omniomni/omni-engineering huggingface dataset:
BAW Yusheng. The BAW Yusheng (北汽BAW 域胜007) or BAW BW007 (), is a compact sports utility vehicle (SUV) produced by the Chinese manufacturer BAW from September 2010, and launched in 2011.

Overview

Debuting during the 2010 Beijing Auto Show, price range of the BAW BW007 ranges from 89,800 yuan to 12,800 yuan at launch, and was adjusted to 82,800 yuan to 107,800 yuan later in the market. 

The BAW BW007 was developed from 2007 when BAW still produce Jeeps in the Beijing-Jeep joint venture. Early prototypes were based on Jeep platforms, and initial styling of the prototypes resembles Jeep-branded vehicles. Engines of the BW007 is a 2.4 liter engine with 105kw and 217nm. 

News of a facelift was revealed in 2013. Known updates for the BAW BW007 facelift are mainly focused on the interior, with the center console updated to resemble that of the Range Rovers.

BAW Ruiling pickup

The BAW Ruiling pickup (锐铃) is a pickup based on the BW007 SUV. It was revealed during the 2012 Beijing Auto Show with a length of 5088mm, a width of 1820mm and a height of 1804mm. The wheelbase is longer than the BW007 at 2735mm. Curb weight of the BAW Ruiling pickup is 2735kg, and max load is 1910kg.

References

External links

BW007 Official website
Pickup Official website

BAW vehicles
Compact sport utility vehicles
Cars introduced in 2010
Cars of China
2010s cars
Sergey Izotov. Sergey Petrovich Izotov (Russian: Серге́й Петро́вич Изо́тов; 30 June 1917 – 6 May 1983) was a Soviet scientist and designer of aircraft engines.

Biography 
Izotov was a Chief and General Designer (1960–1983) of OKB-117 later became the NPO named after V. I. Klimov where Izotov was also the General Designer. Hero of Socialist Labour (1969) and winner of Lenin Prize (1978), Stalin Prize first degree (1949) and the USSR State Prize (1971). 

Izotov was Doctor of Technical Sciences (1968) and Merited Engineering Scientist of the RSFSR. He was the author of 30 scientific papers and 13 inventions. 

He was awarded a title of Freeman of the city of Rzeszów (Poland). Delegate of the 26th Congress of the Communist Party of the Soviet Union.

References

Sources

Further reading 
 Герои труда/ Справочник о Героях Социалистического Труда и кавалерах ордена Трудовой Славы трех степеней из Башкортостана./ сост. Р. А. Валишин [и др.]. — Уфа : Китап, 2011. — 432 с. : ил. -.
 Башкирская энциклопедия. Гл. ред. М. А. Ильгамов т. 3. З-К. 2007. — 672 с.  науч. изд. Башкирская энциклопедия, Уфа.
 

1917 births
1983 deaths
Full Members of the Russian Academy of Sciences
Full Members of the USSR Academy of Sciences
Peter the Great St. Petersburg Polytechnic University alumni
People from Pavlogradsky Uyezd
Heroes of Socialist Labour
Recipients of the Stalin Prize
Recipients of the Lenin Prize
Recipients of the Order of Lenin
Recipients of the Order of the Red Banner of Labour
Recipients of the USSR State Prize
Early spaceflight scientists
Rocket scientists
Russian aerospace engineers
Russian space program personnel
Soviet aerospace engineers
Soviet space program personnel
Burials at Bogoslovskoe Cemetery
Neeranchal National Watershed Project. The Neeranchal National Watershed Project (NNWP) is a World Bank assisted project undertaken by the Government of India to support the Integrated Watershed Management Program (IWMP) for the improvement and conservation of water resources. The project started in 2016 and will continue until 2022.

The Ministry of Rural Development will implement the project and support the Pradhan Mantri Krishi Sinchayi Yojana in water management. Gujarat, Madhya Pradesh, Chhattisgarh, Rajasthan, Telangana, Andhra Pradesh, Jharkhand, and Maharashtra are the chosen states for project implementation. The cost of the total project is Rs. 2142 crore, of which 50% is funded by the World Bank.

References 

World Bank
Aerodynamics Research Institute. The Aerodynamische Versuchsanstalt (AVA) in Göttingen was one of the four predecessor organizations of the 1969 founded "German Research and Experimental Institute for Aerospace", which in 1997  was renamed German Aerospace Center (DLR).

History 

The AVA was created in 1919 from the 1907 Göttingen by Ludwig Prandtl founded "Modellversuchsanstalt für Aerodynamik der Motorluftschiff-Studiengesellschaft". In its founding years, it was still concerned with the development of the "best" form of airship. In 1908, the first wind tunnel was built in Göttingen for tests on models for aviation. In 1915, founded in 1911 Kaiser Wilhelm Society (KWG) and under the direction of Ludwig Prandtl the "Modellversuchsanstalt aerodynamics" was founded in 1919 as the "Aerodynamic Research Institute of the Kaiser Wilhelm Society" (AVA) was transferred to the KWG and converted in 1925 into the "Kaiser Wilhelm Institute for Flow Research linked to the Aerodynamic Research Institute".

Ludwig Prandtl headed the institute until 1937, his successor became Albert Betz. In the same year a spin-off from the institute took place under the name "Aerodynamische Versuchsanstalt Göttingen e. V. in the Kaiser Wilhelm Society ", in which the Reich Ministry of Aviation was involved.
The remaining after the spin-off part was continued under the name "Kaiser Wilhelm Institute for Flow Research" from the 1948, the Max Planck Institute for Fluid Research (today Max Planck Institute for Dynamics and Self-Organization).

The AVA was confiscated in 1945 by the British (until 1948), 1953 as "Aerodynamic Research Institute Göttingen e. V. re-opened in the Max Planck Society and fully integrated in 1956 as the "Aerodynamic Research Institute in the Max Planck Society".

In 1969, the spin-off from the Max Planck Society and the founding of the "German Research and Experimental Institute for Aerospace e. V.".

Bibliography 
 Aerodynamische Versuchsanstalt Göttingen e.V. in der Kaiser-Wilhelm-/Max-Planck-Gesellschaft (CPTS), in: Eckart Henning, Marion Kazemi: Handbuch zur Institutsgeschichte der Kaiser-Wilhelm-/ Max-Planck-Gesellschaft zur Förderung der Wissenschaften 1911–2011 – Daten und Quellen, Berlin 2016, 2 subvolumes, volume 1: Institute und Forschungsstellen A–L (online, PDF, 75 MB), pages 27–45 (Chronologie des Instituts)

Sources 
 Historie des DLR – Gesellschaft von Freunden des DLR e. V.
 100 Jahre DLR – Homepage des DLR
 Archiv zur Geschichte der Max-Planck-Gesellschaft

Former research institutes
Aerodynamics
Research institutes in Göttingen
Max Planck Institutes
Aviation history of Germany
1907 establishments in Germany
1969 disestablishments in West Germany
History of Lower Saxony
Lioré et Olivier LeO 5. The Lioré-et-Olivier LeO 5 was a French ground attack biplane, built shortly after World War I, initially to the S2 armoured attack aircraft specification  and then to the Ab2 specification, from the STAé (Service Technique de l'Aéronautique).

Specifications (Leo 5)

References

Further reading
 Hartmann, Gérard. Les Avions Lioré Et Olivier. Boulogne-Billancourt, France: ETAI. 2002.  (in French)

External links
 Airwar LeO 5

1910s French attack aircraft
5
Aircraft first flown in 1919
Twin piston-engined tractor aircraft
Biplanes
Rotary-engined aircraft
Lioré et Olivier LeO 48. The Lioré-et-Olivier LeO 48 was a French experimental aircraft that was built early in World War II.

Specifications (LeO 48)

References

Further reading
 Hartmann, Gérard. Les Avions Lioré Et Olivier. Boulogne-Billancourt, France: ETAI. 2002.  (in French)

1940s French experimental aircraft
48
Aircraft first flown in 1941
Twin piston-engined tractor aircraft
Mid-wing aircraft
Twin-tail aircraft
Lioré et Olivier LeO H-6. The Lioré-et-Olivier LeO H-6 and LeO H-6/2 were French flying boat and amphibian aircraft, built shortly after World War I.

Design
The LeO H-6 was a biplane flying boat with a monocoque fuselage. The second example, the LeO H-6/2, with similar powerplant, was completed as an amphibian.

Variants
LeO H-6 the first aircraft a flying boat transport.
LeO H-6/2 The generally similar amphibious version.

Specifications (LeO H-6)

References

1910s French civil aircraft
6
Trimotors
Aircraft first flown in 1919
Flying boats
Amphibious aircraft
Gustavo Baquero. Gustavo Baquero is a Venezuelan engineer, professor and oil industry executive.  S&P said he would be named by Juan Guaidó's administration to be president of PDVSA (Venezuela's state-run petroleum company).

Raised in Caracas in a family of doctors, Baquero did undergraduate studies at Venezuela's Andres Bello Catholic University (UCAB) and graduate studies at Harvard University. He has taught petroleum economics at UCAB and business management of hydrocarbons at IESA in Caracas.  He was described by Americas Quarterly as an oil expert who would someday help rebuild Venezuela.  Together with Leopoldo López, he wrote Venezuela Energética.

Publications

References

External links
 

Living people
People of the Crisis in Venezuela
Year of birth missing (living people)
USS Pierre (LCS-38). USS Pierre (LCS-38) will be an  of the United States Navy. She will be the second ship to be named for Pierre, South Dakota, the first being , a  from World War II.

Design and construction
In 2002, the United States Navy initiated a program to develop the first of a fleet of littoral combat ships. The Navy initially ordered two trimaran hulled ships from General Dynamics, which became known as the  after the first ship of the class, . Even-numbered US Navy littoral combat ships are built using the Independence-class trimaran design, while odd-numbered ships are based on a competing design, the conventional monohull . The initial order of littoral combat ships involved a total of four ships, including two of the Independence-class design. On 29 December 2010, the Navy announced that it was awarding Austal USA a contract to build ten additional Independence-class littoral combat ships.

Pierre is being built in Mobile, Alabama by Austal USA.

References

Proposed ships of the United States Navy
Independence-class littoral combat ships
Loening C-1. The Loening C-1 Air Yacht was an amphibious airliner produced in the United States at the end of the 1920s.

Design
The Loening C-1 was based on the OL observation aircraft being developed from the United States Navy (USN). It was a two-bay biplane of unconventional design, with a tall, narrow fuselage that nearly filled the interplane gap. The pilot (and sometimes one passenger) sat in an open cockpit at the top of the fuselage, with the engine mounted in front of them. Underneath the fuselage was a long "shoehorn"-style float, that extended forward underneath the engine and propeller. Four to six passengers could be accommodated in a fully enclosed cabin within the fuselage. The main units of the undercarriage retracted into wells in the sides of the fuselage. Stabilising floats were fitted against the undersides of the lower wing. Eight C-1Ws were built, and the type was further developed into the C-2.

Specifications (C-1W)

References

1920s United States airliners
Floatplanes
C-1
Single-engined tractor aircraft
Biplanes
Aircraft first flown in 1928
Loening M-2 Kitten. The Loening M-2 Kitten was a light aircraft produced in the United States at the end of the 1920s, for use aboard capital ships and submarines of the United States Navy (USN).

Design
The M-2 was a small monoplane designed for operation from battleships or submarines, with either floats or wheels for operations. Three aircraft were built with USN serials A442-A444; the first used an ABC Gnat, but the others were powered by a Lawrance L-3 radial engine.

Loening developed a dedicated floatplane version of the M-2, the Loening M-3, of which one airframe (Navy serial A5469) was built for the Navy.

Specifications (M-2 landplane)

References

1910s United States military reconnaissance aircraft
Floatplanes
M-2
Single-engined tractor aircraft
Monoplanes
Aircraft first flown in 1918
Nicolas-Claude NC-2 Aquilon. The Nicolas-Claude NC-2 Aquilon was a single-seat touring aircraft built in the late 1930s, featuring a low-wing monoplane with canard foreplanes. The NC-2 was first flown on 5 April 1937 at Auxerre.

Specifications (NC-2 Aquilon)

References

1930s French civil utility aircraft
NC-2
Aircraft first flown in 1937
74 Engineer Regiment (United Kingdom). The 74th Engineer Regiment was a former Territorial Army regiment of the Royal Engineers, British Army.  Initially the 74th (Antrim Artillery) Engineer Regiment was a reserve engineer regiment, but was then disbanded in 1994. An independent squadron remained.  As part of Army 2020 the squadron moves to become part of the 71st Engineer Regiment.

History 
The 74th (Antrim Artillery) Engineer Regiment was formed in 1967 in the dramatic reduction and reorganisation of the Territorial Army.  It originally was created by the merger of two existing units: 146 (Antrim Artillery) Corps Engineer Regiment, Royal Engineers and 591 (Antrim) Independent Field Squadron.  Its first headquarters till its disbandment was at Belfast.  The regiment was assigned to the 8th Engineer Brigade the majority of its history from 1967 - 1992.  In 1994 the regiment was disbanded, but a single squadron remained, becoming the 74 Independent Field Squadron (V), later 591 Independent Squadron at Bangor.  Today the regiment has its traditions carried on by 591 (Antrim Artillery) Field Squadron which is still headquartered at Bangor.  As part of Army 2020 the squadron is planned to join the 71st (Northern) Reserve Engineer Regiment, Royal Engineers, remaining at the same location.

Organization 

The regiment's structure changed very little but did have a few changes.  The structure just before the disbandment is:

 Headquarters Squadron
112 (Antrim Fortress) Field Squadron
114 (Antrim Artillery) Field Squadron
 272 (West Riding) Field Squadron

At some time the regiment also controlled the following units:

 591 Field Squadron
 Ballymena Troop
 Bangor Troop
 Carrickfergus Troop
 Antrim Troop
 Regimental Pipes and Drums, 74th Engineer Regiment

References 

Regiments of the Royal Engineers
103 (Tyne Electrical Engineers) Field Squadron. The 72nd (Tyne Electrical Engineers) Engineer Regiment was a territorial regiment of the Royal Engineers, British Army, for three periods between 1967 and 2014. The regiment was later reduced to squadron size and renamed as 103 (Tyne Electrical Engineers) Field Squadron within 71 Engineer Regiment.

History

72nd Engineer Regiment 

The 72nd Engineer Regiment was formed when the Territorial Army was re-organised in the 1960s. It was created from the 50th (Northumbrian) Infantry Division's engineer regiment and some other separate squadrons. Its first and only headquarters were at Gateshead. From 1967 - 1992 it was assigned to the 29th Engineer Brigade. Both 103 and 188 Squadrons were assigned to the "Harrier Support Group" from 1972 - 1982. In 1999 the regiment was disbanded but one squadron remained 72 (Tyne Electrical Engineers) Air Support Field Squadron which was a reserve air support squadron within the 71st Engineer Regiment. In 2006 the regiment was reformed and 72 Squadron became the new headquarters squadron. Under Army 2020 the regiment will disband but the squadrons will be reassigned to other regiments.

During its time, the regiment had the following structure;

 Regimental Headquarters, Gateshead
 Regimental Pipes and Drums of the Tyne Electrical Engineers (moved to 102 Battalion REME and later disbanded)
 103 (Tyne Electrical Engineers) Field Squadron, Newcastle upon Tyne (moved to 21 Engineer Regiment)
 2 Troop, Sunderland
 106 (West Riding) Field Squadron, Sheffield (moved to 32 Engineer Regiment)
 Troop, Bradford
 299 Parachute Squadron, Wakefield (moved to 23 Parachute Engineer Regiment)
 1 Troop, Hull
 3 Troop, Gateshead

72 and 103 (TEE) Field Squadron 
Under the Army 2020 refine, 72 Engineer Regiment was disbanded with most of its units being re-designated and moving to other regiments. Part of the changes was the renaming of 72 (Tyne Electrical Engineers) Air Support Field Squadron to become 103 (Tyne Electrical Engineers) Field Squadron. Another change, was the moving under control of 21st Engineer Regiment. Following this change, the squadron is now the reserve squadron of the regiment, supporting the 1st Strike Brigade. The squadron currently maintains 2 Troop in Sunderland, while the rest of the squadron is based in Heaton.  Following the Field Army changed on 1 August 2019, the squadron was moved from the 21st Engineer Regiment to 71st Engineer Regiment (V) headquartered at Leuchars Station.

References 

Squadrons of the Royal Engineers
Military units and formations in Northumberland
Military units and formations in Newcastle upon Tyne
Military units and formations established in 1967
73 Engineer Regiment (United Kingdom). 73 Engineer Regiment was a Territorial regiment of the Royal Engineers, part of the British Army active from 1969 to 2014.

History 
73 Engineer Regiment was formed when the Territorial Army was drastically reduced in the late 1960s.  The regiment was created as a reinforcement combat engineer unit to support I (BR) Corps in Germany. 

From 1969 - 1991 the regiment was assigned to 29 Engineer Brigade. It sponsored the Robin Hood Battalion cadre, 1969-71. In 1991 the regiment was re-organized to become 73 Air Support Engineer Regiment.  In 1997 the regiment was assigned to 12 (Air Support) Engineer Brigade.  Parts of the regiment served in Operation Telic I and Operation Telic III.  In 2006 the regiment was re-organized to become 73 Engineer Regiment.  In 2014 the regiment was disbanded and only 1 squadron remained and moved to 33 Explosive Ordnance Disposal Engineer Regiment.

Structure 
The regiment's structure changed a bit through its history, the structure just before disbandment:

 Headquarters Troop
575 (Sherwood Foresters) Field Squadron
 129 (East Riding) Field Squadron
 350 (Nottinghamshire) Field Squadron

A number of former squadrons served with the regiment including:

 129 Headquarters and Support Squadron
217 (London) Field Squadron
 272 (West Riding Artillery) Field Squadron
 873 Movement Light Squadron
 106 (West Riding) Field Squadron
 The Jersey Field Squadron, Royal Engineers

References 

Regiments of the Royal Engineers
Morane-Saulnier MS.224. The Morane-Saulnier MS.224 was a prototype fighter plane built by Morane-Saulnier in the early 1930s.

Design
The MS.224 was a high-wing monoplane based on the Morane-Saulnier MS.223, being made from wood and metal. It differed from the MS.223 in having a larger wing and Gnome-Rhône 9Asb engine. The MS.224 flew in 1931 and showed an improvement in top speed over that of the MS.223 despite an increase in weight. Although the MS.224 wasn't ordered into production, it paved way for the development of the Morane-Saulnier M.S.225.

Specifications (MS.224)

References

Further reading

MS.224
1930s French fighter aircraft
High-wing aircraft
Single-engined tractor aircraft
Morane-Saulnier TRK. The Morane-Saulnier TRK (aka Morane-Saulnier MoS-9) was a prototype French bomber built during World War I.

Design
The Morane-Saulnier TRK was a large triplane with the engines mounted in the fuselage, facing outboard and canted upwards. The engines drove a propeller each, through driveshafts and bevel gearboxes, with the propeller gearboxes strut mounted beneath the middle mainplanes. Cooling for the engines was provided by a tall radiator stack above the centre of the fuselage, between the middle and upper mainplanes. The two tractor propellers ran just forward of the middle mainplanes.

Two pilots sat in open cockpits side-by-side in the nose of the aircraft, which also had a wind-driven generator at the very tip. The third crew-member was housed in the rear fuselage and attended the engines in flight or operated defensive armament. The fixed undercarriage was of the conventional contemporary tail-skid type, with a nose-over protection wheel, strut-mounted under the nose. The left and right, strut-supported, mainwheel assemblies were of very wide track, with a wheel at each end of both axles.

Specifications (TRK)

References

Further reading

1910s French bomber aircraft
Racing aircraft
Aircraft first flown in 1915
Triplanes
Twin piston-engined tractor aircraft
Morane-Saulnier MS.250. The Morane-Saulnier MS.250 was a crew-trainer aircraft built by Morane-Saulnier in the late 1920s.

Design
The MS.250 was a parasol-wing monoplane with swept-back wings, similar to the Morane-Saulnier MS.230, but differed in having a new tail. The cockpits had windscreens, and the rear cockpit had a gun ring. The pilot-instructor manned the front cockpit, and the trainee observer manned the rear cockpit. A second aircraft was built with a more powerful engine as the MS.251.

Variants
MS.250 Initial design prototype, powered by a   Salmson 9Ab radial engine; one built.
MS.251 A second aircraft, powered by a  Lorraine 7Mc radial engine.

Specifications (MS.250)

References

Further reading

1920s French military trainer aircraft
Morane-Saulnier aircraft
Aerobatic aircraft
Parasol-wing aircraft
Single-engined tractor aircraft
Aircraft first flown in 1929
Ruan Xueyu. Ruan Xueyu (; 6 January 1933 – 3 February 2019) was a Chinese pressure processing specialist and academician of the Chinese Academy of Engineering (CAE). He had hailed as the "Father of Cold Extrusion Technology" in China. He was a professor at Shanghai Jiao Tong University, a part-time professor at Tsinghua University, and honorary professor at Kumamoto University.

He was the head of Shanghai Mould Technology Research Institute, director of Ford Motor Company-SJTU C3P Research Center, advanced counselor of Swiss FEINTOOL company, director on the Korean journal International Journal of Automotive Technology and the German journal Research in Engineering Design, standing member of ICEM. He was a member of the 10th Central Committee of Jiusan Society, one of the eight legally recognised political parties in China.

Biography
Ruan was born in Shanghai, on 6 January 1933, with his ancestral home in Zhongshan, Guangdong. His paternal grandfather was an overseas Chinese in Australia. His maternal grandfather was an overseas Chinese in Thailand. His father was a businessman in Shanghai and his mother was a famous doctor. He attended the Huanguang School. He elementary studied at the Second Middle School Affiliated to Datong University and secondary studied at the Nanyang Model High School. In 1950 he was accepted to Shanghai Jiao Tong University, where he majored in the Mechanical Department. After graduation, he pursued advanced studies in Tsinghua University.

He taught at Shanghai Jiao Tong University since 1953. His first academic work, Cold Extrusion Technology, was published by Shanghai Science and Technology Publishing House in 1963, which became textbook of Beijing Institute of Technology. In 1983, with the support of Shanghai Jiao Tong University, the leaders of Shanghai Municipal Government, he established the Shanghai Institute of Mold Technology and served as its director. That same year, he joined the Jiusan Society, one of the eight legally recognised political parties in China. In 1994 he was elected a fellow of the Chinese Academy of Engineering (CAE). In 1994, the Department of Plastic Forming Engineering was established in Shanghai Jiao Tong University, Ruan served as its dean. In 1996, with the approval of the State Planning Commission, the National Die and Mould CAD Engineering Research Center was established on the basis of the Shanghai Die and Mould Technology Research Institute, Ruan Xueyu became its director. 

On 3 February 2019, he died of illness at Huadong Hospital, in Shanghai, aged 86.

References

1933 births
2019 deaths
Engineers from Shanghai
Nanyang Model High School alumni
National Chiao Tung University (Shanghai) alumni
Tsinghua University alumni
Academic staff of Shanghai Jiao Tong University
Members of the Chinese Academy of Engineering
Members of the Jiusan Society