FR2309727A1 - Dispositif d'ejection manoeuvrable en vol pour moteur a turbine a gaz - Google Patents

Dispositif d'ejection manoeuvrable en vol pour moteur a turbine a gaz

Info

Publication number
FR2309727A1
FR2309727A1 FR7612512A FR7612512A FR2309727A1 FR 2309727 A1 FR2309727 A1 FR 2309727A1 FR 7612512 A FR7612512 A FR 7612512A FR 7612512 A FR7612512 A FR 7612512A FR 2309727 A1 FR2309727 A1 FR 2309727A1
Authority
FR
France
Prior art keywords
maneuverable
gas turbine
turbine engine
ejection device
flight
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.)
Granted
Application number
FR7612512A
Other languages
English (en)
French (fr)
Other versions
FR2309727B1 (enExample
Inventor
Dudley O Nash
Robert G Beavers
Joseph C Burge
Onofre Tama Manuel Castells
Alan I Parker
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2309727A1 publication Critical patent/FR2309727A1/fr
Application granted granted Critical
Publication of FR2309727B1 publication Critical patent/FR2309727B1/fr
Granted 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
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/006—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector within one plane only
    • 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
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1215—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, and the downstream series having its flaps hinged at their downstream ends on a fixed structure

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
FR7612512A 1975-04-28 1976-04-28 Dispositif d'ejection manoeuvrable en vol pour moteur a turbine a gaz Granted FR2309727A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/572,340 US4000610A (en) 1975-04-28 1975-04-28 Flight maneuverable nozzle for gas turbine engines

Publications (2)

Publication Number Publication Date
FR2309727A1 true FR2309727A1 (fr) 1976-11-26
FR2309727B1 FR2309727B1 (enExample) 1982-08-20

Family

ID=24287369

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7612512A Granted FR2309727A1 (fr) 1975-04-28 1976-04-28 Dispositif d'ejection manoeuvrable en vol pour moteur a turbine a gaz

Country Status (6)

Country Link
US (1) US4000610A (enExample)
JP (1) JPS51130715A (enExample)
DE (1) DE2617752A1 (enExample)
FR (1) FR2309727A1 (enExample)
GB (1) GB1541065A (enExample)
IT (1) IT1059999B (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2463859A1 (fr) * 1979-08-17 1981-02-27 Gen Electric Tuyere d'ejection a flux de gaz ejectes orientable

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4175385A (en) * 1977-12-12 1979-11-27 General Electric Company Thrust reverser for an asymmetric aircraft exhaust nozzle
GB2469613B (en) * 1980-11-28 2011-03-23 Rolls Royce Plc Aircraft
US4392615A (en) * 1981-05-11 1983-07-12 United Technologies Corporation Viol exhaust nozzle with veer flap extension
US4482109A (en) * 1981-06-04 1984-11-13 Dupont Anthony A Jet aircraft
US4519543A (en) * 1982-04-07 1985-05-28 Rolls-Royce Inc. Vectorable nozzles for turbomachines
GB2164613B (en) * 1984-08-16 1987-09-03 Rolls Royce Vectorable exhaust nozzle for gas turbine engines
GB2185718B (en) * 1986-01-23 1989-11-01 Rolls Royce Exhaust nozzle for a gas turbine engine
US4813607A (en) * 1987-10-02 1989-03-21 Allied-Signal Inc. Variable-area thrust vectoring and reversing asymmetric aircraft exhaust nozzle
US5016818A (en) * 1989-08-21 1991-05-21 General Electric Company Integral transition and convergent section exhaust nozzle
FI894371A7 (fi) * 1989-09-15 1991-03-16 Nokia Mobile Phones Ltd Telefonsystem.
FR2680547B1 (fr) * 1991-08-21 1993-10-15 Hispano Suiza Inverseur de poussee de turboreacteur ayant un bord de deviation a courbure evolutive.
US5769317A (en) * 1995-05-04 1998-06-23 Allison Engine Company, Inc. Aircraft thrust vectoring system
US6382559B1 (en) 1999-08-13 2002-05-07 Rolls-Royce Corporation Thrust vectoring mechanism
RU2193680C2 (ru) * 2001-01-03 2002-11-27 Открытое акционерное общество "Авиадвигатель" Регулируемое плоское сопло для газотурбинного двигателя
US6918244B2 (en) * 2001-08-17 2005-07-19 John Eugene Dickau Vertical takeoff and landing aircraft propulsion systems
US6857600B1 (en) 2002-04-26 2005-02-22 General Electric Company Infrared suppressing two dimensional vectorable single expansion ramp nozzle
US7395657B2 (en) * 2003-10-20 2008-07-08 General Electric Company Flade gas turbine engine with fixed geometry inlet
US20070018034A1 (en) * 2005-07-12 2007-01-25 Dickau John E Thrust vectoring
US7669785B2 (en) * 2006-04-24 2010-03-02 The Boeing Company Integrated engine exhaust systems and methods for drag and thermal stress reduction
FR2928900B1 (fr) * 2008-03-20 2010-03-19 Airbus France Dispositif pour reduire les emissions infrarouge d'un turbopropulseur.
US9932845B2 (en) * 2011-06-30 2018-04-03 United Technologies Corporation Impingement cooled nozzle liner
WO2017218841A1 (en) 2016-06-15 2017-12-21 The Regents Of The University Of California Two-dimensional supersonic nozzle thrust vectoring using staggered ramps

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1119126B (de) * 1960-03-18 1961-12-07 Bmw Triebwerkbau Ges M B H Strahltriebwerk mit einer Strahlumlenkeinrichtung
US3019601A (en) * 1959-10-05 1962-02-06 United Aircraft Corp Pen-shaped nozzle with thrust deflector
US3115748A (en) * 1960-05-06 1963-12-31 Rolls Royce Gas turbine engine
FR2010251A1 (enExample) * 1968-06-06 1970-02-13 United Aircraft Corp
US3756542A (en) * 1970-05-04 1973-09-04 Bertin & Cie Aircraft having an auxiliary lift device

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2891740A (en) * 1957-06-27 1959-06-23 John P Campbell External-flow jet flap
US3046730A (en) * 1960-09-21 1962-07-31 Marquardt Corp Variable area exit nozzle
FR1283690A (fr) * 1961-03-15 1962-02-02 B M W Triebwerkbau Ges M B H Réacteur pour la propulsion d'avions
US3258206A (en) * 1964-01-09 1966-06-28 Gen Electric Thrust deflector
US3302889A (en) * 1964-10-01 1967-02-07 United Aircraft Corp Blow-in door ejector for stol
US3390837A (en) * 1965-12-08 1968-07-02 Gen Electric Convergent-divergent plug nozzle having a plurality of freely-floating tandem flaps
US3380660A (en) * 1966-04-28 1968-04-30 United Aircraft Corp Variable area exhaust deflector
US3409250A (en) * 1966-12-27 1968-11-05 Gen Electric Movable fairing for an aircraftmounted nozzle
FR1547756A (fr) * 1967-10-19 1968-11-29 Snecma Silencieux pour réacteurs aéronautiques
US3558058A (en) * 1969-03-14 1971-01-26 Us Air Force Thrust vectorable supersonic nozzle

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3019601A (en) * 1959-10-05 1962-02-06 United Aircraft Corp Pen-shaped nozzle with thrust deflector
DE1119126B (de) * 1960-03-18 1961-12-07 Bmw Triebwerkbau Ges M B H Strahltriebwerk mit einer Strahlumlenkeinrichtung
US3115748A (en) * 1960-05-06 1963-12-31 Rolls Royce Gas turbine engine
FR2010251A1 (enExample) * 1968-06-06 1970-02-13 United Aircraft Corp
US3756542A (en) * 1970-05-04 1973-09-04 Bertin & Cie Aircraft having an auxiliary lift device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2463859A1 (fr) * 1979-08-17 1981-02-27 Gen Electric Tuyere d'ejection a flux de gaz ejectes orientable

Also Published As

Publication number Publication date
GB1541065A (en) 1979-02-21
FR2309727B1 (enExample) 1982-08-20
DE2617752A1 (de) 1976-11-11
IT1059999B (it) 1982-06-21
JPS51130715A (en) 1976-11-13
US4000610A (en) 1977-01-04

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Legal Events

Date Code Title Description
ST Notification of lapse