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Turbomeca Gabizo
The Turbomeca
Turbomeca
Gabizo was a small turbojet engine produced by Turbomeca from the 1950s
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Turbojet
The turbojet is an airbreathing jet engine, typically used in aircraft. It consists of a gas turbine with a propelling nozzle. The gas turbine has an air inlet, a compressor, a combustion chamber, and a turbine (that drives the compressor). The compressed air from the compressor is heated by the fuel in the combustion chamber and then allowed to expand through the turbine. The turbine exhaust is then expanded in the propelling nozzle where it is accelerated to high speed to provide thrust.[1] Two engineers, Frank Whittle
Frank Whittle
in the United Kingdom and Hans von Ohain
Hans von Ohain
in Germany, developed the concept independently into practical engines during the late 1930s. Turbojets have been replaced in slower aircraft by turboprops because they have better range-specific fuel consumption. At medium speeds, where the propeller is no longer efficient, turboprops have been replaced by turbofans
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International Standard Book Number
"ISBN" redirects here. For other uses, see ISBN (other).International Standard Book
Book
NumberA 13-digit ISBN, 978-3-16-148410-0, as represented by an EAN-13 bar codeAcronym ISBNIntroduced 1970; 48 years ago (1970)Managing organisation International ISBN AgencyNo. of digits 13 (formerly 10)Check digit Weighted sumExample 978-3-16-148410-0Website www.isbn-international.orgThe International Standard Book
Book
Number (ISBN) is a unique[a][b] numeric commercial book identifier. Publishers purchase ISBNs from an affiliate of the International ISBN Agency.[1] An ISBN is assigned to each edition and variation (except reprintings) of a book. For example, an e-book, a paperback and a hardcover edition of the same book would each have a different ISBN. The ISBN is 13 digits long if assigned on or after 1 January 2007, and 10 digits long if assigned before 2007
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SNECMA Turbomeca Larzac
The SNECMA
SNECMA
Turbomeca
Turbomeca
Larzac is a military turbofan manufactured by GRTS (Groupement Turbomeca-SNECMA),[1] a consortium between the two French companies, SNECMA
SNECMA
and Turbomeca
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Snecma
Safran
Safran
Aircraft
Aircraft
Engines (previously Snecma) is a French aerospace engine manufacturer headquartered in Courcouronnes, France. It designs and makes engines for commercial and military aircraft as well as rocket engines for launch vehicles and satellites. Some of its notable past developments, alone or in partnership, include the M88 for the Rafale, Olympus 593 for the Concorde, CFM56/CFM-LEAP for single-aisle airliners, and the Vulcain
Vulcain
engines for the Ariane 5. It has 15,700 employees working at 35 production sites, offices, and MRO facilities worldwide
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Rolls-Royce Turbomeca RTM322
The Rolls-Royce Turbomeca
Turbomeca
RTM322 is a turboshaft engine produced by Rolls-Royce Turbomeca
Turbomeca
Limited, a joint venture between Rolls-Royce plc and Turbomeca. The engine was designed to suit a wide range of military and commercial helicopter designs
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Rolls-Royce Turbomeca Adour
The Rolls-Royce Turbomeca
Turbomeca
Adour
Adour
is a two-shaft low bypass turbofan aircraft engine developed by Rolls-Royce Turbomeca
Turbomeca
Limited, a joint venture between Rolls-Royce (UK) and Turbomeca
Turbomeca
(France). The engine is named after the Adour, a river in south western France.[1]Contents1 History 2 Variants2.1 Reheated (Afterburning) 2.2 Dry (Non-afterburning) 2.3 Higher bypass3 Applications3.1 Licence-built4 Specifications ( Adour
Adour
Mk 106)4.1 General characteristics 4.2 Components 4.3 Performance5 See also 6 References 7 External linksHistory[edit] The Adour
Adour
is a turbofan engine developed primarily to power the Anglo-French SEPECAT Jaguar
SEPECAT Jaguar
fighter-bomber, achieving its first successful test run in 1968
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MTR MTR390
The MTU Turbomeca Rolls-Royce MTR390 is a turboshaft developed for light helicopter applications by MTU Turbomeca Rolls-Royce (MTR). The engine is designed to power helicopters in the weight range of 5-7 tonnes in both single and twin engine configurations. So far the only application is the Eurocopter Tiger. Test runs of the MTR390 began in 1989 and the first test flight was performed in 1991
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MTU Turbomeca Rolls-Royce
MTU Turbomeca
Turbomeca
Rolls-Royce GmbH (MTR) is a joint venture among three European aero-engine manufacturers, MTU Aero Engines, Turbomeca
Turbomeca
and Rolls-Royce. The company's only product is the MTR390, a turboshaft developed for helicopter applications such as the Eurocopter Tiger. External links[edit]Official company pagev t eJoint develop
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Hindustan Aeronautics Limited
Hindustan Aeronautics
Hindustan Aeronautics
Limited (HAL) is an Indian state-owned aerospace and defence company headquartered in Bangalore, India. It is governed under the management of the Indian Ministry of Defence. The government-owned corporation is primarily involved in the operations of the aerospace and is currently involved in the design, fabrication and assembly of aircraft, jet engines, helicopters and their spare parts. It has several facilities spread across India including Nasik, Korwa, Kanpur, Koraput, Lucknow, Bangalore
Bangalore
and Hyderabad
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Turboshaft
A turboshaft engine is a form of gas turbine which is optimized to produce shaft power rather than jet thrust. In concept, turboshaft engines are very similar to turbojets, with additional turbine expansion to extract heat energy from the exhaust and convert it into output shaft power. They are even more similar to turboprops, with only minor differences, and a single engine is often sold in both forms. Turboshaft
Turboshaft
engines are commonly used in applications that require a sustained high power output, high reliability, small size, and light weight. These include helicopters, auxiliary power units, boats and ships, tanks, hovercraft, and stationary equipment.Contents1 Overview 2 History 3 See also 4 References 5 External linksOverview[edit] A turboshaft engine may be made up of two major parts assemblies: the 'gas generator' and the 'power section'
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Turboprop
A turboprop engine is a turbine engine that drives an aircraft propeller.[1] In contrast to a turbojet, the engine's exhaust gases do not contain enough energy to create significant thrust, since almost all of the engine's power is used to drive the propeller. In its simplest form a turboprop consists of an intake, compressor, combustor, turbine, and a propelling nozzle. Air is drawn into the intake and compressed by the compressor. Fuel is then added to the compressed air in the combustor, where the fuel-air mixture then combusts. The hot combustion gases expand through the turbine. Some of the power generated by the turbine is used to drive the compressor. The rest is transmitted through the reduction gearing to the propeller. Further expansion of the gases occurs in the propelling nozzle, where the gases exhaust to atmospheric pressure
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France
France
France
(French: [fʁɑ̃s]), officially the French Republic (French: République française [ʁepyblik fʁɑ̃sɛz]), is a country whose territory consists of metropolitan France
France
in western Europe, as well as several overseas regions and territories.[XIII] The metropolitan area of France
France
extends from the Mediterranean Sea
Mediterranean Sea
to the English Channel
English Channel
and the North Sea, and from the Rhine
Rhine
to the Atlantic Ocean. The overseas territories include French Guiana
French Guiana
in South America and several islands in the Atlantic, Pacific and Indian oceans
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Auxiliary Power Unit
An auxiliary power unit (APU) is a device on a vehicle that provides energy for functions other than propulsion
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Aircraft Engine
An aircraft engine is the component of the propulsion system for an aircraft that generates mechanical power
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Special
Special
Special
or specials may refer to:Contents1 Music 2 Film and television 3 Other uses 4 See alsoMusic[edit] Special
Special
(album), a 1992 album by Vesta Williams "Special" (Garbage song), 1998 "Special
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