JPS57193746A - Variable area exhaust nozzle assembled body for gas turbine engine - Google Patents

Variable area exhaust nozzle assembled body for gas turbine engine

Info

Publication number
JPS57193746A
JPS57193746A JP57079819A JP7981982A JPS57193746A JP S57193746 A JPS57193746 A JP S57193746A JP 57079819 A JP57079819 A JP 57079819A JP 7981982 A JP7981982 A JP 7981982A JP S57193746 A JPS57193746 A JP S57193746A
Authority
JP
Japan
Prior art keywords
gas turbine
turbine engine
exhaust nozzle
variable area
assembled body
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
JP57079819A
Other languages
English (en)
Other versions
JPH0256507B2 (ja
Inventor
Maabuin Matsuden Uiriamu
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Publication of JPS57193746A publication Critical patent/JPS57193746A/ja
Publication of JPH0256507B2 publication Critical patent/JPH0256507B2/ja
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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted 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
    • F02K1/002—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Exhaust Silencers (AREA)
  • Control Of Turbines (AREA)
JP57079819A 1981-05-11 1982-05-11 Variable area exhaust nozzle assembled body for gas turbine engine Granted JPS57193746A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/262,367 US4392615A (en) 1981-05-11 1981-05-11 Viol exhaust nozzle with veer flap extension

Publications (2)

Publication Number Publication Date
JPS57193746A true JPS57193746A (en) 1982-11-29
JPH0256507B2 JPH0256507B2 (ja) 1990-11-30

Family

ID=22997194

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57079819A Granted JPS57193746A (en) 1981-05-11 1982-05-11 Variable area exhaust nozzle assembled body for gas turbine engine

Country Status (7)

Country Link
US (1) US4392615A (ja)
JP (1) JPS57193746A (ja)
CA (1) CA1182650A (ja)
DE (1) DE3216690A1 (ja)
GB (1) GB2098145B (ja)
IL (1) IL65660A (ja)
SE (1) SE445844B (ja)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2247048B (en) * 1981-06-27 1992-05-13 Rolls Royce Variable area nozzles for turbomachines
FR2714422A1 (fr) * 1983-01-13 1995-06-30 Snecma Tuyère convergente-divergente, en particulier pour turboréacteur.
JPS59141753A (ja) * 1983-01-31 1984-08-14 Fuji Heavy Ind Ltd Ｖ／ｓｔｏｌ機用推力増大偏向装置
US4714197A (en) * 1986-07-02 1987-12-22 United Technologies Corporation 2-D propulsive lift nozzle
US4819876A (en) * 1987-06-25 1989-04-11 United Technologies Corporation Divergent flap actuation system for a two-dimensional exhaust nozzle
DE3909347A1 (de) * 1989-03-22 1990-09-27 Mtu Muenchen Gmbh Schubduese zur schubvektorsteuerung fuer mit strahltriebwerken ausgeruestete fluggeraete
US5140809A (en) * 1990-02-12 1992-08-25 General Electric Company Exhaust nozzle idle thrust spoiling method
US5235808A (en) * 1990-02-12 1993-08-17 General Electric Company Exhaust nozzle including idle thrust spoiling
US5103639A (en) * 1990-02-26 1992-04-14 General Electric Company Exhaust nozzle having variable contour exhaust flap
US5201800A (en) * 1990-02-26 1993-04-13 General Electric Company Method for discharging combustion gases from an exhaust nozzle
US5102050A (en) * 1991-01-22 1992-04-07 General Electric Company Divergent flap actuation system for two-dimensional convergent - divergent turbojet exhaust nozzle
US5842643A (en) * 1996-12-03 1998-12-01 General Electric Company Articulated exhaust nozzle fairing
FR2789442B1 (fr) 1999-02-04 2001-11-09 Snecma Arriere-corps d'ejection a inversion de poussee de turboreacteur
EP1304472B1 (en) * 2001-10-19 2006-08-09 Industria de Turbo Propulsores S.A. Gas turbine engine two dimensional exhaust nozzle mechanism with reverse exhaust capability
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
GB0503874D0 (en) * 2005-02-24 2005-04-06 Rolls Royce Plc Fluid vectoring nozzle
US8475124B2 (en) * 2007-11-13 2013-07-02 General Electric Company Exhaust hood for a turbine and methods of assembling the same
US20110147533A1 (en) * 2009-12-21 2011-06-23 Honeywell International Inc. Morphing ducted fan for vertical take-off and landing vehicle
US9016695B2 (en) * 2011-08-02 2015-04-28 United Technologies Corporation Gas turbine exhaust nozzle divergent flap seal
RU2686535C1 (ru) * 2018-04-17 2019-04-29 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Плоское выходное устройство трехконтурного газотурбинного двигателя изменяемого цикла
US11339744B1 (en) * 2020-02-07 2022-05-24 Rolls-Royce North American Technologies Inc. Pressure equalization in a dual flow path exhaust of a hypersonic propulsion system
RU2765669C1 (ru) * 2021-02-17 2022-02-01 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Регулируемое сопло турбореактивного двигателя
CN114109648B (zh) * 2021-11-12 2023-02-28 中国航发沈阳发动机研究所 一种可调喷管外罩机构

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2969641A (en) * 1955-10-17 1961-01-31 Gen Electric Aerodynamic nozzle
US3367579A (en) * 1965-12-08 1968-02-06 Air Force Usa Supersonic convergent-divergent jet exhaust nozzle
US3979067A (en) * 1975-04-28 1976-09-07 General Electric Company Actuating means for a thrust vectoring gas turbine engine exhaust nozzle
US4000610A (en) * 1975-04-28 1977-01-04 General Electric Company Flight maneuverable nozzle for gas turbine engines
US4000612A (en) * 1975-07-28 1977-01-04 General Electric Company Cooling system for a thrust vectoring gas turbine engine exhaust system
US4000854A (en) * 1975-10-02 1977-01-04 General Electric Company Thrust vectorable exhaust nozzle
US4013226A (en) * 1976-04-14 1977-03-22 The United States Of America As Represented By The Secretary Of The Navy Variable jet nozzle with balanced two-dimensional blocker flap
US4175385A (en) * 1977-12-12 1979-11-27 General Electric Company Thrust reverser for an asymmetric aircraft exhaust nozzle

Also Published As

Publication number Publication date
GB2098145A (en) 1982-11-17
SE445844B (sv) 1986-07-21
GB2098145B (en) 1984-09-05
IL65660A0 (en) 1982-08-31
US4392615A (en) 1983-07-12
DE3216690A1 (de) 1982-12-02
JPH0256507B2 (ja) 1990-11-30
SE8202910L (sv) 1982-11-12
IL65660A (en) 1985-08-30
CA1182650A (en) 1985-02-19

Similar Documents

Publication Publication Date Title
JPS57193747A (en) Variable area exhaust nozzle assembled body for gas turbine engine
JPS57193746A (en) Variable area exhaust nozzle assembled body for gas turbine engine
JPS5720539A (en) Exhaust nozzle for gas turbine engine
GB2098719B (en) Gas turbine engine combustion apparatus
JPS5791328A (en) Axial flow gas turbine engine
JPS5641436A (en) Exhaust nozzle for gas turbine engines
GB2169696B (en) Gas turbine engine augmentor
JPS5751901A (en) Gas turbine engine
DE3566013D1 (en) Two dimensional gas turbine engine exhaust nozzle
GB2132278B (en) Gas turbine engine exhaust nozzle assembly
JPS5784930A (en) Gas turbine engine
GB2108586B (en) Gas turbine engine active clearance control
JPS572449A (en) Gas turbine engine
DE3175723D1 (en) Extending rocket engine exhaust nozzle assembly
JPS57176306A (en) Axial flow type gas turbine engine
IL67300A (en) Variable area convergent/divergent nozzle for a gas turbine engine
GB2163105B (en) Vectorable exhaust nozzle for gas turbine engine
GB2164613B (en) Vectorable exhaust nozzle for gas turbine engines
GB2194597B (en) A variable area exhaust nozzle for a gas turbine engine
JPS5776230A (en) Gas turbine engine
IL65777A0 (en) Nozzle assembly for gas turbine engines
GB2076893B (en) I c engine exhaust gas silencer
JPS5792609A (en) Fuel nozzle for gas turbine engine
GB2256007B (en) Gas turbine engine including a variable area nozzle
GB2238516B (en) Gas turbine engine