FR1019000A - Dispositif de post-combustion pour turbo-réacteurs et moteurs analogues - Google Patents

Dispositif de post-combustion pour turbo-réacteurs et moteurs analogues

Info

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
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.)
McDonnell Aircraft Corp
Original Assignee
McDonnell Aircraft Corp
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 McDonnell Aircraft Corp filed Critical McDonnell Aircraft Corp
Application granted granted Critical
Publication of FR1019000A publication Critical patent/FR1019000A/fr
Expired legal-status Critical Current

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)
  • Processes For Solid Components From Exhaust (AREA)
  • Exhaust Gas After Treatment (AREA)
FR1019000D 1950-04-27 1950-05-19 Dispositif de post-combustion pour turbo-réacteurs et moteurs analogues Expired FR1019000A (fr)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Cited By (1)

* Cited by examiner, † Cited by third party
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
GB680371A (en) 1952-10-01
US2637972A (en) 1953-05-12

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