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From start (manufacturing process) to finish (bottles will decompose in 6 months in a land fill) so, you can be clean AND green.
On Scene with Watertown Volunteer with a smoky structure fire at 20 McLennan Dr in the Oakville section of town. First due crews found heavy smoke coming from Quality Automatics Inc ,a machine shop located at that address. Crews immediately stretched lines and hit the hydrant at the end of the dead end street for an additional water source. Extension ladders were used to access the roof for ventilation since powerlines prevented the aerial ladders from being used. The fire was brought under control after approximately 30 minutes but required extensive overhaul and ventilation. In addition hazmat precautions had to be taken due to the lubricants and by products of the manufacturing process at the business were mixed with the water and foam used to extinguish the blaze.
Picture taken at night of the Cadbury factory at Bournville, I'm not really sure how the water is used in the chocolate manufacturing process...
At the Cup Noodles Museum, you can learn the secret of cup noodle and even have the opportunity to make one-of-a-kind ramen yourself.
Japanese food company Nissin operates this unique museum for Ramen.
The museum shows the 40 year product history as well as the founder, Mr. Ando Momofuku's creativity, by exhibiting 3,000 kinds of cup noodle packages.
They also recreate Mr. Ando Momofuku's humble research facility.
At "My Cup Noodle Factory," you can make your own cup noodle out of 5,460 soup base / topping combinations.
There is also "Cup Noodles Park", a playground for kids where they can experience the manufacturing process of Cup Noodle.
There is a "Chicken Ramen Factory" where you can make Chicken Ramen by hand, starting with kneading, spreading, and steaming the wheat flour and then drying it with the hot oil drying method. After experiencing the process that led to the invention of the world's first instant ramen, you can take your freshly made ramen with you and enjoy its delicious taste at home.
And of course you can enjoy global varieties of noodles in the contemporarily designed museum restaurant!
www.lcrapid.com/aluminum-extrusion/
ALUMINUM EXTRUSION SERVICE
LC Rapid aluminum extrusion service offers high quality, cost effective extrusion parts. With our professional and experienced engineering team and advanced machines, we not only make excellent tools but we also offer complex extruded parts as a manufacturer of aluminum extrusions. You can be rest assured because we exercise strict quality control through the whole manufacturing process guided by high quality standards of aluminium extrusion technology. Regular testing and verifying at various stages of manufacturing ensure us deliver an extraordinary quality product every time.
Aluminium Extrusion Technology
Aluminum extrusion is the process of forming the aluminum into the desired shape and geometry. Firstly, the mold is fabricated according to the drawing. And then extrude different types of custom aluminum extrusion profiles from the mold by heating and forcing the aluminum billet through the die.
Aluminum extrusions are known for their great strength, lightweight, and good conductivity, which make them an outstanding choice for diverse end-use applications (e.g. enclosures and heat sinks). It is the most cost-effective for high-volume production runs of metal parts due to the significantly low unit price.
Advantages of Custom Aluminium Extrusion
Part ProductionPart Production
Piece price is significantly lower with standard aluminium extrusion services versus other metal forming process.
StrengthStrength
Fabricated aluminium extrusions are very strong, making them suitable for cold weather applications that require high strength. Aluminum extrusions also have high rust and corrosion resistance.
Finishes SelectionFinishes Selection
Aluminum extrusions can be anodized, powder coated, polished, and etc.
PrecisionPrecision
We can conform to very tight tolerances base on customers requirements.
Aluminum Extrusion Process
After we receive your order, we will:
Step 1: Supply a complete cross-sectional drawing for you after review and discuss about your CAD files.
Step 2: Fabricate dies and extrude a sample to get your approval.
Step 3: Make the modification on the die if needed.
Step 4: Exercise process control when extruding your parts.
Step 5: Select from a variety of finishes processing to achieve the effect you want.
Step 6: Inspect finished extruded parts to avoid any dimension deviation.
Aluminum Extrusion Tolerance
The tolerance depends on shape and structure. If you need a very precise tolerance, we can follow it once we confirm your designs.
Aluminum Extrusion Material
Alloy: 6060, 6063, 6061, 6082, 2A12, 2024, 5052, 7075 and etc. (Others Available)
Aluminum Extrusion Finishes
Electrophoresis
After applying electrophoresis, you can get a glossy surface with excellent impact resistance. The electrophoresis layer improves the resistance to chipping, scratching, and fading.
Powder Coating
Typically, powder coating is commonly used on the market to color the aluminum extrusions. It is also applied to cover extrusion lines and defects.
Anodizing
Anodizing is done to improve the corrosion and wear resistance, enhancing the parts durability. Sometimes anodizing is done simply get colors on surfaces, like black, red, blue, gold, and etc.
Aluminum Extrusion Solutions
Solar Energy
Aluminum extrusion is transforming the solar energy industry with its extraordinary physical properties such as strength, malleability, lightweight, and high corrosion resistance. Aluminum is considered to be the preferred state-of-the-art frames and structures for the solar panels, supports and connectors.
Automotive
Aluminum is approximately one-third the weight of steel, but with the similar strength with steel. Aluminum extrusion is helping car makers to reduce vehicle weight precision, create innovative parts. Its quality and mass production technologies have been proven by their actual applications such as bumper beam, motor mount, frame members and other automobile parts.
Electronics
The custom aluminum extrusion has standout durability, high corrosion resistance, weatherproof long-lasting property, which is why there are so many electronics applications made by extrusion, including housings, heat sinks, connectors.
Common Applications of Aluminum Extrusion Technology
Heat Sink
The extruded heat sink is the most commonly used type of heat sinks in the market. The extrusion process makes it cost effectiveness, high quality and excellent thermal conductivity.
Aluminium Profile
Aluminum profile is used in a wide range of applications due to it’s strong tensile strength, flexibility, and durability.
Cylinder Tube
Aluminum cylinder tubes are playing a significant role in various industry sectors.
We, Ashwin Plastics, initiated our momentous lifework as producers and suppliers of plastic packaging products such as Laminated Pouches, Laminated Rolls, BOPP bags, BOPP rolls, HM bags and Rolls, PP Bags and Rolls etc. Offer diverse range of packaging products to meet varied requirements. Follow high quality parameters in business operation, manufacturing process and client servicing. Very particular about not using plastics and laminates that are safe and non-hazardous
The Manufacturing Process Workshop:
You'll work with a team to invent a process for wrapping candy and getting it to its final destination, then go head-to-head with other teams to see whose process is the fastest and best quality. Along the way, you'll learn all about the fundamentals of industrial operations engineering including continuous improvement, quality control, and more.
Thursday session 2
Photo: Jessica Knedgen
MconneX
The Report Titled on “Global Cheese Market Size, Status and Forecast 2019-2024” firstly introduced the Cheese basics: Definitions, Classifications, Applications and Market Overview; product specifications; manufacturing processes; cost structures, raw materials and so on. The Cheese Market also provide assessment of market definition along with the identification of topmost prominent key manufactures ( Arla Foods, Bongrain, Devondale Murray Goulburn, Fonterra, Leprino Foods, Friesland Campina, Groupe Lactalis, Almarai, Calabro Cheese Corporation, Bega Cheese, Bletsoe Cheese, Brunkow Cheese Factory, Burnett Dairy, Cady Cheese Factory, Dupont Cheese, Emmi, Hook’S Cheese Company, Kraft, Mother Dairy, Parag Milk Foods, Saputo, Sargento Foods, Beijing Sanyuan, Yili, Mengniu Dairy, Bright Dairy, Inner Mongolia Licheng, Knight Dairy, Shandong Tianjiao Biotech) are analyzed emphatically by competitive landscape contrast, with respect to Price, Sales, Capacity, Import, Export, Cheese Market Size, Consumption, Gross, Gross Margin, Revenue and Market Share. Quantitative analysis of the Cheese industry from 2014 to 2019 by Region, Type, Application and Consumption assessment by regions.
Raj Process Equipments And Systems Pvt. Ltd. We offer a wide
range of Zero Liquid Discharge Plants in India which are used in wide number of chemical industries.
To know more about Zero Liquid Discharge Plants in India please visit ww.raj-turnkey.com.
130912-N-PM781-004
MARINETTE, Wis. (Sept. 12, 2013) Secretary of the Navy (SECNAV) Ray Mabus delivers remarks to shipyard workers at Marinette Marine Corporation shipyard. During his visit Mabus also toured the facilities and received an update on the Freedom-variant littoral combat ship and its manufacturing process. (U.S. Navy photo by Mass Communication Specialist 1st Class Arif Patani/Released)
By Rebecca Junkin
Widespread reliance on artificial intelligence, a common theme in speculative fiction, is closer than many might believe. This rather macabre image - acrylic paint on canvas which has been scanned and photoshopped - depicts an automated manufacturing process for synthetic faces believed to be inert until integration.
At the Cup Noodles Museum, you can learn the secret of cup noodle and even have the opportunity to make one-of-a-kind ramen yourself.
Japanese food company Nissin operates this unique museum for Ramen.
The museum shows the 40 year product history as well as the founder, Mr. Ando Momofuku's creativity, by exhibiting 3,000 kinds of cup noodle packages.
They also recreate Mr. Ando Momofuku's humble research facility.
At "My Cup Noodle Factory," you can make your own cup noodle out of 5,460 soup base / topping combinations.
There is also "Cup Noodles Park", a playground for kids where they can experience the manufacturing process of Cup Noodle.
There is a "Chicken Ramen Factory" where you can make Chicken Ramen by hand, starting with kneading, spreading, and steaming the wheat flour and then drying it with the hot oil drying method. After experiencing the process that led to the invention of the world's first instant ramen, you can take your freshly made ramen with you and enjoy its delicious taste at home.
And of course you can enjoy global varieties of noodles in the contemporarily designed museum restaurant!
Ah, the trusty old dremel. Well, it is more accurate to call it a die grinder or rotary tool, as Dremel is the brand name of the ubiquitous workshop tool - kinda like how we all call what is identified as an ice box "Esky".
Yes, things were done by hand in the old days with the files and sandpapers and whatnot, but the introduction of the dremel has made things so much faster.
It can use a number of attachments for the speedy removal of material:
Works as a mini sander, angle grinder, rotary cutter, buffing wheel, etc.
Its most useful function for us so far is reshaping lug shorelines and getting a bit of extra wiggle room in lug ports for a good fitup of tubing.
For example, while tubing diameters are a set size and lugs are generally made to these dimensions, the manufacturing process often will have small variances in the inner diameter of the lug ports.
It would take an incredibly long time to sand or file away the inner diameter by hand and remove any meaningful amount of material. With a dremel and sanding drum, the job is done in a number of minutes.
Recent applications for this included Quang cleaning out the bottom bracket chain stay ports of old filler material to properly fit up the replacement chain stays for the Kenevans' repair, and Minh removing excess filler from a scalloped seat stay cap with a cone-shaped grinding stone.
Of course, for applications like these, the margin for error is quite large unless the user is heavy handed and takes off too much material in one go.
But for more intricate uses such as reshaping lug shapes and shorelines, more care is required as material is removed incredibly quickly.
Juices in aseptic packaging are basically used to quench the thirst and to get refreshment. These are used in canteens, hotels, restaurants, homes and also in marriages, birthday parties,and all types of functions.Soft drinks include all drinks made from water or mineral water, sugar, aromas, and essences, and usually contain carbon dioxide. Other beverage products such as flavored water, sports, and energy drinks, and ice teas use a similar manufacturing process.Retail Marketing offer you a Juices Soups Soft Drinks Marketing. From so many real juice flavors and a lot of other brands.
The thing I love about scarves like these? This is screen printing. Every color you see here is another run through the screen printer. As manufacturing processes go, this is insane.
Click To Get Cheap Sleep Innovations 8-inch Sure Temp Memory Foam Mattress - King Size $$$$ Maybe if you are looking for the review on Sleep Innovations 8-inch Sure Temp Memory Foam Mattress - King Size at inexpensive price, We have found a good deal and prices for this product on Amazon. Get it today!. Let's see the product description. The Sleep Innovations 8-Inch SureTemp mattress provides premium memory foam comfort and therapeutic benefits at a great value. Rest in comfort on this deep and responsive 8-inch memory foam mattress. 2-inch premium top layer of Sure Temp memory foam provides all the benefits of traditional memory foam with the added benefit of a neutral temperature sleep surface. This unique, patented formulation and manufacturing process offers improved airflow for a cooler night's sleep. 6-inch base layer of high quality foam provides a supportive sleep surface that disperses your weight evenly. Mattress measures 80-inch long by 76-inch wide by 8-inch high.. Where to buy this Sleep Innovations 8-inch Sure Temp Memory Foam Mattress - King Size? Special Offer, Click Here! www.amazon.com/gp/product/B003CT37I8/ref=as_li_ss_...
Governor Kay Ivey participated in the Grand Opening of Winkelmann Flowform Technology, LP. Thursday October 3, 2019 in Auburn, Ala. Winkelmann Flowform Technology, LP. specializes in high-precision, high-strength, thin wall roto-symmetrical parts from metals such as titanium and steel. Through technical engineering and in-house manufacturing processes, the company seeks to provide high-quality, precise, near net shape designs for use in the Aerospace and defense industries. The project involves the creation of 50 new jobs and a $12 million investment in the Auburn metal forming operation. (Governor's Office/Hal Yeager)
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.
On Scene with Watertown Volunteer with a smoky structure fire at 20 McLennan Dr in the Oakville section of town. First due crews found heavy smoke coming from Quality Automatics Inc ,a machine shop located at that address. Crews immediately stretched lines and hit the hydrant at the end of the dead end street for an additional water source. Extension ladders were used to access the roof for ventilation since powerlines prevented the aerial ladders from being used. The fire was brought under control after approximately 30 minutes but required extensive overhaul and ventilation. In addition hazmat precautions had to be taken due to the lubricants and by products of the manufacturing process at the business were mixed with the water and foam used to extinguish the blaze.
The PRIVILEGE 745 inherits historic know how and the best manufacturing process The Privilege 745 exceeds previous benchmarks in terms of space and style It has the largest sail area, the biggest interior volume and the most expansive owner’s suite of the Privilege range Owners feel the opulence of the 745 when stepping aboard… to enjoying the highest quality woodwork to immersing themselves in spacious elegance confirms Privileges well known stamp of excellence The generous interior of the 745 with expansive passageways, built in equipment, separate living areas, subtle lines and a carefully considered floor plan create a highly functional and eminently elegant interior The huge saloon is gently bathed in light from an expanse of panoramic windows The master suite is most impressive with a large king sized center lined bed and a private ensuite furnished with a luxurious full size Jacuzzi tub and resort style amenities And guests are far from jealous as each have VIP suites royalty would envy Contact Privilege to locate your exclusive North American Dealer
Cricket Batting Gloves that meets international standards are manufactured by HIKE INTERNATIONAL also called the name of HIKE, HIKCO. We are a professionally managed business house bringing wide assortment of leather batting gloves, PU battering Gloves and also PVC Batting Gloves. And they all are prepared from the best quality raw material. We are one of the foremost batting gloves manufacturers and suppliers, incepted in India. We strictly accentuate on the top quality raw material in the entire manufacturing process which is sourced from noted suppliers throughout the world. HIKE INTERNATIONAL are leading manufacturer, suppliers and exporters in India.
“ASHTON-IN-MAKERFIELD LOCAL BOARD. TO CONTRACTORS.- The Gas and Water Committee of this Board are prepared to receive TENDERS for the EXCAVATION and the BRICK and STONEWORK necessary for the construction of a GASHOLDER TANK, 58 feet in diameter, at their Gas Works, Ashton-in-Makerfield.
Plans and Specifications of the work can be seen on application to Mr Wm GOLDWORTH, Prescot, Engineer to the Board, or to me, the undersigned.
Sealed and endorsed Tenders to be sent in to me not later than Monday, May 14th. The lowest or any Tender not necessarily accepted.
JOHN E FAIRLESS,
Clerk to the Board.
Ashton-in-Makerfield,
May 2nd, 1877.”
A basic gas-holder, consisting of an inverted container with the open end partially submerged in a tank of water, was invented by the French chemist Antoine Lavoisier in 1782. His design met the twin requirements for, firstly, a facility for storing a quantity of gas against unexpected surges in demand and/or interruptions to the manufacturing process and, secondly, a means of pressurising the gas so that it could be delivered to the consumer via a network of mains and pipes. The water in the base tank formed an air-tight seal which prevented the gas from escaping except through a valve-controlled outlet. Pressure was provided by the weight of the container itself, which sank down into the water as the volume of gas reduced. In some designs the rise and fall of the container was assisted by counterweights hidden in vertical support columns. A telescopic holder, whereby storage capacity could be doubled, tripled etc depending on the number of lifts, was first devised by Samuel Clegg in 1817 and pioneered at Leeds in 1826.
On taking possession of the Ashton-in-Makerfield Gas Consumers' Company works in 1875 the Local Board inherited a single gasholder with a storage capacity of just 17,000 cubic feet (cf). A report by the works manager in January 1877 contrasted this with the then daily demand for 18,000-22,000 cf of gas during the winter months, and drew attention to the problems that would occur if the manufacturing process was disrupted in any way (Wigan Observer & District Advertiser, 9 February 1877).
In 1878, after a long delay caused by various setbacks including leakage from the base tank, a new holder was installed by J & W Horton of Smethwick, Birmingham, at a cost to the Local Board of £645 (Wigan Observer & District Advertiser, April 1877-June 1878). The holder was still in situ in 1938 but, evidently, had been decommissioned some years earlier and was then ordered to be dismantled and sold as scrap. No plans or photographs have survived, but the reference in 1938 to “cast iron column guides” suggests that it was of the telescopic variety.
This leather case has been handmade by our experienced leather craftsmen in high quality cowskin , it has passed strict quality controls during the whole manufacturing process.
- Magnets system closure.
- Sync through travel cable.
- 1 document compartment.
- Soft Leather Lining.
- ABS inserted protection.
Universal Trailer Corporation Plant Opening Event on March 24, 2017 in Bristol, Indiana. On Friday, March 24, 2017, the Ribbon Cutting Celebration for Universal Trailer Corporation new $25 million, 200,000 sq. feet advanced technology cargo trailer manufacturing facility was held in Bristol, Indiana. The plant is located on 43 acres at the corner of C.R. 4 and Blakesley Parkway (C.R. 29), a half mile east of S.R. 15 on C.R. 4 north of the Indiana Toll Road. 200 new hires are expected over the next 18 months. The plant has new, automotive-style robotic manufacturing capabilities unheard of in the cargo trailer industry. Trailer “kits” will be manufactured here for other Universal Trailer plants across the country. The Plant is designed to be employee-friendly with an emphasis on employee empowerment to assure an efficient and quality manufacturing process. Plant tours were also held. With its innovative engineering and worker empowerment, the location of this new trailer technology in Elkhart County was the result of many public and private entities working together to provide such assistance as annexation for municipal services, tax incentives and industrial revenue bonds, among other aid. Just the Facts: Speakers: Jeff Howes, Universal VP Marketing; Universal CEO & President, Terry Carlson. Op Mgr. Keith Shockey; Indiana EDC President, Elaine Bedel; State Senator Blake Doriot; Elkhart Co. Commissioner, Suzie Weirick; Bristol Town Council President, Ron Norman; Unable to attend, 2nd Dist. Congresswoman, Jackie Walorski, sent a video of congratulations.
Ball mill is an efficient tool in wall putty manufacturing process in small plant. There are two ways of grinding: the dry way and the wet way. To use the ball mill, the material to be ground is loaded into the Neoprene barrel that contains grinding media. As the barrel rotates, the material is crushed between the individual pieces of grinding media that mix and crush the product into fine powder over a period of several hours.
skype: anna.smith20121
Email: shcrusherdhy@gmail.com
The Trackside Beer Garden at Kulshan Brewing in Bellingham, Washington.
These rusty old tanks are digesters that were once used by the Georgia-Pacific Corp. pulp and paper mill to turn wood chips into pulp, using acid and steam. They're 65-feet-tall, 18 feet in diameter at their widest point, and are made from 1.3-inch-thick steel, joined together with large rivets.
The tiled tanks in the background were once filled with bleach used in the tiolet paper manufacturing process back when Georgia Pacific operated a paper mill on this site.
They're pouring beer in those re-purposed shipping containers.
I used a KITE to fly the camera.
On Scene with Watertown Volunteer with a smoky structure fire at 20 McLennan Dr in the Oakville section of town. First due crews found heavy smoke coming from Quality Automatics Inc ,a machine shop located at that address. Crews immediately stretched lines and hit the hydrant at the end of the dead end street for an additional water source. Extension ladders were used to access the roof for ventilation since powerlines prevented the aerial ladders from being used. The fire was brought under control after approximately 30 minutes but required extensive overhaul and ventilation. In addition hazmat precautions had to be taken due to the lubricants and by products of the manufacturing process at the business were mixed with the water and foam used to extinguish the blaze.
Flak Culinair is run by Jan Van Achter, the third generation of a family committed to excellence. This modern marvel of technology that is Falk Culinair still inspects each piece by hand and eye to ensure quality. Jan affirms that, “The challenge of the new generation is to continue to manufacture the finest handcrafted cookware in the world.” We at Falk Culinair UK are pleased to share Jan’s passion and his family’s vision.
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.
TR King Poker Chip set and some angst from the election returns results in me measuring the thickness of this vintage chips. They have barely (or never) been used - but still don't travel well between some of the wooden trays I have - they are way too tight! Seems the manufacturing process was much less rigorous than what we see today.
Anyway - these are special and unique due to the stamp - and I think I know a LOT about where they came from as there was a receipt in the set, and some research shows that these were likely belonging to Francis O. Drummond of Los Angeles and Palm Springs. Email me for details if interested
Universal Trailer Corporation Plant Opening Event on March 24, 2017 in Bristol, Indiana. On Friday, March 24, 2017, the Ribbon Cutting Celebration for Universal Trailer Corporation new $25 million, 200,000 sq. feet advanced technology cargo trailer manufacturing facility was held in Bristol, Indiana. The plant is located on 43 acres at the corner of C.R. 4 and Blakesley Parkway (C.R. 29), a half mile east of S.R. 15 on C.R. 4 north of the Indiana Toll Road. 200 new hires are expected over the next 18 months. The plant has new, automotive-style robotic manufacturing capabilities unheard of in the cargo trailer industry. Trailer “kits” will be manufactured here for other Universal Trailer plants across the country. The Plant is designed to be employee-friendly with an emphasis on employee empowerment to assure an efficient and quality manufacturing process. Plant tours were also held. With its innovative engineering and worker empowerment, the location of this new trailer technology in Elkhart County was the result of many public and private entities working together to provide such assistance as annexation for municipal services, tax incentives and industrial revenue bonds, among other aid. Just the Facts: Speakers: Jeff Howes, Universal VP Marketing; Universal CEO & President, Terry Carlson. Op Mgr. Keith Shockey; Indiana EDC President, Elaine Bedel; State Senator Blake Doriot; Elkhart Co. Commissioner, Suzie Weirick; Bristol Town Council President, Ron Norman; Unable to attend, 2nd Dist. Congresswoman, Jackie Walorski, sent a video of congratulations.
A material handling “masterpiece”! Ideal for confined areas
Onboard the lorry, on the loading bay, on the production floor, in small warehouses...
Works from ambient to cold store environments (down to -35°C).
500 hours between services.
An environmentally friendly product from an environmentally friendly manufacturing process.
Handling all types of load carriers.
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.
From the planting of the seed to the end of the manufacturing process, Portuguese cork makes for authentic, high quality and eco-efficient cork products that are created with true craftsmanship and care.
A Medical Device Master File is a submission to U.S. FDA that may be used in support of premarket submissions to provide confidential detailed information about establishments, processes, or articles used in the manufacturing, processing, packaging, and storing of one or more medical devices. Registrar Corp's team of medical device regulatory experts provides guidance as to required elements, formats, and particularities of Medical Device Master File submissions. For assistance submitting a Medical Device Master File, simply click the Medical Device Master File Certificate shown on the left.
Just after midnight Waterbury Fire received a call from the Brass Mill Mall Security Office reporting a fire in a commercial structure on East Main in the area of Wolcott St. Crews arrived to find heavy smoke showing from the building which housed Plasma Coat Inc at 785 East Main St. As fire fighters stretched lines Truck 1 and Truck 3 set up for operation. An additional call was made for Engine 5 to assist the first alarm assignment companies, specifically to feed Truck 3's operation. The stubborn and smoky fire was brought under control in about 50 minutes. Members of he City's Fire Marshal's Office responded to investigate the fire as well as the Connecticut Department of Protection to investigate and clean up any hazards from the manufacturing process that may have been released by the fire and suppression effort.
If you would like to see more fire scene photography visit my website onscenefirephoto.com
Ascent Heat Exchanger Copper Nickel Tube ♣ Top China Heat Exchanger Copper Nickel Tube Supplier
❤About Ascent Heat Exchanger Copper Nickel Tube：
We manufacture, process and sell heat exchanger copper nickel tubes of good quality and dependability you can rely on. Shop for other equally qualified tubes of heat exchanger copper alloy tube, coopper nickel tube, etc. at our website of ascentcopper.com. Save time and shop with the trusted brass tube manufacturer.
❤Description:
Applied vacuum melting technology, our tubes are of superior quality: stable chemical composition, precise dimensions, and clean, smooth and bright inner and outer surface. Good mechanical properties - free from defects such as blowholes, cracks, pin hole leaks etc.
❤Features:
* Good corrosion resistance, especially in sea water; * Suitable for high temperature service; * Applicable for condenser for ship, heat and water supply, chemical industry, desalinator etc.* Copper Alloy UNS Nos.C70600 and C71500 are seamless Copper Nickel Tubes of standard specifications for Water Desalting Plants.
OD Range:3mm to 70mm
Wall Range:0.2mm to 5mm
Shape:Seamless Tube
At the Cup Noodles Museum, you can learn the secret of cup noodle and even have the opportunity to make one-of-a-kind ramen yourself.
Japanese food company Nissin operates this unique museum for Ramen.
The museum shows the 40 year product history as well as the founder, Mr. Ando Momofuku's creativity, by exhibiting 3,000 kinds of cup noodle packages.
They also recreate Mr. Ando Momofuku's humble research facility.
At "My Cup Noodle Factory," you can make your own cup noodle out of 5,460 soup base / topping combinations.
There is also "Cup Noodles Park", a playground for kids where they can experience the manufacturing process of Cup Noodle.
There is a "Chicken Ramen Factory" where you can make Chicken Ramen by hand, starting with kneading, spreading, and steaming the wheat flour and then drying it with the hot oil drying method. After experiencing the process that led to the invention of the world's first instant ramen, you can take your freshly made ramen with you and enjoy its delicious taste at home.
And of course you can enjoy global varieties of noodles in the contemporarily designed museum restaurant!
Half-grain leather is processed and repaired by equipment in the manufacturing process to become half-grain, so it is called half-grain cowhide. It maintains the style of natural leather. The pores are flat and oval, arranged irregularly, and feel hard.
1/8 scale model of a 2 part skull ( Left side view of bottom part ) printed using the Fused Deposition Modeling (FDM) additive manufacturing process.
In 2005 we acquired the assets to Kriz-Kraft, a unique case design that allows our customers even more choices when selecting a case to fit their needs. Working exclusively with Stins, the owner, we learned his unique design and manufacturing processes for the Kriz-Kraft racks first-hand. Because A&S quality met his standards, he has trusted us to continue serving his clientele. Always innovating to meet our customers’ needs, we feel fortunate to be able to exclusively offer this line as another option to consider when selecting the best rack for you.
The PRIVILEGE 745 inherits historic know how and the best manufacturing process The Privilege 745 exceeds previous benchmarks in terms of space and style It has the largest sail area, the biggest interior volume and the most expansive owner’s suite of the Privilege range Owners feel the opulence of the 745 when stepping aboard… to enjoying the highest quality woodwork to immersing themselves in spacious elegance confirms Privileges well known stamp of excellence The generous interior of the 745 with expansive passageways, built in equipment, separate living areas, subtle lines and a carefully considered floor plan create a highly functional and eminently elegant interior The huge saloon is gently bathed in light from an expanse of panoramic windows The master suite is most impressive with a large king sized center lined bed and a private ensuite furnished with a luxurious full size Jacuzzi tub and resort style amenities And guests are far from jealous as each have VIP suites royalty would envy Contact Privilege to locate your exclusive North American Dealer
On Scene with Watertown Volunteer with a smoky structure fire at 20 McLennan Dr in the Oakville section of town. First due crews found heavy smoke coming from Quality Automatics Inc ,a machine shop located at that address. Crews immediately stretched lines and hit the hydrant at the end of the dead end street for an additional water source. Extension ladders were used to access the roof for ventilation since powerlines prevented the aerial ladders from being used. The fire was brought under control after approximately 30 minutes but required extensive overhaul and ventilation. In addition hazmat precautions had to be taken due to the lubricants and by products of the manufacturing process at the business were mixed with the water and foam used to extinguish the blaze.
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.
PCB CNC Router JCUT-6090
The most boring ting to do is to make the PCB. Though now most people give the boring affairs to the PCB factory, yet it is indeed too long to wait for about three days or a week. New inspiration for a design is usually given up because of the trouble. While a PCB making machine can finish making a piece of PCB only in a few minutes, which can let your inspiration instant come true.
Main features:
1. High efficiency: It merely needs a few minutes to make a piece of PCB.
2. Accuracy: The min error of numerical control drill hole less than 1mil (0.025mm).
3. Automatism and convenience: Simple software hardware installation, operate the manufacturing process by striking the function keys of operation system.
Main technical parameter:
Whole cast iron with linear rail(vacuum table and dust collector)
Machined surface: single/double
Worktable board: 600*900mm
Max. speed: 8000mm/min
Working speed: 0-4000mm/min
Working accuracy: 6 - 8mil
Least line diameter and least line spacing: 6 - 8mil
Drilling depth: 0.02 ~ 3mm
Drilling diameter: 0.4 ~ 3.175mm
Drilling holes: 40-100/min
Repeat Accuracy: 0.025mm
The least error of Data control drill less than 1mil (0.015mm)
Operation system: WIN2000/XP /VISTA
Means of communication: PCI
Function Request: Protel PCB document can be directly put in. (gerber)
Spindle speed: 24000rpm
Spindle power: 1500W
Power supply: AC210-240V
Volume: 1200*1200*1600mm
Gross: 300Kg
SHERA splendid plank, a stylish plank siding, is a unique composite of natural fibers bonded tightly in a high-grade silicate structure. This autoclaved wood-grain plank siding acquires impressive strength and immense durability during the manufacturing process, yet retains its flexibility and dimensional stability. It is an environmentally friendly product that contains absolutely NO asbestos fiber.
This iPhone 5 wallet has been handmade by our experienced leather craftsmen in first quality cowskin-crocodile.
It has passed strict quality controls during the whole manufacturing process.
- iPhone 5 cases with closure system by lapel.
- This iPhone 5 case allows you to sync the device through travel cable.
- These iPhone 5 cases have 3 credit card slots, 1 window for documents and 1 Money Pocket.