IL129287A - Adjustable axial nozzle operating system with multiple power control circuits - Google Patents

Adjustable axial nozzle operating system with multiple power control circuits

Info

Publication number
IL129287A
IL129287A IL12928796A IL12928796A IL129287A IL 129287 A IL129287 A IL 129287A IL 12928796 A IL12928796 A IL 12928796A IL 12928796 A IL12928796 A IL 12928796A IL 129287 A IL129287 A IL 129287A
Authority
IL
Israel
Prior art keywords
actuators
vectoring
failsafe
nozzle
actuating system
Prior art date
Application number
IL12928796A
Other languages
English (en)
Hebrew (he)
Other versions
IL129287A0 (en
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IL129287A0 publication Critical patent/IL129287A0/xx
Publication of IL129287A publication Critical patent/IL129287A/en

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
    • F02K1/008—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 in any rearward direction
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • F02K1/15—Control or regulation
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Control Of Turbines (AREA)
IL12928796A 1995-04-13 1996-10-16 Adjustable axial nozzle operating system with multiple power control circuits IL129287A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/422,731 US5740988A (en) 1995-04-13 1995-04-13 Axisymmetric vectoring nozzle actuating system having multiple power control circuits
PCT/US1996/016406 WO1998016732A1 (fr) 1995-04-13 1996-10-16 Systeme de commande d'une tuyere d'ejection axisymetrique, dote de plusieurs circuits de commande d'energie

Publications (2)

Publication Number Publication Date
IL129287A0 IL129287A0 (en) 2000-02-17
IL129287A true IL129287A (en) 2001-10-31

Family

ID=23676115

Family Applications (1)

Application Number Title Priority Date Filing Date
IL12928796A IL129287A (en) 1995-04-13 1996-10-16 Adjustable axial nozzle operating system with multiple power control circuits

Country Status (9)

Country Link
US (1) US5740988A (fr)
EP (1) EP0932755B1 (fr)
JP (1) JP3884482B2 (fr)
KR (1) KR100432405B1 (fr)
DE (1) DE69627713T2 (fr)
ES (1) ES2197251T3 (fr)
IL (1) IL129287A (fr)
TW (1) TW353698B (fr)
WO (1) WO1998016732A1 (fr)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6318668B1 (en) 1996-08-02 2001-11-20 Allison Advanced Development Company Thrust vectoring techniques
US6109021A (en) * 1998-07-22 2000-08-29 General Electric Company Vectoring nozzle calibration
US6382559B1 (en) 1999-08-13 2002-05-07 Rolls-Royce Corporation Thrust vectoring mechanism
GB0120747D0 (en) * 2001-08-25 2001-10-17 Lucas Western Inc Control method
US7587899B2 (en) * 2004-08-27 2009-09-15 University Of Houston Shape memory alloy actuated adaptive exhaust nozzle for jet engine
CN100523472C (zh) * 2006-02-24 2009-08-05 同济大学 一种轴对称矢量喷管a9作动应急复位液压系统
CN100480500C (zh) * 2006-02-24 2009-04-22 同济大学 一种轴对称矢量喷管a9/a8面积比失调防护液压系统
US8347601B2 (en) * 2006-05-04 2013-01-08 Volvo Aero Corporation Device for pivoting at least one pivotable element in a gas turbine engine
US9719370B2 (en) * 2007-03-30 2017-08-01 United Technologies Corporation Linkage system with wear reduction
JP5604856B2 (ja) * 2009-11-18 2014-10-15 富士通株式会社 制御装置、制御方法および制御プログラム
RU2504815C2 (ru) * 2011-02-09 2014-01-20 Николай Евгеньевич Староверов Способ управления самолетом и устройство для его осуществления
RU2553614C1 (ru) * 2014-01-17 2015-06-20 Николай Евгеньевич Староверов Способ управления самолётом с двумя и более двигателями-2
KR102006845B1 (ko) 2019-04-18 2019-08-05 주식회사 스틸티앤씨 산화방지용 전극봉 코팅시스템
US10837402B2 (en) 2020-01-09 2020-11-17 Guanhao Wu Thrust vector nozzle
US11772809B2 (en) 2021-11-27 2023-10-03 Airbus Defence and Space GmbH Fuselage for an aircraft with fuselage-integrated tailplane

Family Cites Families (28)

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Publication number Priority date Publication date Assignee Title
US2272725A (en) * 1939-07-13 1942-02-10 Glenn L Martin Co Control of aircraft surfaces
US2834182A (en) * 1955-06-21 1958-05-13 Charles H Culbertson High altitude compensation of two position exhaust nozzle control
US3138002A (en) * 1961-04-07 1964-06-23 Snecma Safety device, especially for aircraft servo-controls
US3171618A (en) * 1963-01-30 1965-03-02 Honeywell Inc Signal selector for control apparatus
US3136504A (en) * 1963-07-02 1964-06-09 William F Carr Electrical primary flight control system
US3554084A (en) * 1967-11-17 1971-01-12 Honeywell Inc Redundant force summing servo unit
GB1288302A (fr) * 1969-11-01 1972-09-06
US3612400A (en) * 1970-06-02 1971-10-12 Gen Motors Corp Variable jet propulsion nozzle
US3806063A (en) * 1971-10-08 1974-04-23 Chandler Evans Inc Thrust vector steering techniques and apparatus
US4000854A (en) * 1975-10-02 1977-01-04 General Electric Company Thrust vectorable exhaust nozzle
US4030291A (en) * 1976-01-02 1977-06-21 General Electric Company Thrust reverser for a gas turbofan engine
US4128208A (en) * 1977-07-11 1978-12-05 General Electric Company Exhaust nozzle flap seal arrangement
US4718647A (en) * 1980-02-20 1988-01-12 Avm, Inc. Pneumatic counterbalance with dual force
US4428196A (en) * 1980-10-14 1984-01-31 Mcdonnell Douglas Corporation Aircraft split hydraulic system
US4807517A (en) * 1982-09-30 1989-02-28 Allied-Signal Inc. Electro-hydraulic proportional actuator
US4805515A (en) * 1983-11-18 1989-02-21 General Electric Company Fail-safe servovalve system
US4538504A (en) * 1983-11-18 1985-09-03 General Electric Company Fail-safe servovalve system
US4711089A (en) * 1984-07-16 1987-12-08 The Boeing Company Hydraulic system for aircraft
US4704865A (en) * 1984-07-16 1987-11-10 The Boeing Company Hydraulic reserve system for aircraft
US5074495A (en) * 1987-12-29 1991-12-24 The Boeing Company Load-adaptive hybrid actuator system and method for actuating control surfaces
US5115720A (en) * 1990-04-02 1992-05-26 Baker Material Handling Corporation Hydraulic valve bank
US5011080A (en) * 1990-04-18 1991-04-30 United Technologies Corporation Convergent/divergent nozzle construction
US5261605A (en) * 1990-08-23 1993-11-16 United Technologies Corporation Axisymmetric nozzle with gimbled unison ring
US5174502A (en) * 1991-05-10 1992-12-29 General Electric Company Support for a translating nozzle vectoring ring
US5279107A (en) * 1992-06-30 1994-01-18 United Technologies Corporation Fuel control system with fuel metering valve fault accommodation
US5215257A (en) * 1992-07-16 1993-06-01 United Technologies Corporation Divergent seal arrangement for a convergent/divergent nozzle
US5267436A (en) * 1992-09-28 1993-12-07 United Technologies Corporation Vectoring nozzle control of gas turbine engines
US5335489A (en) * 1993-07-09 1994-08-09 United Technologies Corporation Gas turbine vectoring exhaust nozzle

Also Published As

Publication number Publication date
IL129287A0 (en) 2000-02-17
JP3884482B2 (ja) 2007-02-21
WO1998016732A1 (fr) 1998-04-23
KR20000049112A (ko) 2000-07-25
JP2001505636A (ja) 2001-04-24
US5740988A (en) 1998-04-21
EP0932755A1 (fr) 1999-08-04
DE69627713D1 (de) 2003-05-28
TW353698B (en) 1999-03-01
KR100432405B1 (ko) 2004-05-22
ES2197251T3 (es) 2004-01-01
DE69627713T2 (de) 2004-02-26
EP0932755B1 (fr) 2003-04-23

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