JPS59141753A - Ｖ／ｓｔｏｌ機用推力増大偏向装置 - Google Patents

Ｖ／ｓｔｏｌ機用推力増大偏向装置

Info

Publication number
JPS59141753A
JPS59141753A JP58014441A JP1444183A JPS59141753A JP S59141753 A JPS59141753 A JP S59141753A JP 58014441 A JP58014441 A JP 58014441A JP 1444183 A JP1444183 A JP 1444183A JP S59141753 A JPS59141753 A JP S59141753A
Authority
JP
Japan
Prior art keywords
deflector
exhaust
thrust
exhaust passage
turbine engine
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
JP58014441A
Other languages
English (en)
Japanese (ja)
Other versions
JPS6360222B2 (enExample
Inventor
Shigeru Horinouchi
茂 堀之内
Atsushi Tanaka
敦 田中
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.)
Subaru Corp
Original Assignee
Fuji Jukogyo KK
Fuji Heavy Industries Ltd
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 Fuji Jukogyo KK, Fuji Heavy Industries Ltd filed Critical Fuji Jukogyo KK
Priority to JP58014441A priority Critical patent/JPS59141753A/ja
Priority to DE8484300436T priority patent/DE3463821D1/de
Priority to EP84300436A priority patent/EP0118181B1/en
Priority to US06/574,495 priority patent/US4587804A/en
Publication of JPS59141753A publication Critical patent/JPS59141753A/ja
Publication of JPS6360222B2 publication Critical patent/JPS6360222B2/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
    • F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
  • Exhaust Silencers (AREA)
JP58014441A 1983-01-31 1983-01-31 Ｖ／ｓｔｏｌ機用推力増大偏向装置 Granted JPS59141753A (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP58014441A JPS59141753A (ja) 1983-01-31 1983-01-31 Ｖ／ｓｔｏｌ機用推力増大偏向装置
DE8484300436T DE3463821D1 (en) 1983-01-31 1984-01-25 Device for increasing and deflecting thrust of jet-propulsion engine of v/stol aircraft
EP84300436A EP0118181B1 (en) 1983-01-31 1984-01-25 Device for increasing and deflecting thrust of jet-propulsion engine of v/stol aircraft
US06/574,495 US4587804A (en) 1983-01-31 1984-01-27 Device for increasing and deflecting thrust of jet-propulsion engine of V/STOL aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58014441A JPS59141753A (ja) 1983-01-31 1983-01-31 Ｖ／ｓｔｏｌ機用推力増大偏向装置

Publications (2)

Publication Number Publication Date
JPS59141753A true JPS59141753A (ja) 1984-08-14
JPS6360222B2 JPS6360222B2 (enExample) 1988-11-22

Family

ID=11861111

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58014441A Granted JPS59141753A (ja) 1983-01-31 1983-01-31 Ｖ／ｓｔｏｌ機用推力増大偏向装置

Country Status (4)

Country Link
US (1) US4587804A (enExample)
EP (1) EP0118181B1 (enExample)
JP (1) JPS59141753A (enExample)
DE (1) DE3463821D1 (enExample)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63162955A (ja) * 1986-12-26 1988-07-06 Fuji Heavy Ind Ltd ナセル格納式エジエクタ
US4898343A (en) * 1987-12-25 1990-02-06 Fuji Jukogyo Kabushiki Kaisha Thrust-deflecting vane device of V/STOL aircraft
WO2011064962A1 (ja) * 2009-11-25 2011-06-03 ナブテスコ株式会社 鉄道車両用非常ブレーキ装置、鉄道車両用非常ブレーキシステム、及び鉄道車両用非常ブレーキ装置を備えた鉄道車両
CN107618654A (zh) * 2017-08-03 2018-01-23 南京航空航天大学 飞行器姿态控制系统及其控制方法、控制喷嘴

Families Citing this family (19)

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Publication number Priority date Publication date Assignee Title
GB2323065B (en) * 1993-03-13 1998-12-09 Rolls Royce Plc Vectorable nozzle for aircraft
GB2281262B (en) * 1993-08-27 1997-04-16 Rolls Royce Plc Stowable nozzle
RU2116223C1 (ru) * 1994-10-04 1998-07-27 ОЛЕЙНОВ Геннадий Александрович Устройство для улучшения аэрогидродинамических качеств конструкций
US5680755A (en) * 1995-09-25 1997-10-28 General Electric Company Convertible ejector selectively cooled thrust vectoring exhaust nozzle
RU2150593C1 (ru) * 1999-03-29 2000-06-10 Акционерное общество закрытого типа "Энерготех" Эжекторный усилитель тяги газотурбинного двигателя
US6382559B1 (en) 1999-08-13 2002-05-07 Rolls-Royce Corporation Thrust vectoring mechanism
RU2194873C2 (ru) * 2000-05-06 2002-12-20 Казанская государственная архитектурно-строительная академия Ракетный двигатель
US6918244B2 (en) * 2001-08-17 2005-07-19 John Eugene Dickau Vertical takeoff and landing aircraft propulsion systems
US6694723B2 (en) * 2002-03-27 2004-02-24 United Technologies Corporation Valve assembly for gas turbine engine
US20040244633A1 (en) * 2003-05-08 2004-12-09 Witmer Warner H. Cats-constrained airplane transportation system
US20070018034A1 (en) * 2005-07-12 2007-01-25 Dickau John E Thrust vectoring
JP2009029400A (ja) * 2007-06-22 2009-02-12 Toyota Motor Corp 飛翔体
RU2405977C1 (ru) * 2009-07-09 2010-12-10 Открытое Акционерное Общество "Научно-Исследовательский Институт Металлургической Теплотехники Оао "Вниимт" Способ пламенно-струйного эжектирования
US20160258358A1 (en) * 2015-03-02 2016-09-08 Sikorsky Aircraft Corporation High turning angle ejector cooled turbine engine exhaust duct
US11965456B2 (en) * 2015-09-02 2024-04-23 Jetoptera, Inc. Fluidic turbo heater system
US11258333B2 (en) * 2019-07-29 2022-02-22 Aurora Flight Sciences Corporation Propulsor system with integrated passive cooling
US20220144422A1 (en) * 2020-10-26 2022-05-12 Hugh Bryan Welcel Modular Device For Propulsion In A Vehicle
US11732626B2 (en) * 2021-12-28 2023-08-22 Honda Motor Co., Ltd. Mixer and mobile body
CN114576035B (zh) * 2022-01-13 2024-01-30 中国航发沈阳发动机研究所 一种可旋转式马达长距可调引气喷管

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2951660A (en) * 1956-06-25 1960-09-06 James V Giliberty Method and means for controlling the jet thrust of an aircraft
DE1119126B (de) * 1960-03-18 1961-12-07 Bmw Triebwerkbau Ges M B H Strahltriebwerk mit einer Strahlumlenkeinrichtung
FR1279495A (fr) * 1960-11-10 1961-12-22 Snecma Dispositif de déviation de jet pour avion à réaction
FR1283690A (fr) * 1961-03-15 1962-02-02 B M W Triebwerkbau Ges M B H Réacteur pour la propulsion d'avions
US3178887A (en) * 1963-01-21 1965-04-20 Rolls Royce Pivotal nozzle deflector for jet lift engine
US3380660A (en) * 1966-04-28 1968-04-30 United Aircraft Corp Variable area exhaust deflector
US3527408A (en) * 1968-06-06 1970-09-08 United Aircraft Corp Curved exhaust deflection system
GB1395709A (en) * 1971-07-06 1975-05-29 Rolls Royce Jet propulsion power plant
US3979067A (en) * 1975-04-28 1976-09-07 General Electric Company Actuating means for a thrust vectoring gas turbine engine exhaust nozzle
US4000612A (en) * 1975-07-28 1977-01-04 General Electric Company Cooling system for a thrust vectoring gas turbine engine exhaust system
GB1550633A (en) * 1976-07-21 1979-08-15 Gen Electric Thrust-vectoring gas turbine engine exhaust nozzles
US4222234A (en) * 1977-07-25 1980-09-16 General Electric Company Dual fan engine for VTOL pitch control
US4295332A (en) * 1978-11-13 1981-10-20 General Electric Company Infrared suppressor system
US4392615A (en) * 1981-05-11 1983-07-12 United Technologies Corporation Viol exhaust nozzle with veer flap extension

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63162955A (ja) * 1986-12-26 1988-07-06 Fuji Heavy Ind Ltd ナセル格納式エジエクタ
US4898343A (en) * 1987-12-25 1990-02-06 Fuji Jukogyo Kabushiki Kaisha Thrust-deflecting vane device of V/STOL aircraft
WO2011064962A1 (ja) * 2009-11-25 2011-06-03 ナブテスコ株式会社 鉄道車両用非常ブレーキ装置、鉄道車両用非常ブレーキシステム、及び鉄道車両用非常ブレーキ装置を備えた鉄道車両
CN107618654A (zh) * 2017-08-03 2018-01-23 南京航空航天大学 飞行器姿态控制系统及其控制方法、控制喷嘴

Also Published As

Publication number Publication date
EP0118181B1 (en) 1987-05-20
JPS6360222B2 (enExample) 1988-11-22
US4587804A (en) 1986-05-13
EP0118181A1 (en) 1984-09-12
DE3463821D1 (en) 1987-06-25

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