KR880013767A - 축회전 조절 날개를 지니는 면적조절 및 추력 벡터링 날개캐스케이드 - Google Patents

축회전 조절 날개를 지니는 면적조절 및 추력 벡터링 날개캐스케이드

Info

Publication number
KR880013767A
KR880013767A KR1019880006051A KR880006051A KR880013767A KR 880013767 A KR880013767 A KR 880013767A KR 1019880006051 A KR1019880006051 A KR 1019880006051A KR 880006051 A KR880006051 A KR 880006051A KR 880013767 A KR880013767 A KR 880013767A
Authority
KR
South Korea
Prior art keywords
thrust
control
blades
vectoring
area
Prior art date
Application number
KR1019880006051A
Other languages
English (en)
Other versions
KR960003685B1 (ko
Inventor
보이드 도이어 에드워드
러셀 스코트 필립
알프레드 로우츠 토마스
Original Assignee
유나이티드 테크놀로지스 코오포레이숀
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 유나이티드 테크놀로지스 코오포레이숀 filed Critical 유나이티드 테크놀로지스 코오포레이숀
Publication of KR880013767A publication Critical patent/KR880013767A/ko
Application granted granted Critical
Publication of KR960003685B1 publication Critical patent/KR960003685B1/ko

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
    • 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/62—Reversing jet main flow by blocking the rearward discharge by means of 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
    • 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)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
KR1019880006051A 1987-05-22 1988-05-21 축회전 조절 날개를 지니는 면적조절 및 추력 벡터링 날개캐스케이드 KR960003685B1 (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/053,282 US4798328A (en) 1987-05-22 1987-05-22 Area controlled, thrust vectoring vane cascade with nutating control vane
US053,282 1987-05-22

Publications (2)

Publication Number Publication Date
KR880013767A true KR880013767A (ko) 1988-12-21
KR960003685B1 KR960003685B1 (ko) 1996-03-21

Family

ID=21983132

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1019880006051A KR960003685B1 (ko) 1987-05-22 1988-05-21 축회전 조절 날개를 지니는 면적조절 및 추력 벡터링 날개캐스케이드

Country Status (5)

Country Link
US (1) US4798328A (ko)
EP (1) EP0292421B1 (ko)
KR (1) KR960003685B1 (ko)
CN (1) CN1028051C (ko)
DE (1) DE3870032D1 (ko)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1989012741A1 (en) * 1989-08-21 1989-12-28 Moog Inc. Vane-type thrust vectoring nozzle
US5255850A (en) * 1992-06-29 1993-10-26 The United States Of America As Represented By The Secretary Of The Air Force Pivoting flaps and vane pack in a nozzle reverser assembly
CN2188544Y (zh) * 1994-04-09 1995-02-01 卢杲 飞碟
US5485958A (en) * 1994-06-06 1996-01-23 Rolls-Royce, Incorporated Mechanism for operating a cascade of variable pitch vanes
DE4426195C2 (de) * 1994-07-23 1998-02-05 Daimler Benz Aerospace Ag Schubdüse in Rechteckbauweise für Strahltriebwerke
US6318668B1 (en) 1996-08-02 2001-11-20 Allison Advanced Development Company Thrust vectoring techniques
US6105901A (en) * 1996-08-02 2000-08-22 Allison Engine Co., Inc. Thrust vectoring system
US6382559B1 (en) 1999-08-13 2002-05-07 Rolls-Royce Corporation Thrust vectoring mechanism
US6311928B1 (en) 2000-01-05 2001-11-06 Stage Iii Technologies, L.C. Jet engine cascade thrust reverser for use with mixer/ejector noise suppressor
CN100436837C (zh) * 2005-10-25 2008-11-26 西北工业大学 一种提高气动稳定性的叶栅布局
US7836681B2 (en) * 2006-06-13 2010-11-23 Rolls-Royce Corporation Mechanism for a vectoring exhaust nozzle
US7926290B2 (en) * 2006-12-18 2011-04-19 General Electric Company Turbine engine with modulated flow fan and method of operation
US20110167792A1 (en) * 2009-09-25 2011-07-14 James Edward Johnson Adaptive engine
US20110167791A1 (en) * 2009-09-25 2011-07-14 James Edward Johnson Convertible fan engine
EP2813696B1 (de) * 2013-06-12 2015-12-02 MTU Aero Engines GmbH Schubumlenkvorrichtung sowie Flugtriebwerk
CN103692899A (zh) * 2013-12-23 2014-04-02 北京二七轨道交通装备有限责任公司 电动轮自卸车后桥门及电动轮自卸车
CN104033282B (zh) * 2014-06-09 2016-05-04 中国航空工业集团公司沈阳发动机设计研究所 一种具有反推力功能的二元收敛喷管
JP6361404B2 (ja) * 2014-09-17 2018-07-25 三菱重工業株式会社 推力偏向装置、および、推力偏向装置を備える飛しょう体
US9874176B2 (en) * 2015-01-14 2018-01-23 The Boeing Company Methods and apparatus to vary reverse thrust of aircraft engines
US10018151B2 (en) 2015-01-14 2018-07-10 The Boeing Company Methods and apparatus to vary reverse thrust of aircraft engines
US10077740B2 (en) * 2015-10-16 2018-09-18 The Boeing Company Folding door thrust reversers for aircraft engines
US10343786B2 (en) * 2017-06-28 2019-07-09 General Electric Company System and method of operating a ducted fan propulsion system during aircraft taxi
US11338926B2 (en) * 2018-08-10 2022-05-24 Rolls-Royce North American Technologies Inc. Aircraft with electric propulsor
FR3115837A1 (fr) * 2020-11-03 2022-05-06 Safran Aircraft Engines Ensemble pour turbomachine d’aeronef a double flux, l’ensemble etant equipe d’ailettes de decharge d’air pilotees en incidence

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3025667A (en) * 1957-07-22 1962-03-20 Boeing Co Rotary turret reversible thrust noise suppression jet engine nozzles
US3100377A (en) * 1960-11-14 1963-08-13 Northrop Corp Deflecting means for jet aircraft and the like
US3081597A (en) * 1960-12-06 1963-03-19 Northrop Corp Variable thrust vectoring systems defining convergent nozzles
US3174709A (en) * 1962-11-29 1965-03-23 Gen Electric Vectorable thrust mechanism
US3335960A (en) * 1965-03-04 1967-08-15 Gen Electric Louver actuation system
US3344604A (en) * 1965-12-14 1967-10-03 Gen Dynamics Corp Apparatus for selectively reversing the thrust of front fan jet engines
US3380661A (en) * 1966-04-12 1968-04-30 United Aircraft Corp Thrust deflector
US3601992A (en) * 1970-06-10 1971-08-31 Rohr Corp Thrust reversing apparatus
US3739582A (en) * 1972-04-13 1973-06-19 Rohr Industries Inc Thrust reversing apparatus
US4073440A (en) * 1976-04-29 1978-02-14 The Boeing Company Combination primary and fan air thrust reversal control systems for long duct fan jet engines
US4183478A (en) * 1977-11-25 1980-01-15 The Boeing Company Jet thrust reverser
US4241647A (en) * 1979-08-20 1980-12-30 Dayco Corporation Air damper valve
GB2155552B (en) * 1981-02-24 1986-02-26 Rolls Royce Adjustable jet propulsion nozzle
US4753392A (en) * 1984-11-02 1988-06-28 United Technologies Corporation Two dimensional gas turbine engine exhaust nozzle

Also Published As

Publication number Publication date
EP0292421B1 (en) 1992-04-15
CN1028051C (zh) 1995-03-29
EP0292421A3 (en) 1989-11-15
US4798328A (en) 1989-01-17
KR960003685B1 (ko) 1996-03-21
EP0292421A2 (en) 1988-11-23
DE3870032D1 (de) 1992-05-21
CN1032217A (zh) 1989-04-05

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