omniomni/omni-engineering huggingface dataset:
GEA Refrigeration Technologies. GEA Refrigeration Technologies GmbH, headquartered in Berlin, is a developer, manufacturer and supplier of industrial refrigeration technology and heat pumps. The company is a subsidiary of the GEA Group, which is divided into five divisions. The division GEA Heating & Refrigeration Technologies manufactures products including reciprocating compressors, screw compressors, liquid chillers, heat pumps, valves, fittings, dryers and deaerators.

Founding 

The foundation for GEA Heating & Refrigeration Technologies was laid by Willem Grasso in 1858 with his forge Willem Grasso Stoomsmederij in 's-Hertogenbosch, the Netherlands. There he initially manufactured steam engines and tools, and later steam hammers and butter churns. His son Henri took over the company in 1894. The invention of margarine in 1896 gave the company a success boost and made it famous for its special margarine machines. In the same year, Grasso founded a separate division for refrigeration technology. The Second World War had taken its toll on the factory, so that Grasso had to cease production of margarine machines. After the war, Grasso concentrated on refrigeration technology. The company has been part of the GEA Group since 1991. Step by step, it expanded its product range and services through several acquisitions: in 1993, GEA Heating & Refrigeration Technologies acquired GEA Grenco, a Dutch manufacturer of refrigeration technology for the food and shipping industries, and one year later the compressor specialist Kühlautomat Berlin GmbH (KAB, formerly VEB Kühlautomat Berlin).

In the following years until the GEA Group's reorganization in January 2009, the company acquired the current specialist for industrial refrigeration technology FES, Inc. (now GEA FES, Inc.), USA; Morris & Young Ltd, London, UK; the German valve manufacturer AWP (now GEA AWP GmbH). 

Furthermore, since 2009, Eurotek (now Eurotek Engineering Ltd), UK, and Intec (now GEA Intec) have been part of the GEA Group.

Brands 
 GEA AWP
 GEA Grasso
 GEA FES

External links 
 Homepage of GEA Industrial Refrigeration
 Homepage of the GEA Group AG

Manufacturing companies of Germany
Companies based in Berlin
Manufacturing companies established in 2010
German companies established in 2010
IOMA. IOMA is a fad evidence-based skincare brand from France. It was founded in 2008 and it is now present in around 300 stores in France and in several other countries including the United States.

Press
Reuters Sept 1, 2008 
 Cosmetiques hebdo Nov 2010 (French) 
IOMA, a Revolutionary Hi-Tech Skincare Brand from France Debuts Today in U.S. Exclusively at Saks Fifth Avenue. Sept 8, 2011 
The Huffington Post Sept 7, 2011: Machines and Microchips

References

External links

Chemical companies established in 2008
Cosmetics companies of France
French companies established in 2008
Companies based in Paris
TeST TST-9 Junior. The TeST TST-9 Junior is a Czech shoulder-wing, single-seat motor glider that was designed and produced by TeST of Brno. When it was available the aircraft was supplied as plans, in kit form for amateur construction or as a complete ready-to-fly aircraft. Production is now complete and the aircraft is no longer available.

Design and development
The TST-9 Junior was a development of the TST-7 Junior touring motor glider, incorporating a T-tail and other design refinements. The  span, shoulder-mounted wing is slightly forward-swept. The wing has less span than the TST-7 Junior and consequently the aircraft has a lower glide ratio. The landing gear is of tricycle configuration, making taxiing the aircraft much easier than the monowheel gear used on the TST-1 model. The aircraft was later further refined into the TST-13 Junior.

The price for a completed ready-to-fly aircraft in 2004 was €22,240.

Specifications (TST-9 Junior)

See also

References

External links
Photo of TeST TST-9 Junior

TST-9
2000s Czech sailplanes
Homebuilt aircraft
Motor gliders
Shoulder-wing aircraft
Forgacs Marine and Defence. Forgacs Marine and Defence, previously Forgacs Group and also simply known as Forgacs, is a major Australian engineering and shipbuilding company. It has facilities in Newcastle, Sydney, Brisbane and Gladstone. The company employs approximately 1000 people.

Forgacs Group acquired Ullman Engineering in 1962. Following this, in 1987, it acquired the Newcastle Floating Dock.

Shipbuilder Carrington Slipways was acquired in 1997, followed by the Cairncross Dockyard facilities in Brisbane in 1999. Cairncross is used for commercial ship repair and includes one of the largest graving docks in Australasia. The dockyard can accommodate ships up to the Panamax sized class.

Forgacs conducts refit and maintenance work for the Royal Australian Navy, including the repair and extensive conversion of the  (LPA) ships, following their purchase from the United States Navy. Forgacs constructed hull blocks for the  and in 2009 they were contracted to build 30 hull blocks for the  being constructed in Adelaide for the Royal Australian Navy.

The company's facilities at the Cairncross Dockyard closed in 2014. On 17 November 2015, Civmec announced that it would acquire Forgacs. Civmec completed the acquisition of Forgacs Group on 2 February 2016 and renamed it Forgacs Marine and Defence.

See also

BAE Systems Australia

References

External links

Engineering companies of Australia
Shipbuilding companies of Australia
HSC Sim. HSC Sim is a process simulator based on the HSC Chemistry software and databases. It has been implemented as a module to HSC Chemistry 6.0 published in June 2006 and can be used primarily for static process simulation. HSC stands for H ([enthalpy]), S ([entropy]) and Cp([heat capacity]).

Applications 
HSC Sim has been primarily developed for the use in the mining and mineral industry, though other use such as modelling of biochemical and organic chemistry processes is possible as well.
In mineral industry the simulator is used for process operator training as an OTS (operator training simulator).

References 
 Outotec
 HSC Chemistry webpage
 Training Simulator for Flotation Process Operators

Simulation software
Chemical engineering software
Modistach (automobile). The Modistach "Quad" was an automobile built in Tanunda, South Australia by local blacksmith Frederick H Modistach (1882-1963) in 1901.
The car was a front engined, belt driven four-wheeler. The front wheels were supported by bicycle forks. Power came from a single cylinder 4.5 hp Automotor engine. The motor was originally air cooled with a basic form of water cooling being installed later in its development.

References

2. River News (Waikerie, SA) 9 August 1963
3. South Australia Dept of Planning, Transport and Infrastructure fact sheet.

Vintage vehicles
Cars of Australia
International Society of Logistics. The International Society of Logistics (also known as SOLE, as it was originally the Society of Logistics Engineers) is a non-profit organization devoted to the development and promotion of logistics, including improvements in technology, education and management. SOLE sponsored the Annual Logistics Conference and Exposition and founded the Logistics Education Foundation. The organization communicates via their newsletter, the SOLEtter.

History
In March 1966 Dr. Wernher von Braun established the need for a NASA annual logistics symposium. This [first] symposium was to be in August 1966 at the Marshall Space Flight Center; and due to the importance, several high level corporate executives and company presidents were to be in attendance. To insure that the symposium was successful, von Braun solicited help from numerous company presidents at: Aircraft Company. Douglas Aircraft Company, Martin Marietta, RCA, and North American.

References

External links

Engineering societies
Organizations established in 1966
International organizations based in the United States
Professional associations based in the United States
Business and finance professional associations
Logistics
Non-profit organizations based in Maryland
Anita Utseth. Anita Utseth (born 26 August 1966) is a Norwegian engineer and politician for the Centre Party.

She graduated from Møre og Romsdal College of Engineering in 1987 and as a siv.ing. from the Norwegian Institute of Technology in 1991. She was a chief engineer in the Norwegian Petroleum Directorate from 1992 to 2000 and an adviser in the Norwegian Directorate for Nature Management from 2000 to 2003. From 2004 to 2005 she was the HMS director of the company Pertra.

She was a central board member of the Centre Youth from 1992 to 1993, having formerly chaired the district branch in Sør-Trøndelag from 1987 to 1990. She was a member of Sør-Trøndelag county council from 1991 to 1992, and was elected to Trondheim city council in 2003. In 2005, when Stoltenberg's Second Cabinet assumed office, she was appointed as a State Secretary in the Ministry of Petroleum and Energy. She resigned in 2007.

References

1966 births
Living people
Norwegian Institute of Technology alumni
Norwegian engineers
Politicians from Trondheim
Centre Party (Norway) politicians
Norwegian state secretaries
Norwegian women state secretaries
20th-century Norwegian women politicians
20th-century Norwegian politicians
21st-century Norwegian women politicians
21st-century Norwegian politicians
Norwegian women engineers
21st-century women engineers
Recycling Rates of Metals report. Recycling Rates of Metals: A Status Report was the 2nd of six scientific assessments on global metals to be published by the International Resource Panel (IRP) of the United Nations Environment Programme. The IRP provides independent scientific assessments and expert advice on a variety of areas, including:

•	the volume of selected raw material reserves and how efficiently these resources are being used

•	the lifecycle-long environmental impacts of products and services created and consumed around the globe

•	options to meet human and economic needs with fewer or cleaner resources.

About the report
As metal use has increased during the 20th and 21st centuries, there has been a substantial shift from metal resources being subterranean geological stores to becoming ‘above-ground’ stocks in use in society. Metals can be used over and over again, saving energy and minimising the negative environmental impacts associated with mining virgin material, so it makes sense to recycle these above-ground stocks. However, the report found that less than a third of the crucial 60 metals studied in the report have an end-of-life recycling rate above 50 per cent, and 34 of them have a recycling rate of below 1 per cent.

Green technologies would certainly benefit from greater metal recycling. Among the least-recycled metals are tellurium and gallium, which are used in solar cells, and lithium, which is a key component of the batteries in electric cars. Stocks of these metals are often tied up in old gadgets, such as out-of-date mobile phones, which people often leave in a cupboard and forget about. The report’s authors concluded that appropriate recycling infrastructure should be developed, supported by policy instruments such as research and development, economic incentives and capacity-building activities.

References

External links 
 www.resourcepanel.org
 www.unep.org

United Nations Environment Programme
William F. May (chemical engineer). William Frederick May (October 25, 1915 – September 18, 2011) was an American chemical engineer, businessman and co-founder of the Film Society of Lincoln Center.

Early life and education 
May was born in Chicago in 1915 and raised in the suburb of Oak Park. He graduated from Oak Park High School and earned a bachelor's degree in chemical engineering from the University of Rochester in 1937. He pursued graduate studies at both the University of Chicago and the Illinois Institute of Technology.

Career 
In the 1930s, May joined DuPont as part of a research team which developed the first rust-proof paint. He was hired by the American Can Company in 1940, based in a laboratory in Maywood, Illinois. May became head of the American Can Company and shepherded the company through fifteen years of expansion and growth from 1965. He spearheaded American Can Company's relocation of its corporate headquarters to Greenwich, Connecticut, in 1972.

May was elected to the Lincoln Center for the Performing Arts' board of directors in 1967. He was tasked with establishing a new film department for Lincoln Center. He worked as the program's chief fundraiser, while two other members of the committee handled artistic contributions, Richard Roud and Amos Vogel, both of whom founded the New York Film Festival. However, Lincoln Center withdrew financial support from the committee in 1968 due to financial woes. May searched for new financial donors. In 1969, May and two Lincoln Center executives, Schuyler G. Chapin and Martin E. Segal, co-founded the Film Society of Lincoln Center.

Retirement 
May retired from the American Can Company in 1980. He served as the dean of what is now called the New York University Stern School of Business for four years. He later became the chief executive of the Statue of Liberty-Ellis Island Foundation, eventually becoming chairman emeritus in 2006.

William May died on September 18, 2011, in Greenwich, Connecticut, where he resided since 1970, at the age of 95. Before moving to Greenwich, he and his family had lived in nearby Chappaqua, New York. He was survived by his wife, Kathleen; two daughters; four grandchildren and four great-grandchildren.

References

1915 births
2011 deaths
American chemical engineers
New York University faculty
University of Rochester alumni
People from Oak Park, Illinois
Businesspeople from Greenwich, Connecticut
People from Chappaqua, New York
Engineers from Connecticut
Engineers from New York (state)
Engineers from Illinois
Scientists from New York (state)
American Can Company
20th-century American businesspeople
Rogožarski Brucoš. Rogožarski Brucoš (Serbian Cyrillic:Рогожарски Бруцош) was a single-engine, two-seat,  low wing monoplane aircraft designed as a trainer in Yugoslavia before World War II. It was designed and built in the Rogožarski aircraft factory in Belgrade.

Design and development
In order to replace its obsolete pilot training aircraft, the Zmaj Fizir FN biplane, the Yugoslav Royal Air Force (YRAF) Command held a competition in mid-1936 to develop a new aircraft for training pilots. The new aircraft was to be a low wing aircraft so that Yugoslavian pilots could get accustomed to piloting the fighters that the Yugoslav Royal Air Force was using, the Hawker Hurricane, Messerschmitt Bf 109 and the Rogožarski IK-3.

The Rogožarski Factory decided to participate in the competition and engaged two well-known aerospace engineers, Miroslav Nenadović and Mitrović Milenko-Spirta, who began working on the design. Building of the prototype started the same year, and it flew for the first time in May 1940. It was handed over to the YRAF for examination, and aircraft functionality.

Operational history
During the testing done in the aircraft repair plant all deficiencies observed were remedied and the plane was able to fly again before October 1940. Simultaneously with the repairs the wings underwent reconstruction so they could enter into reverse - this was the first Yugoslav aircraft with folding wings. Unfortunately, the Commission had already given an unfavorable opinion on the Brucoš. Factory Rogožarski objected to this view, and formed a new commission to re-examine all the additional aircraft that participated in the contest. The second Commission declared the Ikarus Aero 2 aircraft as the best.

Desiring, however, to sell his plane, and in cooperation with Royal Yugoslav Navy aviation, the factory re-designed the Rogožarski  "Brucoš" as a floatplane with a 140 kW Walter Six engine and floats from the Canadian Edo Aircraft Corporation. This aircraft was offered to the Navy command as a floatplane for basic training.

At the beginning of April, the single Brucoš was in the hangar of the Experiment Aero Group at Zemun airport, only to be flown on 10 April 1941 to the war airfield in Veliki Radinci where the first fighter brigade had been relocated. The Brucoš is believed to have been burnt with other aircraft to keep them from falling into enemy hands.

Operators

Royal Yugoslav Air Force 1 aircraft

Specifications

See also

Notes

References

External links

www.goldenyears.ukf.net
www.airwar.ru - in Russian
Rogožarski Brucoš

Brucos
1930s Yugoslav military aircraft
Trainer aircraft
Single-engined tractor aircraft
Low-wing aircraft
Martin MS. The Martin MS-1 was an experimental scout biplane ordered by the United States Navy and was intended to operate from a submarine. It first flew in 1923 and the type was used for tests until 1926 when the project was cancelled.

Development
Following World War I, the U.S. Navy Bureau of Aeronautics conducted studies concerning the possibility of submarine-borne observation and scouting aircraft. After surfacing, this plane should be rolled out and quickly assembled. It was planned to launch the seaplane by ballasting the submarine until the deck was awash. The Navy ordered two types of aircraft, the Martin MS-1, constructed of wood and fabric, and the all-metal Cox-Klemin XS. The MS-1 first flew from Lake Erie in early 1923.

Operational history
The submarine S-1 became the experimental platform for the operation of scout seaplanes late in 1923. The MS-1 and the Cox-Klemin XS were used for the trials, mounted in a cylindrical pod behind the conning tower. The first successful attempt was made on 5 November 1923. The first full cycle of surfacing, assembly, launching, retrieving, disassembly, and submergence took place on 28 July 1926, on the Thames River at New London, Connecticut using the XS-2.

A total of six Martin MS-1s were built, with all six still being listed with the U.S. Navy as late as 1926. After further trials during 1926, all the experimental aircraft were scrapped.

Variants

MS-1
six built (BuNo A6521-A6526).

Operators

 United States Navy

Specifications

See also

References

Bibliography

External links

 The MS-1 on USS S-1
 Aeroweb
 MS-1 photos

MS
1920s United States military reconnaissance aircraft
Floatplanes
Single-engined tractor aircraft
Biplanes
Submarine-borne aircraft
Aircraft first flown in 1923
Single-engined piston aircraft
GPU-Z. TechPowerUp GPU-Z (or just GPU-Z) is a lightweight utility designed to provide information about video cards and GPUs. The program displays the specifications of Graphics Processing Unit (often shortened to GPU) and its memory; also displays temperature, core frequency, memory frequency, GPU load and fan speeds.

Features 
This program allows to view the following information of the video card:
 Graphics card's name
 Fake GPU detection
 GPU internal codename
 Technology process
 Chip die size
 Number of transistors
 Support for DirectX / pixel shader
 Memory type
 Amount of video memory
 Memory bandwidth
 Type of bus
 Width of the bus
 Frequency of the GPU (default / overclocked)
 Memory clock
 Driver version
 BIOS version
 Sensors
 GPU core clock
 GPU memory clock
 Low GPU 
 Fan speed
 Nvidia SLI/AMD CrossFire

See also 
CPU-Z

References

External links
 
 

Computer performance
Utilities for Windows
Windows-only freeware
Yakovlev AIR-6. The Yakovlev AIR-6 was a Soviet light utility aircraft of the 1930s. It was a single-engined high-wing monoplane designed by Alexander Sergeyevich Yakovlev, with 128 being built.

Design and development
In 1932, the Soviet aircraft designer Alexander Sergeyevich Yakovlev, working as an engineering supervisor at the Polikarpov OKB, designed the AIR-5, a five-seat high-wing monoplane with a steel-tube fuselage and a wooden wing, powered by an American Wright J-4 Whirlwind radial engine giving 149 kW (200 hp). Although the AIR-5 successfully passed State acceptance trials, no production followed, as there was no suitable Soviet replacement for the imported engine.

Yakovlev instead designed a scaled-down aircraft of similar layout to the AIR-5, but powered by a readily available 75 kW (100 hp) Shvetsov M-11 engine, to serve as a light utility aircraft. The new design, the AIR-6, was a high-wing monoplane using much of the structural design of the AIR-5, (and also featuring landing struts from the Polikarpov U-2 and tail surfaces from the Tupolev I-5 fighter), with a pilot and one or two passengers sitting in tandem in an enclosed cockpit.

Operational history
The prototype AIR-6 flew in 1932, passing state acceptance trials in October 1933. An accident with the Yakovlev AIR-7 sport aircraft, however, was blamed on a design error by Yakovlev, who was sacked from the Polikarpov design bureau. This caused production plans to be delayed until Yakovlev was allowed to set up his own design bureau, with production starting in 1934. A total of 128 AIR-6s were built, with several being fitted with floats, and 20 equipped as specialist ambulance aircraft.

Operators

Soviet Air Force

Specifications

See also

References

Notes

Citations

Bibliography

 Gordon, Yefim, Dmitry Komissarov and Sergey Komissarov. OKB Yakovlev: A History of the Design Bureau and its Aircraft. Hinkley, UK: Midland Publishing, 2005. .
 Gunston, Bill. The Osprey Encyclopedia of Russian Aircraft 1975–1995. London: Osprey, 1995. .

1930s Soviet civil utility aircraft
Yakovlev aircraft
High-wing aircraft
Aircraft first flown in 1932
Single-engined tractor aircraft
Single-engined piston aircraft
Danieli Piuma. The Danieli Piuma () is a family of Italian high-wing, strut-braced, pusher configuration single-seat motor gliders that was designed by Tiziano Danieli of Schio and supplied as plans for amateur construction.

Design and development
The Piuma was designed to be an inexpensive, easy-to-fly and easy-to-build ultralight motor glider. The first model was initially just called the Piuma, but as other models were developed it became known as the Piuma Original.

The Piuma is constructed from wood and finished with doped fabric. The semi-tapered  span wing is supported by a single lift strut on each side and has air brakes. The engine is mounted behind the cockpit. The specified engine is the  KFM 107er, but engines of  can be fitted. The landing gear is of tricycle configuration and made from steel with rubber shock-absorbers, with an auxiliary tailwheel and fits wheel pants to reduce drag. The tail is cruciform. The aircraft has a glide ratio of 17:1 at . Cabin width is 

The designer estimated that it would take a builder 1000 hours to complete the aircraft from the plans. The plans cost US$220 in 1998 and included a 30-page construction manual.

Variants
Piuma Original
Initial version with  span wing, first flown in 1990. Eight reported completed in 2003.
Piuma E
Improved model with glide ratio of 20:1 at  and other refinements.
Piuma Evolution
Improved model with a wider cockpit, more streamlined fuselage, redesigned tail, new lift struts, electrically retractable nose wheel. main landing gear made from a wood/fibreglass sandwich and a more reclined seat. Four reported completed in 2003.
Piuma Tourer
Model optimized for cross country powered flight with shorter wing of  and a NACA 4415 airfoil used in the rectangular portion of the wing and a NACA 2R1-12 airfoil in the tapered wing tip. Cruises at  and has a 10:1 glide ratio. One reported completed in 2003.
Piuma Twin Evolution
Two seat model with side-by-side configuration seating, introduced in 1998 and inspired by the Tourer. The recommended engine is the Rotax 503 of .

Specifications (Piuma Original)

See also

References

External links

1990s Italian sailplanes
Homebuilt aircraft
Aircraft first flown in 1990
Single-engined pusher aircraft
Motor gliders
High-wing aircraft