FR1203751A - Perfectionnements aux moteurs à turbine à gaz - Google Patents

Perfectionnements aux moteurs à turbine à gaz

Info

Publication number
FR1203751A
FR1203751A FR1203751DA FR1203751A FR 1203751 A FR1203751 A FR 1203751A FR 1203751D A FR1203751D A FR 1203751DA FR 1203751 A FR1203751 A FR 1203751A
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
engine improvements
gas
turbine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1203751A publication Critical patent/FR1203751A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38—Introducing air inside the jet
    • F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Silencers (AREA)
  • Supercharger (AREA)
FR1203751D 1957-04-03 1958-04-02 Perfectionnements aux moteurs à turbine à gaz Expired FR1203751A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB10962/57A GB852829A (en) 1957-04-03 1957-04-03 Improvements in or relating to gas-turbine jet propulsion engines

Publications (1)

Publication Number Publication Date
FR1203751A true FR1203751A (fr) 1960-01-21

Family

ID=9977507

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1203751D Expired FR1203751A (fr) 1957-04-03 1958-04-02 Perfectionnements aux moteurs à turbine à gaz

Country Status (4)

Country Link
US (1) US3100627A (fr)
DE (1) DE1118538B (fr)
FR (1) FR1203751A (fr)
GB (1) GB852829A (fr)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB918778A (en) * 1959-06-23 1963-02-20 Rolls Royce Improvements in or relating to gas-turbine engines
DE1230619B (de) * 1960-03-14 1966-12-15 Rolls Royce Mantelstromgasturbinentriebwerk
DE1193312B (de) * 1961-03-21 1965-05-20 Rolls Royce Mantelstromtriebwerk
DE1209808B (de) * 1961-12-27 1966-01-27 Rolls Royce Zweistromgasturbinenstrahltriebwerk mit einer Nachbrenner-Brennstoffeinspritzvorrichtung im Schubrohr
US3348379A (en) * 1963-09-25 1967-10-24 Rolls Royce Turbojet engine with compressor bypass and aft fan
US3330117A (en) * 1964-11-27 1967-07-11 Rolls Royce By-pass gas turbine jet engine
US3343629A (en) * 1965-01-11 1967-09-26 Koppers Co Inc Sound suppressor for reaction engines
GB1139005A (en) * 1966-03-25 1969-01-08 Rolls Royce Improvements in or relating to gas turbine by-pass engines
US3377804A (en) * 1966-06-13 1968-04-16 Gen Electric Flow mixers particularly for gas turbine engines
US3393516A (en) * 1966-12-05 1968-07-23 United Aircraft Corp Curved exhaust deflector
DE1923150A1 (de) * 1968-05-08 1970-01-15 Man Turbo Gmbh Zweistromturbinenstrahltriebwerk
US4226084A (en) * 1970-07-24 1980-10-07 General Motors Corporation Ducted fan engine exhaust mixer
US3999378A (en) * 1974-01-02 1976-12-28 General Electric Company Bypass augmentation burner arrangement for a gas turbine engine
US4018046A (en) * 1975-07-17 1977-04-19 Avco Corporation Infrared radiation suppressor for gas turbine engine
US4217756A (en) * 1977-12-27 1980-08-19 Boeing Commercial Airplane Company Vortex mixers for reducing the noise emitted by jet engines
FR2456216A1 (fr) * 1979-05-11 1980-12-05 Astech Sa Turbomoteur a double flux equipe d'un inverseur de poussee
US4315401A (en) * 1979-11-30 1982-02-16 United Technologies Corporation Afterburner flameholder construction
US4817378A (en) * 1987-02-13 1989-04-04 General Electric Company Gas turbine engine with augmentor and variable area bypass injector
US6098402A (en) * 1989-02-10 2000-08-08 Sawruk; Stephen D. Infra-red stealth masking device (IRSMD)
US5117628A (en) * 1990-01-25 1992-06-02 General Electric Company Mixed flow augmentor pre-mixer
US5638675A (en) * 1995-09-08 1997-06-17 United Technologies Corporation Double lobed mixer with major and minor lobes
FR2858999B1 (fr) * 2003-08-18 2005-11-11 Snecma Moteurs Turbomachine pour aeronef a emissions de bruit reduites
US20100146980A1 (en) * 2007-05-22 2010-06-17 Volvo Aero Corporation masking arrangement for a gas turbine engine
US8904799B2 (en) * 2009-05-25 2014-12-09 Majed Toqan Tangential combustor with vaneless turbine for use on gas turbine engines
RU2550370C2 (ru) * 2011-05-11 2015-05-10 Альстом Текнолоджи Лтд Центробежная форсунка с выступающими частями
US8938971B2 (en) 2011-05-11 2015-01-27 Alstom Technology Ltd Flow straightener and mixer
WO2014113038A1 (fr) * 2013-01-21 2014-07-24 United Technologies Corporation Relation entre des vitesses de courants d'échappement primaire et de ventilateur dans un moteur à turbine à gaz à engrenages
CA2862597C (fr) * 2013-10-03 2018-12-11 Karl L. Hasel Architecture de turbine a gaz a engrenages pour une efficacite amelioree
JP6229590B2 (ja) 2014-04-30 2017-11-15 株式会社Ihi アフタバーナ及び航空機エンジン
FR3036138B1 (fr) * 2015-05-12 2020-01-31 Safran Aircraft Engines Turbomachine comportant un melangeur a plusieurs series de lobes

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB766728A (fr) * 1900-01-01
GB650710A (fr) * 1900-01-01
US2088591A (en) * 1935-12-27 1937-08-03 Atlantic Refining Co Mixing device
US2421518A (en) * 1940-07-05 1947-06-03 United Aircraft Corp Jet propulsion
US2297910A (en) * 1941-02-18 1942-10-06 Alfons H Neuland System for charging and cooling internal combustion engines
US2308059A (en) * 1941-04-03 1943-01-12 Ammiel F Decker Exhaust device for internal combustion engines
US2358690A (en) * 1942-11-21 1944-09-19 Decker Products Co Exhaust system
US2588532A (en) * 1943-05-12 1952-03-11 Allis Chalmers Mfg Co Jet propulsion unit
US2501633A (en) * 1943-06-28 1950-03-21 Lockheed Aircraft Corp Gas turbine aircraft power plant having ducted propulsive compressor means
US2426833A (en) * 1943-11-05 1947-09-02 Power Jets Res & Dev Ltd Apparatus for mixing fluids
US2465099A (en) * 1943-11-20 1949-03-22 Allis Chalmers Mfg Co Propulsion means comprising an internal-combustion engine and a propulsive jet
US2488783A (en) * 1945-03-12 1949-11-22 Edward A Stalker Gas turbine
FR995990A (fr) * 1945-04-04 1951-12-11 Rateau Soc Perfectionnement aux turbines à gaz entraînant une hélice aérienne
US2620622A (en) * 1945-05-12 1952-12-09 Svenska Turbinfab Ab Reverse thrust arrangement for braking jet-propelled aircraft
US2647369A (en) * 1946-09-06 1953-08-04 Leduc Rene Combustion chamber for fluid fuel burning in an air stream of high velocity
US2653446A (en) * 1948-06-05 1953-09-29 Lockheed Aircraft Corp Compressor and fuel control system for high-pressure gas turbine power plants
US2650073A (en) * 1949-06-25 1953-08-25 Air Preheater Combined regenerator and precooler for gas turbine cycles
GB695482A (en) * 1950-11-28 1953-08-12 Rolls Royce Improvements in or relating to gas-turbine engines
US2600733A (en) * 1950-12-06 1952-06-17 Standard Oil Co Gas mixing apparatus
BE503064A (fr) * 1951-05-10 1900-01-01
US2825204A (en) * 1951-05-30 1958-03-04 Snecma Jet propulsion units
US2852233A (en) * 1952-12-23 1958-09-16 Parsons C A & Co Ltd Regenerative heat exchangers especially for combustion turbines
GB749009A (en) * 1953-04-24 1956-05-16 Power Jets Res & Dev Ltd An improved jet propulsion plant

Also Published As

Publication number Publication date
GB852829A (en) 1960-11-02
US3100627A (en) 1963-08-13
DE1118538B (de) 1961-11-30

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