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- [[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 ...6 KB (848 words) - 20:51, 22 June 2025
- |caption=MTR 390 on display at the [[MTU Aero Engines]] museum, [[Munich]] |ref=''Aviation Week & Space Technology'' <ref>Gas Turbine Engines. ''Aviation Week & Space Technology Source Book 2009''. p. 121.</ref> ...3 KB (450 words) - 02:24, 20 February 2024
- {{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]]. ...7 KB (946 words) - 00:38, 21 January 2025
- ...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 ...5 KB (676 words) - 08:22, 31 March 2025
- ..., 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== ...5 KB (681 words) - 15:00, 18 August 2024
- [[File:Labyrinthdichtung01.jpg|right|thumb|250px|A labyrinth seal on a steam turbine shaft]] ...sher=Butterworth-Heinemann|isbn=978-0-08-099416-1}}</ref> Indeed, many gas turbine engine seals leak by design.<ref name="AircraftCabinAir">{{cite speech|last ...4 KB (610 words) - 14:53, 10 August 2024
- ...d air flowed into an annular combustion chamber between the compressor and turbine, which made the engine longer.{{Citation needed|date=June 2014}} The first ...ough the combustor. The flow was then turned radially inwards to enter the turbine. Although not as compact as the original design, the 3b was much simpler. T ...7 KB (1,075 words) - 19:31, 19 January 2024
- {{Short description|Canadian series of aircraft engines}} ...iver-first-engines-for-phenom-100/72650.article |title= P&WC deliver first engines for Phenom 100 |author= Guy Norris |date= 21 March 2007 |work= FlightGlobal ...7 KB (1,009 words) - 18:14, 26 December 2024
- ..."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 ...4 KB (528 words) - 08:09, 26 March 2025
- ...om copying captured German equipment, it succeeded in producing home grown engines. ==Engines== ...4 KB (510 words) - 07:48, 1 August 2024
- |type =Constant volume gas turbine jet engine ...stant-volume combustion, similar to the [[Otto cycle]] used in most piston engines, is considerably more fuel efficient than the [[Brayton cycle|constant-pres ...5 KB (716 words) - 06:20, 24 November 2024
- {{Short description|Type of gearbox used on jet engines}} ...aulic transmissions]] found in the [[accessory drive]]s of [[gas turbine]] engines, such as aircraft [[jet engine]]s. On modern aircraft, the CSD is often com ...5 KB (699 words) - 17:23, 9 December 2024
- ;RB.44 Tay:Rolls-Royce development engines only, no production. ...ef name=AEotW57>{{cite book |last=Wilkinson |first=Paul H. |title=Aircraft engines of the World 1957 |year=1957 |publisher=Sir Isaac Pitman & Sons Ltd. |locat ...5 KB (705 words) - 13:42, 31 March 2025
- ...ical stress.<ref>{{Cite book|title=The Development of Jet and Turbine Aero Engines|last=Gunston|first=Bill|publisher=PSL|year=2006|isbn=0-7509-4477-3}}</ref> ...nd.<ref>{{Cite book|title=The Design of High-Efficiency Turbomachinery and Gas Turbines|last=Wilson|first=David|publisher=The MIT Press|year=2014|isbn=978 ...4 KB (566 words) - 03:05, 24 December 2023
- |manufacturer= [[Lycoming Engines]] <br> [[Honeywell Aerospace]] <br> [[Ozark Aeroworks LLC]] ...raft]] since the 1950s. It was designed at the [[Lycoming Engines|Lycoming Turbine Engine Division]] in [[Stratford Army Engine Plant|Stratford, Connecticut]] ...7 KB (914 words) - 19:36, 24 June 2025
- ...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 ...10 KB (1,304 words) - 16:58, 19 January 2025
- ...Heritage of Aircraft Turbine Technology |date=1990 |publisher=GE Aircraft Engines |pages=54 |lccn=90082948}}</ref> ...loy B]].<ref>[http://www.machinedesign.com/technologies/100-years-aircraft-engines Machine Design] (retrieved 30 May 2017)</ref> ...8 KB (1,121 words) - 21:05, 5 May 2025
- ...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]]. ...6 KB (896 words) - 14:31, 28 May 2025
- ...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 —which were back-to-back in the HeS 1— and place the combustion ...8 KB (1,298 words) - 01:14, 24 April 2024
- ...tion chamber, and a power output section consisting of a single-stage free turbine driving an output shaft via a two-stage reduction gearbox. ...is taken from the front of the [[gearbox]] and is transmitted beneath the gas generator via a flexible coupling, while the drive for the [[tail rotor]] i ...5 KB (738 words) - 13:46, 18 June 2023