FR1203751A - Perfectionnements aux moteurs à turbine à gaz - Google Patents
Perfectionnements aux moteurs à turbine à gazInfo
- 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
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)
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)
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 |
WO2008143556A1 (fr) * | 2007-05-22 | 2008-11-27 | Volvo Aero Corporation | Agencement de masquage pour moteur à turbine à gaz |
US8904799B2 (en) * | 2009-05-25 | 2014-12-09 | Majed Toqan | Tangential combustor with vaneless turbine for use on gas turbine engines |
US8938971B2 (en) | 2011-05-11 | 2015-01-27 | Alstom Technology Ltd | Flow straightener and mixer |
RU2550370C2 (ru) * | 2011-05-11 | 2015-05-10 | Альстом Текнолоджи Лтд | Центробежная форсунка с выступающими частями |
EP2946102A4 (fr) * | 2013-01-21 | 2016-01-20 | United Technologies Corp | 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)
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 |
NL161099C (nl) * | 1951-05-10 | 1900-01-01 | Tecalemit Group Services Limit | Inrichting voor het smeren van een voertuig af- hankelijk van de afgelegde weg. |
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 |
-
1957
- 1957-04-03 GB GB10962/57A patent/GB852829A/en not_active Expired
-
1958
- 1958-03-31 US US725326A patent/US3100627A/en not_active Expired - Lifetime
- 1958-04-02 FR FR1203751D patent/FR1203751A/fr not_active Expired
- 1958-04-03 DE DER23073A patent/DE1118538B/de active Pending
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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