View allAll Photos Tagged Manufacturing_process
Io Aircraft - www.ioaircraft.com
Drew Blair
www.linkedin.com/in/drew-b-25485312/
io aircraft, phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air-Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, hypersonic plane, hypersonic aircraft, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, defense science, missile defense agency, aerospike,
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
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
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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!
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.
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!
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
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
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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.
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.
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"
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.
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.
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
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!
Mascots with complex shapes and textures like Bobo can be replicated with high detail thanks to modern inflatable manufacturing processes.
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!
Watch cases under manufacture - post polishing.
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!
During the assembly stage, Gestamp effectively combines components of all our different manufacturing processes using welding, clinching and adhesive technologies. Our body shops use the most advanced technologies for assembling complex parts.
Thai silk is produced from the cocoons of Thai silkworms. Thai weavers, mainly from the Khorat Plateau in the northeast region of Thailand, raise the caterpillars on a steady diet of mulberry leaves. Khorat is the center of the silk industry in Thailand and a steady supplier of rose Thai silk for many generations.
Today, Thai silk is famous for its special qualities produced through unparalleled manufacturing processes, bearing unique patterns and colors.
Hafted knife - "PALEO TOOLS: The kinds of tools used by the Paleoindians can tell us much about their way of life. Most of the tools surviving today are made of stone. Spear points, knives, drills, and scrapers are typical Paleoindian artifacts. They were used for a variety of tasks, including hunting and butchering animals, processing plants, and working raw materials to make other tools. Archaeological sites of the Paleoindians contain mostly chipped stone tools and waste flakes left from the manufacturing process. However it is almost certain that these people made wide use of other raw materials including bone, wood, ivory, and antler. Objects made of these materials do not preserve as well as stone and have likely decayed over the past 10,000 years. Springs, sinkholes and deep river beds offer good conditions for preserving organic materials because of their high mineral content and lack of oxygen. Fragments of bone, wood, and other plant remains will give clues to future archaeologists who research the skills that Paleoindians needed to survive in Ice Age Florida. " ~ Display at the Florida Museum of Natural History. (Photo 091712-013.jpg) Paleoindians section of the Division of Historical Resources - Florida Museum of History - Where I used to work - September 17, 2012: A Walk Down Memory Lane - revisiting College Town - Tallahassee, Florida. (c) 2012 - photography by Leaf McGowan, Thomas Baurley, Eadaoin Bineid - technogypsie.com. To purchase this photo or to obtain permission to use, go to www.technogypsie.com/photography/
"PALEOINDIANS: The earliest people who inhabited North America are called Paleoindians. They came to Florida during the end of the last Ice Age, at least 12,000 years ago. Their way of life lasted for about 2,500 years. Archaeologists have found few Paleoindian sites. If, as it seems likely, these early people lived along the coast of Florida, their settlements have been covered by the rising sea level. Compared to later Florida Indian cultures, Paleoindians lived in small, widely dispersed groups. Their artifacts are often found around outcrops of a flint-like rock called chert. Pieces of chert were chipped, or knapped, to make stone tools. Paleoindian artifacts are also found in springs, sinkholes and rivers that were probably ancient waterholes. These were important sources of fresh water in an otherwise dry landscape.
PALEO TIMELINE: 12,000 B.P. to 9,500 B.P. (Before present) - EARLY PALEO PERIOD: 12,000-10,000 BP - Simpson point on mammoth ivory foreshaft (circa 11,500 BP) - First evidence of people on the Florida peninsula, Paleoindians live a semi-nomadic life, hunt big game like mastadon, climate was drier than today, and sea level is more than 100 feet lower than today. - Bison antiguns skull with embedded spearpoint, Wacissa River (circa 11,000 BP).
LATE PALEO PERIOD: 10,000 to 9500 BP - stone bola weight (circa 10,000 BP) had most big game animals extinct, wetter climate prevails, sea level rises gradually, several new styles of stone points appear, like the side notched bolan point. " ~ Display in the Florida Museum of Natural History.
For more information visit:
Paleoindians: www.technogypsie.com/science/?p=939 (expected publication December 2012)
Tallahassee: www.technogypsie.com/reviews/?p=5093 (Expected publication November 2012)
Florida: www.technogypsie.com/reviews/?p=5079 (Expected Publication December 2012)
For travel tales, visit:
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.
Minton Tiles
The richly patterned and colored Minton tile floors are one of the most striking features of the extensions of the United States Capitol. They were first installed in 1856, when Thomas U. Walter was engaged in the design and construction of vast additions to the Capitol (1851-1865). For the floors in his extensions, Walter chose encaustic tile for its beauty, durability and sophistication.
•Artist: Minton, Hollins and Company
•Date: Installed in 1856
One striking example of the contrast between the interiors of the Old Capitol (finished in 1826) and the extensions (begun in 1851) may be seen in the differences in flooring materials. In the Old Capitol, stone pavers were used in corridors and other public spaces, such as the Rotunda and Crypt, while brick was used to floor committee rooms and offices. These materials, although durable and fireproof, would have looked plain and old-fashioned to the Victorian eye. In the mid-19th century, encaustic tile flooring was considered the most suitable and beautiful material for high-traffic areas. Unlike ordinary glazed tile, the pattern in encaustic tile is made of colored clays inlaid or imbedded in the clay ground. Because the color is part of the fabric of the encaustic tile, it will retain its beauty after years of wear. One observer noted:
“The indestructibility of tiles may be judged from the fact that the excavations at Pompeii have unearthed apartments where painted tiles are just as beautiful, the colors as fresh and bright as... when the fated city was in all its glory.”
Two types of tile were used at the U.S. Capitol: plain and inlaid encaustic tiles in a range of colors. Plain tiles were used as borders for the elaborate inlaid designs or to pave large corridor areas. They were available in seven colors: buff, red, black, drab, chocolate, light blue and white. Additional colors, such as cobalt blue, blue-gray, and light and dark green, appear in the inlaid encaustic tiles that form the elaborate centerpieces and architectural borders. They were made by “filling indentations in the unburnt tile with the desired colors and burning the whole together.”
The patterns and designs formed in the inlaid tiles were limited only by taste and imagination. They include geometric patterns such as the Greek key, guilloche, and basket weave; floral designs such as the fleur-de-lis; and figures such as dolphins and classical heads. Few of the patterns are repeated. Although most of the tiles are six-by-six-inch squares, some are round, triangular or pie-shaped. Approximately 1,000 different tile patterns are used in the corridors of the Capitol alone, and up to 100 different tiles may be needed to create a single design.
The original encaustic tiles in the Capitol extensions were manufactured at Stoke-upon-Trent in Staffordshire, England, by Minton, Hollins and Company. The firm’s patented tiles had won numerous gold medals at international exhibitions and were considered the best tiles made. In 1876, having seen Minton’s large display at the Centennial Exhibition in Philadelphia, one critic wrote, “Messr. Minton shone superior to all exhibits of the sort… and may be cited as showing the highest results in tile-pottery achieved by modern skill and research.”
Beginning in 1856, and continuing for five years, the tile was installed by the import firm of Miller and Coates of New York City. For the journey from New York to Washington, the tiles were packed in wooden casks weighing about 1100 pounds; each cask contained enough tiles to pave about 100 square feet. The cost of the tile ranged from $0.68 to $2.03 per square foot.
Thomas U. Walter had every reason to believe that the encaustic tile floors would last as long as his extensions stood. One visitor noted in 1859 that the tile floors vied with the beauty of marble and surpassed it in durability. While perhaps valid for other installations, however, this prediction proved overly optimistic for the Capitol Building. By 1924, the Minton tile was removed from the corridors in the first and second floors of the House Wing and replaced by “marble tile in patterns of a simple order.” In that day, marble was selected for its superior durability and because suitable replacement tile was difficult to find.
In the 1970s, however, a similar condition prompted a very different response. In 1972, a search was undertaken to determine a source of similar tiles in order to restore the original appearance of the building. Inquiries were made of all major American tile manufacturers, the American Ceramic Tile Manufacturers Association, and even Mexican and Spanish tile suppliers. Although the colors and designs could be reproduced relatively easily, the patterns would quickly wear because they would be applied to the surface. The “inlaid” feature of the encaustic tiles, i.e., the approximately 1/8-inch thickness of the pattern and color, is the characteristic that enables the Minton tiles to be walked upon for over 100 years without signs of wear. It was this technique that formed the basic difficulty of manufacture.
Finally, as a result of the Capitol’s needs becoming generally known, the Architect of the Capitol was placed in contact with H & R Johnson Tiles Ltd., located at Stoke-on-Trent, England. It was discovered that that firm was a successor company to the Minton Tile Co. and had even retained many of the original hand tools and forms in a private museum at the company’s manufacturing site.
Contact was then made with Mr. James Ellis, the Directing Architect of Ancient Monuments and Historic Buildings for the Crown. He had been trying for many years to establish a program for the replacement of the worn Minton tiles at the Houses of Parliament but had more or less given up the attempt because of H & R Johnson’s continued unwillingness to revive the encaustic tile process. However, the restoration work at the Arts and Industries Building of the Smithsonian Institution was in process at about the time the needs of the Capitol became known; it thus appeared that a market for such tiles was developing to the degree that the manufacturer began to reconsider its prior position. The company thus began the experiments that finally led to the present availability, after many decades, of the original Minton-type tiles.
Because the tiles in the Capitol are more decorative and have more complicated designs and color combinations than those in either the Houses of Parliament or the Smithsonian, those institutions were able to obtain replacement tiles sooner than the Capitol. The lessons learned in the manufacture of the simpler tiles served as a basis for filling the later needs.
Color photographs and full-sized drawings of the many required patterns were made and recorded, and many developmental submissions were made as the hand-made manufacturing process was re-developed. Finally, in 1986, the first acceptable tiles were delivered. The installation process was accomplished with modern cement adhesives and has yielded excellent results.
The program enabled the original tiles to be replaced with exact replicas. This project began on the first floor of the Senate wing, where the effects of 130 years of wear and tear were most noticeable. Replacement tile was closely scrutinized to ensure fidelity to the nineteenth-century originals. While difficult and slow, this process is the only fitting response to the history of the Capitol extensions, not only to restore the original beauty and elegance of these unique floors, but also to provide for their continuing attractiveness for the foreseeable future.
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/
Apparently the lid missed a step in the manufacturing process. The squirrel image is just a sticker, added, I assume, by an owner. The puzzle within is the scene at right, with cattle beside a mountain stream.
Xci Class A is an exterior wall insulation panel composed of a Class A rigid polyisocyanurate foam core laminated during the manufacturing process to embossed foil facers.
Hunter Xci polyiso products:
- Have the highest R-Value per inch of any insulation
- NFPA 285 TEST - Passed
- Energy Star approved
- Contribute toward LEED certification credits
- HCFC, CFC, zero ODP, and negligable GWP.
Project Contractor: Caslor Masonary
Sold Through: Thermal Foams
XCI Twitter: twitter.com/#!/HunterXCI
XCI Facebook: www.facebook.com/pages/Hunter-Xci-Exterior-Continuous-Ins...
View more: www.hunterxci.com/
At Sense Organics, we believe the clothing of babies and children should be cuddly, soft and kind to their skin. That's why we only use 100% organic cotton in our clothing ranges. Find out more about why buying organic for your kids just make sense. Visit www.sense-organics.com
We're proud to make clothing for our little ones that’s stylish, organic and fair trade — and for the past twenty years, we’ve been making organic baby and children's clothes affordable to all.
All our sustainable baby clothes start with 100% organic cotton and are certified fair trade. We avoid the harsh chemicals used in the traditional cotton manufacturing process and our organic baby and children's clothes are snuggly and soft. They’ll look and feel wonderful on the skin of your little bundle of joy!
These Lynx helicopters manouevered so close that at times they appeared to be touching. Possibly a cheap manufacturing process!! The pilots must have amazing confidence in one another. Seen at Bournemouth air show. 2012
The video captures Albion's Bradbury Line cold roll-forming manufacturing process. The West Bromwich facility houses Albion Sections' state of the art Bradbury line which was exported from the USA. Fitted in 2006, this £1million investment allows custom roll forming and an instant changeover. It can manufacture Sigma Purlins, Zed Purlin, Steel Purlins, Eaves Beams, Cee Sections, Mezzanine Floor channels, Side Rails, and Structural Steel Framing (SFS) - Stud and Track from S390 and S450 yield strength steel. Albion now supports numerous Steel Construction Markets, such as portal frames, steel framing and Modular Construction both for off site and on site assembly. Albion Sections are a part of the Sebden Steel Group.
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/
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!
W.A.S Benson Lamps and hollow ware
In 1880 having been taught the use of simple lathes and machinery by his uncle,
and encouraged by William Morris, William Arthur Smith Benson began metalwork production
in Fulham, London. As his business grew Benson closely followed developments in technology, mastering all the processes of casting, turning, folding and riveting many variations of interchangeable components. He opened a showroom in Bond Street in 1887 displaying
light fittings, fireplace accessories, plant stands and hollow-ware, in silver, copper, brass,
iron and polished steel, patenting many of his popular designs to protect them from the
array of sub-standard copies that flooded the market.
WAS Benson was at the forefront of electric installation in homes all over Britain, advising on suitable lighting schemes and installation. In 1893 he electrified Philip Webb’s latest architectural commission, Standen, near East Grinstead, Sussex, now owned by the National Trust.
His metalwork and lighting designs reached iconic status, sold in galleries throughout Europe,
and in 1896 when William Morris died it was Benson with a colleague who bought Morris & Co and ran it alongside his own company until he resigned in 1917.
Benson attracted much acclaim for his metalwork designs and manufacturing processes.
The Studio Magazine of Decorative Arts, The Magazine of Art, and Herman Muthesius in
Das Englische Haus, were among the many who applauded his innovations.