Search results

[[File:Turbine gaz animee.gif|thumb|Diagram of gas turbine with axial compressor]] ...[[mixed flow compressor]]. A fourth, unusual, type is the [[free-piston]] gas generator, which combines the functions of compressor and [[combustion cham ...

...ngle stage HP turbine drives the 9 stage HP compressor, while a 2-stage LP turbine drives the 3 stage fan. The combustor is annular. In 1998, the USAF's [[Loc |ref=<ref>Gas Turbine Engines. ''Aviation Week & Space Technology Source Book 2009''. p. 118.</ref> ...

...cycle]], but with continuous pulsed combustion, similar to that of a [[gas turbine]]. It can burn most commonly available hydrocarbon fuels and features the h ==Similar engines== ...

[[György Jendrassik]] worked on [[gas turbine]]s and in order to speed up research, he established the Invention Developm Following the successful running of a small experimental [[gas turbine]] engine of 100 bhp output in 1937, began to design a larger turboprop eng ...

...715.html ''Flight'', 1979. www.flightglobal.com]</ref> RB.401-06 prototype engines were already being manufactured when a decision to develop the higher thrus ...harged the HP compressor which was driven by the single stage transonic HP turbine. The combustor was annular and the co-annular exhaust featured a lightweigh ...

...om copying captured German equipment, it succeeded in producing home grown engines. ==Engines== ...

...pressor is driven by a single-stage turbine. On the LP spool a three-stage turbine drives a single-stage fan and a four-stage LP compressor. ...012-03-21 }}</ref> The engine final assembly line is located at [[MTU Aero Engines]] at their location in [[Hanover]], Germany. ...

..., driven by a single stage HP turbine. Power from a two-stage free (power) turbine is delivered to the load via a third shaft. A reverse flow combustor is fea ==Engines on display== ...

...EoAE">{{cite book|last=Gunston|first=Bill|title=World Encyclopedia of Aero Engines|publisher=Sutton Publishing|location=Stroud|year=2006|edition=5th|pages=194 As with subsequent Rolls-Royce gas turbines, it was named after a river, the [[River Clyde]]. ...

...ogle.com/books?id=oGPLBQAAQBAJ&pg=PA16 Aircraft Propulsion and Gas Turbine Engines By Ahmed F. El-Sayed p. 16]</ref> ...aracterized by high thrust-to-weight ratios and the use of [[turbine blade|turbine]] air cooling.<ref>Sosounov, V.A. (1990). ''The Development of Aircraft Pow ...

...rcharging a 14-stage high pressure (HP) compressor, driven by a 2-stage HP turbine. An annular combustor is featured. The TF34-GE-400A is rated at 9,275&nbsp; |turbine=4 stage LP, 2 stage HP ...

..."fi"/> and the later 2B2 variant made 1,100 horsepower.<ref name="military engines"/> ...al.com/news/articles/military-engines-local-power-213590/ | title=Military engines: Local power | publisher=Flightglobal | date=1 May 2007 | accessdate=13 Apr ...

...ame the [[Hawker Siddeley P.1127]] but with a [[Bristol Siddeley Orpheus]] gas generator which had a compressor derived from the Orion low pressure compre ...essor, the [[Bristol Proteus]], had a [[free-turbine turboshaft|free-power turbine]]. The [[combustor]] used separate [[flame can]]s. ...

...ame=Wilkinson70>{{cite book |last=Wilkinson |first=Paul H. |title=Aircraft engines of the World 1970 |year=1970 |publisher=Paul H. Wilkinson |location=Washing |turbine=1-stage HP turbine, 2-stage LP turbine ...

| known_for = Founder of Turbomeca and Bet Shemesh Engines ...in southern France. Once the war was over he developed small [[Gas turbine|turbine engine]]s for [[helicopter]]s. Turbomeca became a major supplier of [[helic ...

...s that von Ohain no longer favoured the [[centrifugal compressor]] for jet engines. He had been "sold" on the axial compressor as early as 1938, after a meeti ...in 1937. His first attempt at the HeS 3 was to separate the compressor and turbine &mdash;which were back-to-back in the HeS 1&mdash; and place the combustion ...

...gine has been in production since May 1960. The power unit consists of two engines coupled to a gearbox weighing 3,200&nbsp;kg (7,050&nbsp;lb). ; D-25V: Standard helicopter use production engines ...

...heseus''' was the [[Bristol Aeroplane Company]]'s first attempt at a gas-[[turbine]] engine design. A [[turboprop]] delivering just over 2,000&nbsp;hp (1,500 <ref>Making Jet Engines in World War II: Britain, Germany, and the United States', Hermione Giffard ...

...over of [[Bristol Siddeley]] in 1966, Bristol having absorbed de Havilland Engines Limited in 1961. ...dy been used in helicopters and de Havilland were able to test their first engines in a [[Westland Whirlwind (helicopter)|Westland Whirlwind]] and [[Westland ...

{{Short description|American manufacturer of small gas turbine engines}} ...gines based in [[Pontiac, Michigan]], [[United States]]. It produces [[jet engines]] for [[cruise missile]]s and small [[jet aircraft]]. ...