of history with all completed models lost.

Specifications:

Crew: 1

Length: 28.05 ft (8.55 m)

Width: 35.43 ft (10.80 m)

Height: 10.83ft (3.30 m)

Weight: Empty 4,519 lb (2,050 kg), MTOW 5,853 lb (2,655 kg)

Maximum Speed: 398 mph (641 kmh at 10.000m)

Maximum Range: 746 miles (1,200 km)

Service Ceiling: 39,305 ft (12.000 m; 7.458 miles)

Powerplant:

1x Hispano-Suiza 12Y-77 V-12 liquid-cooled inline piston engine

with two Brown-Boveri exhaust turbochargers, developing 1,100 hp (820 kW).

Armament:

1x 20mm Hispano-Suiza HS.404 cannon, firing through the propeller hub

4x 7.5mm MAC 1934 machine guns in the outer wings

The kit and its assembly:

I found the VG-33 fascinating - an obscure and sleek fighter with lots of potential that suffered mainly from bad timing. There are actually VG-33 kits from Azur and Pegasus, but how much more fun is it to create your own interpretation of the historic events, esp. as a submission to a Battle of Britain Group Build at whatifmodelers.com?

I had this project on the whif agenda for a long time, and kept my eyes open for potential models. One day I encountered Amodel's Su-1 and Su-3 kits and was stunned by this aircraft's overall similarity to the VG-33. When I found the real VG-38 description I decided to convert the Su-3 into this elusive French fighter!

The Su-3 was built mainly OOB, it is a nice kit with much detail, even though it needs some work as a short run offering. I kept the odd radiator installation of the Suchoj aircraft, but changed the landing gear from a P-40 style design (retracting backwards and rotating 90°) into a conservative, inward retracting system. I even found forked gear struts in the spares box, from a Fiat G.50. The covers come from a Hawker Hurricane, and the wells were cut out from this pattern, while the rest of the old wells was filled with putty.

Further mods include the cleaned cowling (the Su-3's fuselage-mounted machine guns had to go), while machine guns in the wings were added. The flaps were lowered, too, and the small cockpit canopy cut in two pieces in, for an opened position - a shame you can hardly see anything from the neat interior. Two large antenna masts complete the French style.

Painting and markings:

Again, a rather conservative choice: typical French Air Force colors, in Khaki/Dark Brown/Blue Gray with light blue-gray undersides.

One very inspiring fact about the French tricolor-paint scheme is that no aircraft looked like the other – except for a few types, every aircraft had an individual scheme with more or less complexity or even artistic approach. Even the colors were only vaguely unified: Field mixes were common, as well as mods with other colors that were mixed into the basic three tones!

I settled for a scheme I found on a 1940 Curtiss 75, with clearly defined edges between the paint fields. Anything goes! I used French Khaki, Dark Blue Grey and Light Blue Grey (for the undersides) from Modelmaster's Authentic Enamels range, and Humbrol 170 (Brown Bess) for the Chestnut Brown. Interior surfaces were painted in dark grey (Humbrol 32) while the landing gear well parts of the wings were painted in Aluminum Dope (Humbrol 56).

The decals mainly come from a Hobby Boss Dewoitine D.520, but also from a PrintScale aftermarket sheet and the scrap box.

The kit was slightly weathered with a black ink wash and some dry-painting, more for a dramatic effect than simulating wear and tear, since any aircraft from the VG-33 family would only have had a very short service career.

Well, a travesty whif - and who would expect an obscure Soviet experimental fighter to perform as a lookalike for an even more obscure French experimental fighter? IMHO, it works pretty fine - conservative sould might fair over the spinal radiator outlet and open the dorsal installation, overall both aircraft are very similar in shape, size and layout. :D

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Nation : Czechoslovakia

Pavilion Name : Czechoslovakia Pavilion

Subject : Handicraft

Island : Ile Notre Dame

Description : Modern Czechoslovakian glass showcased in the Hall of Traditions.

General Description:

The two storey Czechoslovakia Pavilion consisted of two buildings linked by an entrance hall. A simple, clear architectural strategy provided a harmonious backdrop for the exhibition's exciting displays. The first building featured two levels of exhibition space with a central courtyard which drew some of the largest crowds at Expo. Czechoslovakian art, technology and industry were presented to visitors through an attractive mixture of light, sound and video. The Hall of Centuries exhibit showcased texts and artifacts from ancient royalty. In the Hall of Tradition, visitors could find old and new glass and crystal and learn about their manufacturing processes. The World of Children enchanted the pavilion's younger visitors featuring puppet shows performing traditional tales. The second building featured four restaurants; Le Bistro served light snacks; the Bratislava Inn was a wine tavern; the Castle Restaurant featured fine Czechoslovakian cuisine; and the Prague was home to the famous pilsener Urquell beer. Offices, a gift shop and a theatre could also be found in this second Czechoslovakian building.

Source: digital.library.mcgill.ca/expo-67

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!

Went for a morning walk around Alcester in Warwickshire. Alcester is market town that was founded by the Romans.

A look at Minerva Mill in Alcester. Located on Station Road.

Grade II Listed Building.

Minerva Needle Works

Listing Text

The following building shall be added:

ALCESTER

SP0857 STATION ROAD

419-0/4/10000 (North East side)

Minerva Needle Works

II

Needlemaking factory. Circa 1880-5 for Alfred Allwood, needlemaker; C20 extension at

rear. Red brick with terracotta dressings. Hipped Welsh slate roof with lead roll hips and

crested ridge tiles. 2 small brick axial stacks. PLAN: Long and shallow 20-bay range with 2

short rear wings at either end, the righthand wing's SE return has a 5-bay front; the space

between the rear wings has been infilled by a C20 extension. Italianate style. EXTERIOR:

3 storeys. 20-bay south west front with round-headed windows in recessed panels with

enriched moulded terracotta imposts and heads and ramped cills. Also moulded terracotta

eaves course. Multi-pane cast-iron windows. Central doorway with segmental arch.

Righthand south east return is similar, but 5 bays and with round-headed doorway. At rear

2-bay wings to left and right, C20 extension between the wings and 3 bays to right.

INTERIOR: Part of the rear wall of the main range has been demolished creating partly

open plan on the ground and tint floors. HISTORY: William Allwood and his son Joseph

were needlemakers in premises at Henley Street, Alcester, but here they employed

outworkers for such stages in the manufacturing process as spitting and packeting and the

scouring would have been done by another mill. The firm was so successful that in circa

1880-5 Joseph Allwood's son, Alfred, moved to this purpose-built factory in Station Road.

It is believed that all the processes of needlemaking were done here. The needle's brand

name was Minerva and the firm also produced hat-pins with glass birds on the end. In 1912

the premises were bought by Terry's Springs, makers of the Anglepoise lamp. SOURCE:

Needlemakers and Needlemaking of Alcester, Sambourne and Studley Area, paper no.24;

Alcester and District Local History Society; 1981.

Listing NGR: SP0857557637

This text is from the original listing, and may not necessarily reflect the current setting of the building.

Prism Pharma Machinery founded in 2003 and has been manufacturing Process equipments for Pharmaceuticals, Biotech, Nutraceuticals, Cosmetics, Foods, Dairy, Bakery, Confectionery, Agro Chemical, Chemical, Herbals, Paint, Ceramics &, Catalysts for production, pilot & lab scale.Prism Pharma Machinery Ahmedabad, Gujarat, INDIA.

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

In spring 1917, the British Royal Flying Corps introduced the Sopwith Triplane, a three-winged version of the earlier Sopwith Pup fighter. The “Tripe” was only built in limited numbers, but it was issued to elite pilots, such as the famous “Black Flight” of the Royal Naval Air Service—commanded by ace Raymond Collishaw, the Black Flight’s five Triplanes shot down 87 German aircraft in three months.

The German Luftstreitskrafte reacted with shock. To this point, the Germans had usually enjoyed a qualitative advantage over the Allies in the air with their Albatros D.IIIs The Triplane could operate higher and was faster than German fighters, which gave their British and Canadian adversaries the advantage in a dogfight. Germany embarked on a crash program to field their own triplanes, with 37 manufacturers all producing prototypes. The best by far, however, was Fokker’s Dreidekker I, abbreviated Dr.I. After a short period of testing of prototypes, two pre-production aircraft were built and sent to the Western Front for evaluation. Both were given to exceptional pilots—Manfred von Richthofen and Werner Voss. Richthofen, testing the Dr.I in combat for the first time in September 1917, promptly shot down two aircraft and proclaimed the Dr.I a superb aircraft, if tricky to fly. If there was any doubt of its lethality, it was removed on 23 September, when Voss engaged nine British SE.5s of 56 Squadron, all of which were flown by British aces with more than ten victories apiece. Though Voss was killed, his skill and the Dr.I’s manueverability held off nine British aces for ten minutes. Fokker immediately received a production order for 300 Dr.Is.

In combat, the Dr.I was not as fast as the Albatros, but it had a higher rate of climb and phenomenal manueverability—the design was slightly unstable, but an experienced pilot could use its high lift, light controls, and the torque of the engine to make snap rolls to the right almost within the length of the aircraft. It required an experienced pilot, especially on landing, where the torque of the engine and the wings also had a tendency to ground-loop the aircraft. This could be fatal, because the position of the two Spandau machine guns extending into the cockpit could cause a crash-landing pilot to hurtle forward into the gun butts, face-first. The Oberursel engine had a tendency to fall off in power at higher altitudes due to poor lubrication. By far, however, the worst drawback of the Dr.I was its tendency towards wing failures, which were initially believed due to poor workmanship by Fokker. It would be not until after the war that it was learned that the very triple-winged design of the Dreidekker was the problem: the top wing exerted more lift than the bottom two, with the result that the top wing would literally lift itself away from the rest of the aircraft. While it was possible to still fly with the missing top wing, the Dr.I would not fly for long and the pilot would have to make a high-speed landing in an aircraft notorious for crash landings.

Though the Dr.I was issued to two Jasta wings, including von Richthofen’s, in 1917-1918, it was never very popular with the majority of German pilots, and the production of the superb Fokker D.VII, which started about the same time, meant that the Luftstreitskrafte already had a fighter that was faster and more durable than the Dr.I, if not quite as manueverable. A few German aces still preferred the Dr.I, namely von Richthofen—because of the Dreidekker was good at something, it was attacking from ambush. A skilled ace could quickly gain altitude over an unsuspecting enemy, dive down, attack, and then use the kinetic energy built in the dive to zoom back to position, or manuever out of trouble with a quick right roll. Von Richthofen would score his last 20 (out of 80) kills in the Dr.I.

Following the end of World War I, nearly all of Germany’s fighters were purposely burned, either by their own pilots or by the Allies. By World War II, only one Dr.I was known to exist, one of von Richthofen’s aircraft, preserved in a museum in Berlin; the museum was flattened in an Allied bombing raid in 1944. Today, only scattered pieces of original Dr.Is exist. However, the simple manufacturing process of World War I fighters meant that reproductions could easily be built, and several dozen Dr.I replicas continue to fly today.

Naturally, this is a replica Dr.I, built in 1982 by a private collector in Ohio. Planes of Fame in Chino, California acquired it in 2013. Like many Dr.I replicas, it is painted in Richthofen's colors, that of his "show plane," 152/17, which retained the earlier Maltese crosses and white stripes; the Dr.I he was killed in had Latin crosses and no white markings. It is still flyable, and is displayed with two of the Dr.I's adversaries--a Sopwith Pup and a Hanriot HD.1.

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.

3T RPD created this model of the Berlin Free Library Oval Roof for Foster & Partners using the plastic Additive Manufacturing process. www.3trpd.co.uk

Xci Foil is a high thermal, rigid building insulation composed of a closed cell polyisocyanurate 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.

XCI Twitter: twitter.com/HunterXCI

XCI Facebook: www.facebook.com/pages/Hunter-Xci-Exterior-Continuous-Ins...

View more: www.hunterxci.com/

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!

The current Prim range.

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!

Manufacturing process of rich silk sarees in Kanchipuram -

1.Silk thread rolled in those spinners

2.Weaver spinning a patterned saree.

3.Silk thread arranged in a weaving machine.

4.Ready product in the market for selling.

Indian saris come in a mind-boggling variety of textures, colors and designs. Silk saris form an integral part of Indian weddings and celebrations. The rich weave and feel of kanjivaram silk saris hold everyone in their sway. Be it simple contrast border silk sarees or those with gold zari dots and patterns, the kanjivaram silk sari continues to hold pride of place among the various silk sari varieties available in the country.

* one normal medium range silk saree takes almost fifteen days to get ready. All work is done manually and is time consuming.

HercuWall is manufactured with EPS foam.

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.

This image was reproduced from slides taken by George C. Guthrie, editor of the Ardrossan & Saltcoats Herald. These slides represent only a small selection of the complete collection, which gives a valuable insight into the early half of the 20th century. The complete collection of the Guthrie slides is held at The Heritage Centre.

A view of the loading gates at the Nobel Factory in Ardeer circa 1900, the employees are all wearing Tam O’Shanters except of course for the foreman with his bowler hat.

In the Early 19th century nitro-glycerine was the main explosive used in mining throughout the world, even though it was incredibly unstable, it had caused many fatal accidents in its use and just as many in its manufacture. Nitro-glycerine was so unsafe that many countries outright banned its use, a safer form of blasting had to be developed.

Alfred Nobel invented Dynamite in 1864; he used a method of saturating diatomaceous earth with nitro-glycerine and various other chemicals to make a solid compound. This made it far safer to handle; it could even undergo force-impacts and not explode, unlike nitro-glycerine that would sometimes explode literally at the drop of a hat. He was only able to manufacture small quantities at a time, as had limited working space and it was still a very dangerous manufacturing process.

In choosing the location for his new explosives plant, he sought an isolated location, with goods access links by sea. The Ardeer peninsula seemed perfect with it was isolated from any major settlement and could be accessed by sea easily. The plant opened for business December 1872, a notice appeared in the Mining Journal:

'The British Dynamite Company, having erected extensive works at Ardeer, Ayrshire, near Glasgow, with all Mr. Nobel's recent improvements for the manufacture of dynamite, are now prepared to execute orders for Home Consumption and Export.'

For more information on the Yesterd@ys project, please visit Our Website, or email us at NAHeritage@North-Ayrshire.gov.uk

DISCLAIMER

All archival images on this website have been made available by The North Ayrshire Council in good faith for reference and/or educational purposes only and without intent to breach any proprietary rights which may subsist in the work. Images may not be printed, copied, distributed, published or used for any commercial purposes without the prior written consent of the individual or body which holds such rights. Should any alleged breach of proprietary rights be brought to the attention of The North Ayrshire Council, relevant material will be removed from the website with immediate effect.

The North Ayrshire Council is not responsible for the content, reliability or availability of external websites and cannot be held liable for any loss or damage to the user, of whatever kind, arising either directly or indirectly from use of same. Listing should not be taken as an endorsement of any kind and in particular, of views expressed within any such site.

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

SureFlex coax jumpers are manufactured using a patented process that utilizes a 360-degree lead-free solder joint to physically bond the connector to the jumper. This highly controlled manufacturing process produces a premium cable assembly that delivers higher RF performance, consistent reliability and outstanding durability. Each assembly is individually tested and guaranteed for exceptional electrical performance and superior weather resistance. And because SureFlex cable assemblies are pre-manufactured, they arrive on-site ready to go. You save valuable time and potential connection error. The SureFlex process is used on all CommScope cable assemblies and for nearly two decades has been recognized as a leading product for RF performance in the wireless industry. As focus in the industry has moved towards high PIM performance products, so has the SureFlex process with the introduction of new IP in 2013 and the recent release of the industry’s first D-Class (Dynamic PIM) rated cable assembly products. www.commscope.com/top-40-innovations/

DUMBO, Brooklyn

Features: Nineteen bays on Bridge Street, nine bays on Water Street, and nine bays on Front Street; large segmental-arch openings separated by brick piers; end bays on Bridge Street narrower than other bays; building reflects slight slope of site, with the basement only partially above sidewalk level on Front Street rising to a full story on Water Street; multi-pane metal windows with operable awnings; iron tie rods; corbelled cornice; pedestrian entrance in westernmost bays on Front Street and Water Street; bluestone stairs at pedestrian entrance on Water Street; three fire escapes on Bridge Street.

Significant alterations: Two corner bays on Front Street partially filled in and converted into loading docks on first floor; eighth bay on Water Street partially filled in and converted into vehicular entrance.

History: The western portion of this block was home to the Union White Lead Works (later the National Lead Company) which began purchasing property on the block as early as 1837. The lead company’s property was sold to James and John H. Hanan in 1893. Although already occupied by a factory, James Hanan and his son John chose to demolish the existing buildings and replace it with a new factory for the manufacturing of shoes. Hanan initially announced construction of a seven-story structure; he actually built a five-story factory. Even before purchasing the DUMBO property, James Hanan was a resident of Brooklyn, living in a large mansion at 45 Eighth Avenue (demolished) in Park Slope. James Hanan (1819-1897) was born in Ireland and learned the shoe trade from his father. In 1849 he moved to America and in 1854 established a small shoemaking business in New York City. In about 1865, his son, John Henry Hanan (1849-1920), entered his father’s firm, and in 1882 the company became Hanan & Son.

The Hanan Company was among the first to stamp the firm’s name on every shoe, a daring idea at a time when most people still sought shoes handmade by the dealer. The firm was successful and in 1888 Hanan began opening retail stores to sell the factory’s product directly to consumers.

In 1894, the company had stores in New York, Brooklyn, Boston, Philadelphia, Cleveland, Milwaukee, New Haven, Buffalo, Chicago, and St. Paul. By 1914 the firm had thirteen retail stores in the United States and Europe (apparently in London and Paris).

Shoe manufacturing was a major industry in Brooklyn in the late nineteenth century, with 65 factories doing a combined business of $2,300,000 in 1894; one-third of that business was done at the Hanan factory. The manufacture of a pair of shoes began on the upper floor of the factory where thin leather uppers were cut from patterns; women then stitched the uppers together on sewing machines; boys then took the uppers and smoothed the seams. The uppers were then moved to the third floor where lasters worked. The uppers were tacked to lasts and leather attached to the last mold to create the form of the bottom of the shoe. The bottom and upper were sewn together and then the shoes proceed to men who inserted the insoles, largely by machine. Then glue was placed on the insole and another employee added the heavy sole, again by machine. The shoes now moved sown to the next floor where heels were nailed on by machine and where soles and heels were trimmed. Finally the shoes moved to the lower floor where they were washed, cleaned, and boxed. On this lower floor, machines also stamped out the soles. The company’s offices were on the first floor facing Front Street.

In 1894, when the description of the manufacturing process was written, there were between three and four hundred employees in the factory, although the article notes that there was capacity for 600 people. In 1913 the company employed 1,131 people in its Brooklyn factory (871 men,210 women, and 50 office workers). John Hanan also owned shoe companies in other cities and served as president of the National Boot and Shoe Manufacturers’ Association. He was also the founder of the United Shoe Machinery Corporation, which manufactured machines for use in show factories. After John Hanan’s death, the firm was taken over by his sons Herbert Wilmer Hanan (1872-1933) and Addison Garthwaite Hanan (1876-1923) and grandson Robert Wilmer Hanan (1903-1933). The company went bankrupt in 1935. Old signs extant on the building in 2000 recorded some of the complex’s later occupants: Starlite Lamp Shade Company, Fashion Decor Lamp Shade Company, Washington Garter Corporation, National Leather Manufacturing Company, Gotham Furniture Frame Company, Modern Box Company, Star Fastener Company, Embassy Archives Center, Melcon Design Company, Shaw Television Corporation, Deluxe Novelty Company (DLX Industries), and Latex Specialties.

The simple brick facade, articulated by large segmental openings, simple brick piers, and corbelled cornice, marks 54 Bridge Street as a significant example of transition from the American Round Arch style to the daylight factory. This, together with its slow-burning mill construction, makes it representative of American factory architecture of this period and contributes to the architectural and historical character of the DUMBO Historic District. Built in 1893, during a major period of development when manufacturers such as Hanan & Son were making DUMBO into one of the city’s most important industrial neighborhoods, the structure contributes to the district through its architecture, structure, and the fact that its owners played a significant role in the area’s history.

- From the 2007 NYCLPC Historic District Designation Report

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

These salt lamps come in special shapes, including book salt lamp, cone salt lamp, bamboo wall salt lamp, boot salt lamp and many more. To carve these lamps, first a block of required size is cut from the raw lumps of salt rock, and then a hole is drilled to accommodate the bulb. Duly drilled block then passed over to Machinist who carves the desire shape on the machine. Once finished, the lamp is then fixed with a wooden or onyx base then plastic shrink wrapped and manufacturing process is completed.

We do make custom shapes and designs according to given diagrams, not every design is possible to Craft on the Rock Salt, but we can try to make one of your choice. Any kind of logo or name or diagram in shape of flower or any special characters can be carved on salt

Size: small, large and usb

Colors: Red, Reddish Orange, pink and white salt

Base Polished Wood, marble and Onyx and plastic in usb

Cable: 110,220 volt with on off switch or usb port cable

Packing: shrink wrapping on each lamp ,air bubble packing, 4 ply inner, 7 ply master cartoon

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/

Paul Ohodnicki, Kevin Byerly - Materials Processing & Power Electronics

NETL fabricates advanced prototype magnetic material components, including inductors, transformers, motors, and sensors, to support multiple NETL research areas in sensors, fuel cells, and electric grid modernization. This discussion will demonstrate varied fabrication equipment used for raw materials, such as amorphous metal ribbons fabricated by external partners and industry, to produce high-value components. Researchers are then able to test the components using specialized electromagnetic testing equipment in order to provide performance characteristics based on the real operating conditions. Further efforts to benchmark commercial magnetic core solutions against the lab's custom fabrication capabilities are continually investigated and reported on in the form of data sheets.

Materials Discovery & Development by Design for CO2 Capture and Advanced Sensors

Advanced energy systems require affordable cutting-edge materials than can withstand high-pressure, high-temperature, corrosive or otherwise harsh service environments. In this laboratory the development of novel, cost effective materials and devices for use in sensing of fossil energy systems to provide cleaner usage and production of fossil fuels will be discussed. The lab places an emphasis on new sensor material technologies integrated with advanced sensing device platforms to allow for operation under harsh environments and enhanced sensor device functionality. Embedded sensors are under development for applications such as monitoring of CO2 migration and groundwater impacts for CO2 sequestration, corrosion monitoring in wellbores and natural gas pipelines, and in situ process control in high-temperature power generation systems such as Solid Oxide Fuel Cells (SOFCs), gas turbines, and combustion systems. The laboratory capabilities are also relevant for other high priority emerging needs within DOE including the Grid Modernization Laboratory Consortium as well as process monitoring and control for advanced manufacturing processes.

A beautiful Prim Sport "Igen" 38 being rebuilt in the watch restoration and assembly room 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!

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.

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.

Photo of an Intel 40486 microprocessor circuit on a silicon wafer, part way through the manufacturing process.

Museu del Disseny / Design Museum Barcelona, Spain

The Museu del Disseny de Barcelona brings together, under one roof, the collections of the Museu de les Arts Decoratives, the Museu de Ceràmica, the Museu Tèxtil i d'Indumentària and the Gabinet de les Arts Gràfiques, to showcase its vast heritage of more than 70,000 objects.

The Museu del Disseny is based on a common theme «From the decorative arts to design», and is dedicated to the culture of the object, focusing on pieces that are often from the everyday sphere, their design, manufacturing process, use and distribution, aesthetic and functional obsolescence, all from a 21st-century perspective.

The Disseny Hub Barcelona building was designed by MBM architects. The building comprises two parts: an underground section made possible by the change in level caused by the redevelopment of the square; and a block at street level, which cantilevers out towards the Plaça de les Glòries, 14.5 metres above the ground. This block houses the venues for long- and short-term temporary exhibitions, as well as a hall for events and a large auditorium. Most of the building's floor space is located below this level and houses key areas such as the main exhibition gallery, the documentation centre, research rooms, the bar and restaurant and the shop. The entire project complies with high environmental quality and sustainability standards which are achieved through a large-scale, self-sufficient energy system.

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

A selection of our hair accessories made from fabrics rescued from the manufacturing process, sold at Sydney's Paddington Markets.

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!

4689 Confederate Powder Works Chimney, 1717 Goodrich St., Augusta, Richmond, GA. April 19, 2011. Decimal degrees: 33.486746, -81.992356

"The Confederate States Powder Works"

"...the best powder in the world ..."

"Georgia Civil War Heritage Trails"

"When the conflict began in April 1861, leader on both sides were unprepared to wage a long war. The Confederacy's industrial capacity was especially lacking, and munitions of all types were scare. Initial stores of gunpowder were inadequate, and attempts to overcome these deficiencies by existing powder mills or blockade runners proved costly, unreliable, and dangerous. Confederate President Jefferson Davis assigned Colonel George Washington Rains the task of constructing and operating a gunpowder factory. Reaching for two miles along the banks of the Augusta Canal, the Confederate States Powder Works produced much for Confederate armies from April 1862 until the war's end three years later.

On July 20, 1861, Rains examined the old United States Arsenal site along the banks of the Augusta Canal, one-half mile from the western city limit of Augusta. According to Rains, " Augusta was selected, for several reasons: for its central position; for its canal transportation and water-power; for its railroad facilities; and for its security from attack-since the loss of the works would have been followed by disastrous consequences." But at first he was hampered by a lack of detailed plans or experienced personnel.

With assistance from powder maker Frederick Wright, engineer and architect C. Shaler Smith, and master mechanic William Pendleton, Rains oversaw construction, beginning on September 13, 1861. The Powder Works complex was designed for manufacturing efficiency and safety. Thirteen major brick buildings and nearly twenty wooden structures were arranged in order of manufacturing process. Raw materials entered at one end of the Powder Works and finished gunpowder exited the other. Granite from Georgia's Stone Mountain, five million locally produced bricks, and machinery from throughout the Confederacy were assembled. Most visually remarkable were the battlemented Refinery with its 153-foot-tall smokestack and the Laboratory with its unfinished clock tower.

Gunpowder production commenced on April 10, 1862, and continued almost uninterrupted until April 29, 1865. Working only during daylight and overcoming four explosions plus shortages of raw material and labor, the facility produced some three million pounds of the best quality gunpowder. Jefferson Davis later noted, "it is but a just tribute to say that, beginning without even instructed workmen, he [Colonel Rains] had before the close of the war made what, in the opinion of competent judges, has been pronounced to be the best powder mill in the world..."

The approach of Union Major General William T. Sherman's army in late November 1864 prompted Rains to consider moving at least some of the Powder Works machinery to safety. But Sherman bypassed Augusta while production continued to the end of the war. After the war the Powder Works declined into ruin. The city of Augusta acquired tracts of land from the federal government in 1871 and 1872. An enlargement of the canal, begun in 1872, compelled the razing of remaining Powder Works structures, with the exception of the Refinery smokestack. At the request of Rains, it was left standing as a monument to the fallen heroes of the Confederacy. "

Under first column photo:

"Colonel George Washington Rains, Courtesy of the Augusta Museum of History"

Under second column photo:

"View from the north, circa 1865, Courtesy of the Augusta Museum of History"

Under third column map

"The Confederate States Powder Works complex, Courtesy of Michael C. White"

Photo by Rebecca Bolte, All Rights Reserved (c) 2010, www.rebeccabolte.com

Name: Doh Driver

Age: 40

Neighborhood: North Seattle

Vegan Circa: 2001

Why I Find Her Interesting: She is one of the co-owners of the most beloved Wayward Vegan Cafe. But more importantly, you won't meet anyone more knowledgeable or passionate about vegan products than Doh. She knows every ingredient, history, maker, and manufacturing process you can imagine. Why? She has to make sure everything at Sidecar is 100% vegan. She also manages to wrangle ~20 volunteers (without being able to pay or fire them); and she does it with charm, humor, and patience. She also used to teach Sivananda yoga, worked in restaurants for 10 years, worked in record stores for 8 years, and studied International Development, Women's Studies, and Spanish. Plus she has a rad name. Am I right?

Why Vegan: "After 11 years as a vegetarian, it dawned on me one day that I might as well go vegan. I was hardly eating any diary products or eggs at that point; I realized I was nearly there, so ... why not? It was just logical. There was no "a-ha" moment, and I hadn't learned anything new that convinced me. Only after I went vegan did I find out just how horrendous the dairy and egg industries were, as well as all the other reasons to go vegan." - Doh Driver

Spends Time:

-Doing "non-profit" work as one of the owners of Wayward Vegan Cafe. (That's a joke, it's theoretically a for-profit business.)

-As the full-time manager the all-vegan store, Sidecar for Pigs Peace, which is owned by Pigs Peace Sanctuary. She says she is ridiculously happy there because she is able to promote veganism and help make it accessible, She loves helping her consistently awesome customers. (Sounds like a dream job, but I've seen her work, it is HARD).

-Staying involved with her son's school. (He is 11 and has been vegan his whole life).

-Helping other parents put the principles of Positive Discipline into practice in their lives, via a listserv.

-She has also volunteered as a rape crisis counselor, and a meal-delivery service for AIDS patients.

Doh Suggests: that we all support vegan businesses!

If you see Doh on the street: talk to her about rescued greyhounds, or vitamin D deficiency.

Get to know Doh better by coming into Sidecar during the week day hours (10a-5p), or by becoming fans of Sidecar and Wayward on Facebook.

Delvendahl Martin Architects’ installation for Moss Bross explores the possibilities of the windows by distorting the perception of depth and perspective as viewed from the street. This is achieved by using hundreds of cotton strings to stitch the edges of the window space to form a series of seemingly floating voids, where the three main strands of Moss Bros products arebe displayed. The material expression of the cotton strings recall the raw materials of garments, the loom-based manufacturing process of cloth, and the craftsmanship of the Moss Bespoke service.

Photography (c) Agnese Sanvito

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/

By renowned architect James Salmon Jr. (Salmon, Son and Gillespie), 1904-7. Glasgow Style Art Nouveau. Tall, 8-storey commercial building with shop at ground floor. Reinforced concrete construction. Casement windows with small-pane glazing. 1st floor cill band. Sculpted panel between 1st and 2nd floors: THE LION CHAMBERS. Square canted section in southmost bay rising from 1st to 4th floor corbelled out on sculpted judges heads at 4th floor; wide semi-circular keyblocked window at 6th floor surmounted by pedimented gable. Canted corner bay slightly advanced over 4th floor and surmounted by octagonal cupola. Southern return: simple fenestration and pedimented gable. Return to Bath Lane: canted return bays with metal casements.

Built for lawyer/writer William George Black. This explains the sculpted judges heads. Black was well-established within the Glasgow Art Club and provided artists studios into his plans for the upper floors of the building. The building is the second reinforced concrete structure in Glasgow and amongst the first few in Britain.

The building was built using the Hennebique system by French Engineer, François Hennebique. This system involves reinforced concrete instead of steel frames, making the building fireproof. The Hennebique system was designed to strengthen concrete to make it withstand forces which damage concrete the most. This allows the walls to be extremely thin with a thickness of only 100mm. However, the Hennebique system does have negative attributes, including the complexity of the framework and moulding in the manufacturing process. The concrete can weather away easily, considerably in weather in the United Kingdom, which was one of the main reasons the Lion Chambers has had to be abandoned.

Sadly this important building is on the Buildings at Risk register listed “critical” with the owners, having been served with a Dangerous Building Notice, wanting to demolish it. Only it’s A-listed status saving it. Remedial repairs were estimated at £1-1.5 million back in 1991 when occupants of the building were evacuated following fears of collapse. Money has been raised to cover parts of the building with mesh after lumps were spotted falling off it.

i was a little disturbed reading this part of our gas fireplace's manual. "When lit for the first time, the appliance will emit a slight odor for an hour or two. This is due to the "curing" of the logs and "burn-off" of internal paints and lubricants used in the manufacturing process."

Dolby's Flint Mill, sits beside the Trent and Mersey Canal in Lytton Street, Stoke. A part of our old pottery manufacturing process, flint was ground and heated in kilns to provide a major ingredient in the clay with which earthenware pottery was produced.