FR1019000A - Dispositif de post-combustion pour turbo-réacteurs et moteurs analogues - Google Patents
Dispositif de post-combustion pour turbo-réacteurs et moteurs analoguesInfo
- Publication number
- FR1019000A FR1019000A FR1019000DA FR1019000A FR 1019000 A FR1019000 A FR 1019000A FR 1019000D A FR1019000D A FR 1019000DA FR 1019000 A FR1019000 A FR 1019000A
- Authority
- FR
- France
- Prior art keywords
- turbo
- reactors
- post
- combustion device
- similar engines
- 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
- 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
- F02K1/78—Other construction of jet pipes
- F02K1/80—Couplings or connections
- F02K1/805—Sealing devices therefor, e.g. for movable parts of jet pipes or nozzle flaps
-
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
-
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/11—Varying effective area of jet pipe or nozzle by means of pivoted eyelids
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Gas After Treatment (AREA)
- Processes For Solid Components From Exhaust (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB10381/50A GB680371A (en) | 1950-04-27 | 1950-04-27 | Reheater for jet propulsion engines |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1019000A true FR1019000A (fr) | 1953-01-15 |
Family
ID=9966787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1019000D Expired FR1019000A (fr) | 1950-04-27 | 1950-05-19 | Dispositif de post-combustion pour turbo-réacteurs et moteurs analogues |
Country Status (3)
Country | Link |
---|---|
US (1) | US2637972A (fr) |
FR (1) | FR1019000A (fr) |
GB (1) | GB680371A (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2676779A1 (fr) * | 1991-05-21 | 1992-11-27 | Lair Jean Pierre | Tuyere a section variable. |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2828603A (en) * | 1948-04-09 | 1958-04-01 | Westinghouse Electric Corp | Afterburner for turbo jet engines and the like |
US2771740A (en) * | 1950-11-16 | 1956-11-27 | Lockheed Aircraft Corp | Afterburning means for turbo-jet engines |
US2981065A (en) * | 1951-01-26 | 1961-04-25 | David H Sloan | Ramjet device |
US2775864A (en) * | 1951-04-10 | 1957-01-01 | Gen Motors Corp | Jet propulsion engine with afterburner |
US2782593A (en) * | 1951-06-08 | 1957-02-26 | United Aircraft Corp | Multi-unit ramjet |
US2760339A (en) * | 1952-06-02 | 1956-08-28 | Douglas Aircraft Co Inc | Flameholder |
US2744384A (en) * | 1952-08-09 | 1956-05-08 | United Aircraft Corp | Burner construction for high velocity gases |
NL182171C (nl) * | 1952-09-12 | Delta Nederland B V | Collectorzonweringsstelsel. | |
US2866314A (en) * | 1953-01-02 | 1958-12-30 | United Aircraft Corp | Flame holding device movable between a flameholding position and a streamlined position |
US2746243A (en) * | 1954-01-14 | 1956-05-22 | Solar Aircraft Co | Variable nozzle and sealing means therefor for jet engine |
US2839131A (en) * | 1956-01-16 | 1958-06-17 | Darwin G Pattinson | Gas burner |
US2944399A (en) * | 1956-05-31 | 1960-07-12 | Gen Electric | Afterburner combustion means |
US2865167A (en) * | 1957-08-22 | 1958-12-23 | United Aircraft Corp | Inner cone attachment |
US3085401A (en) * | 1959-01-22 | 1963-04-16 | Rolls Royce | Reheat combustion equipment of gas-turbine engines |
US3021386A (en) * | 1960-03-30 | 1962-02-13 | Gen Electric | Boiler port viewing system |
US3514957A (en) * | 1967-02-27 | 1970-06-02 | Gen Electric | High speed propulsion engine |
US3792582A (en) * | 1970-10-26 | 1974-02-19 | United Aircraft Corp | Combustion chamber for dissimilar fluids in swirling flow relationship |
FR2182647B1 (fr) * | 1972-05-02 | 1975-08-29 | Snecma | |
US4662658A (en) * | 1984-06-04 | 1987-05-05 | General Electric Company | Seal |
US6968694B2 (en) * | 2003-03-13 | 2005-11-29 | United Technologies Corporation | Augmentor |
US20080196414A1 (en) * | 2005-03-22 | 2008-08-21 | Andreadis Dean E | Strut cavity pilot and fuel injector assembly |
DE102011118735A1 (de) * | 2011-11-17 | 2013-05-23 | Alstom Technology Ltd. | Diffusor, insbesondere für eine axiale strömungsmaschine |
US10563620B2 (en) * | 2016-08-12 | 2020-02-18 | Rolls-Royce North American Technologies Inc. | Expandable exhaust cone |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2405723A (en) * | 1946-08-13 | Propulsion apparatus | ||
US2304008A (en) * | 1938-07-30 | 1942-12-01 | Muller Max Adolf | Combined recoil drive |
US2268464A (en) * | 1939-09-29 | 1941-12-30 | Bbc Brown Boveri & Cie | Combustion chamber |
US2385833A (en) * | 1943-01-27 | 1945-10-02 | Kevork K Nahigyan | Fuel vaporizer for jet propulsion units |
US2408099A (en) * | 1943-04-07 | 1946-09-24 | Sherman Albert | Variable-area nozzle for jetpropelled aircraft |
US2402363A (en) * | 1943-10-21 | 1946-06-18 | Westinghouse Electric Corp | Turbine apparatus |
FR919004A (fr) * | 1944-11-27 | 1947-02-25 | Power Jets Res & Dev Ltd | Perfectionnements apportés aux tuyères à section utile variable, notamment à celles utilisées pour une propulsion par réaction |
FR920910A (fr) * | 1945-02-01 | 1947-04-22 | Power Jets Res & Dev Ltd | Perfectionnements apportés aux dispositifs de combustion, plus spécialement à ceux dans lesquels circulent des courants gazeux à vitesse élevée |
US2447482A (en) * | 1945-04-25 | 1948-08-24 | Westinghouse Electric Corp | Turbine apparatus |
US2448561A (en) * | 1946-05-01 | 1948-09-07 | Westinghouse Electric Corp | Gas turbine apparatus |
US2522081A (en) * | 1947-06-23 | 1950-09-12 | Armstrong Siddeley Motors Ltd | Combustion chamber with fuel vaporizing pipes for internal-combustion turbine plants |
US2518881A (en) * | 1947-06-25 | 1950-08-15 | Daniel And Florence Guggenheim | Fuel feeding and cooling construction for rotating combustion chambers |
US2506611A (en) * | 1948-03-02 | 1950-05-09 | Westinghouse Electric Corp | Fuel control for aviation gas turbine power plants |
CA486078A (fr) * | 1950-04-27 | 1952-08-26 | W. Kellal George | Controle d'espace de sortie pour moteurs thermopropulseurs |
-
1948
- 1948-04-09 US US19957A patent/US2637972A/en not_active Expired - Lifetime
-
1950
- 1950-04-27 GB GB10381/50A patent/GB680371A/en not_active Expired
- 1950-05-19 FR FR1019000D patent/FR1019000A/fr not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2676779A1 (fr) * | 1991-05-21 | 1992-11-27 | Lair Jean Pierre | Tuyere a section variable. |
Also Published As
Publication number | Publication date |
---|---|
US2637972A (en) | 1953-05-12 |
GB680371A (en) | 1952-10-01 |
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