JPS51130715A - Gas turbine engine exhaust device and method of operating same - Google Patents

Gas turbine engine exhaust device and method of operating same

Info

Publication number
JPS51130715A
JPS51130715A JP51047944A JP4794476A JPS51130715A JP S51130715 A JPS51130715 A JP S51130715A JP 51047944 A JP51047944 A JP 51047944A JP 4794476 A JP4794476 A JP 4794476A JP S51130715 A JPS51130715 A JP S51130715A
Authority
JP
Japan
Prior art keywords
gas turbine
turbine engine
exhaust device
engine exhaust
operating same
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.)
Pending
Application number
JP51047944A
Other languages
English (en)
Inventor
Oouen Natsushiyu Deyuudoree
Jierarudo Biibaazu Robaato
Kureiton Baajie Jiyosefu
Tama Manueru Kasuteeru Onofuri
Ira Paakaa Aran
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 JPS51130715A publication Critical patent/JPS51130715A/ja
Pending 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)
JP51047944A 1975-04-28 1976-04-28 Gas turbine engine exhaust device and method of operating same Pending JPS51130715A (en)

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 (1)

Publication Number Publication Date
JPS51130715A true JPS51130715A (en) 1976-11-13

Family

ID=24287369

Family Applications (1)

Application Number Title Priority Date Filing Date
JP51047944A Pending JPS51130715A (en) 1975-04-28 1976-04-28 Gas turbine engine exhaust device and method of operating same

Country Status (6)

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

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
US4280660A (en) * 1979-08-17 1981-07-28 General Electric Company Vectorable 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
FI894371A (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
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

Family Cites Families (15)

* 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
NL255475A (ja) * 1959-10-05
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
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
US3527408A (en) * 1968-06-06 1970-09-08 United Aircraft Corp Curved exhaust deflection system
US3558058A (en) * 1969-03-14 1971-01-26 Us Air Force Thrust vectorable supersonic nozzle
FR2087976B1 (ja) * 1970-05-04 1973-03-16 Bertin & Cie

Also Published As

Publication number Publication date
FR2309727A1 (fr) 1976-11-26
GB1541065A (en) 1979-02-21
DE2617752A1 (de) 1976-11-11
FR2309727B1 (ja) 1982-08-20
IT1059999B (it) 1982-06-21
US4000610A (en) 1977-01-04

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