JP6087068B2 - ジェットエンジンノズルの流れ変更部品をリニア駆動する装置および方法 - Google Patents

ジェットエンジンノズルの流れ変更部品をリニア駆動する装置および方法 Download PDF

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Publication number
JP6087068B2
JP6087068B2 JP2012135276A JP2012135276A JP6087068B2 JP 6087068 B2 JP6087068 B2 JP 6087068B2 JP 2012135276 A JP2012135276 A JP 2012135276A JP 2012135276 A JP2012135276 A JP 2012135276A JP 6087068 B2 JP6087068 B2 JP 6087068B2
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Japan
Prior art keywords
chevron
cowl
linear actuator
jet engine
flow path
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Expired - Fee Related
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JP2012135276A
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Japanese (ja)
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JP2013002447A (ja
JP2013002447A5 (enExample
Inventor
デイビッド・パトリック・カルダー
パピンダー・ブティアーニ
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General Electric Co
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General Electric Co
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    • 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
    • F02K1/38—Introducing air inside the jet
    • F02K1/383—Introducing air inside the jet with retractable elements
    • 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
    • F02K1/38—Introducing air inside the jet
    • F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
    • 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
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Nozzles (AREA)
  • Fuel-Injection Apparatus (AREA)
JP2012135276A 2011-06-17 2012-06-15 ジェットエンジンノズルの流れ変更部品をリニア駆動する装置および方法 Expired - Fee Related JP6087068B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/163,463 US8613398B2 (en) 2011-06-17 2011-06-17 Apparatus and methods for linear actuation of flow altering components of jet engine nozzle
US13/163,463 2011-06-17

Publications (3)

Publication Number Publication Date
JP2013002447A JP2013002447A (ja) 2013-01-07
JP2013002447A5 JP2013002447A5 (enExample) 2015-07-30
JP6087068B2 true JP6087068B2 (ja) 2017-03-01

Family

ID=46318981

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012135276A Expired - Fee Related JP6087068B2 (ja) 2011-06-17 2012-06-15 ジェットエンジンノズルの流れ変更部品をリニア駆動する装置および方法

Country Status (6)

Country Link
US (1) US8613398B2 (enExample)
EP (1) EP2535547B2 (enExample)
JP (1) JP6087068B2 (enExample)
CN (1) CN102828850B (enExample)
BR (1) BR102012014640A8 (enExample)
CA (1) CA2779811C (enExample)

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US9328695B2 (en) * 2006-10-12 2016-05-03 United Technologies Corporation Variable fan nozzle using shape memory material
US9551295B2 (en) * 2012-07-24 2017-01-24 Rohr, Inc. Variable area fan nozzle position and skew sensing
US9989009B2 (en) 2012-10-31 2018-06-05 The Boeing Company Methods and apparatus for sealing variable area fan nozzles of jet engines
FR3000994A1 (fr) * 2013-01-16 2014-07-18 Aircelle Sa Tuyere de nacelle a dispositifs de regulation de pression
GB2510635B (en) * 2013-02-12 2017-11-01 Ge Aviat Systems Ltd Method for predicting faults in an aircraft thrust reverser system
WO2014197030A2 (en) * 2013-03-12 2014-12-11 United Technologies Corporation Expanding shell flow control device
US9581145B2 (en) * 2013-05-14 2017-02-28 The Boeing Company Shape memory alloy actuation system for variable area fan nozzle
CN106364653A (zh) * 2016-08-31 2017-02-01 何洪波 全垫升气垫船
FR3075760B1 (fr) * 2017-12-21 2020-01-31 Safran Nacelles Nacelle de moteur d’aeronef
US10906661B2 (en) * 2018-11-05 2021-02-02 Rohr, Inc. Nacelle cowl hinge
US11440671B2 (en) * 2019-01-24 2022-09-13 Amazon Technologies, Inc. Adjustable motor fairings for aerial vehicles
CN110439707B (zh) * 2019-07-26 2021-10-01 中国航发沈阳发动机研究所 一种飞机尾部弹性片组件
FR3102148B1 (fr) * 2019-10-16 2022-07-01 Safran Système propulsif pour un aéronef
US11834189B2 (en) * 2020-04-09 2023-12-05 Gulfstream Aerospace Corporation Exhaust nozzle assembly, propulsion system employing the exhaust nozzle assembly, and aircraft employing the propulsion system
US12018838B2 (en) 2022-06-21 2024-06-25 General Electric Company Cowl assembly for a gas turbine engine
US12442333B1 (en) 2024-10-09 2025-10-14 General Electric Company Turbine engine having a variable engine intake system
US12435666B1 (en) * 2024-10-09 2025-10-07 General Electric Company Turbine engine having a variable engine intake system

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GB1008322A (en) * 1964-08-04 1965-10-27 Rolls Royce Gas turbine engine
US3449914A (en) * 1967-12-21 1969-06-17 United Aircraft Corp Variable flow turbofan engine
US3829020A (en) 1973-06-13 1974-08-13 Boeing Co Translating sleeve variable area nozzle and thrust reverser
US3931708A (en) 1973-10-11 1976-01-13 United Technologies Corporation Variable flap for a variable pitch ducted fan propulsor
US4533098A (en) † 1983-06-20 1985-08-06 General Electric Company Thrust reverser attachment
US5261229A (en) * 1992-08-03 1993-11-16 General Electric Company Noise-suppressed exhaust nozzles for jet engines
GB2308866B (en) 1996-01-04 1999-09-08 Rolls Royce Plc Ducted fan gas turbine engine with secondary duct
US6318070B1 (en) 2000-03-03 2001-11-20 United Technologies Corporation Variable area nozzle for gas turbine engines driven by shape memory alloy actuators
GB2372779A (en) 2001-03-03 2002-09-04 Rolls Royce Plc Gas turbine engine nozzle with noise reducing tabs
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US6718752B2 (en) 2002-05-29 2004-04-13 The Boeing Company Deployable segmented exhaust nozzle for a jet engine
US7458221B1 (en) 2003-10-23 2008-12-02 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Variable area nozzle including a plurality of convexly vanes with a crowned contour, in a vane to vane sealing arrangement and with nonuniform lengths
US7174704B2 (en) * 2004-07-23 2007-02-13 General Electric Company Split shroud exhaust nozzle
US7340883B2 (en) * 2004-11-12 2008-03-11 The Boeing Company Morphing structure
US7216831B2 (en) * 2004-11-12 2007-05-15 The Boeing Company Shape changing structure
US8235325B2 (en) 2005-10-04 2012-08-07 United Technologies Corporation Fan variable area nozzle positional measurement system
US7721551B2 (en) 2006-06-29 2010-05-25 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle
FR2904372B1 (fr) * 2006-07-26 2008-10-31 Snecma Sa Tuyere d'ejection des gaz pour turbomachine a double flux ayant une section d'ejection ou de col variable par deplacement du capot secondaire
GB0618072D0 (en) 2006-09-14 2006-10-25 Rolls Royce Plc Aeroengine nozzle
US7966828B2 (en) 2007-01-08 2011-06-28 United Technologies Corporation Variable area nozzle with woven sleeve extension
US7721549B2 (en) 2007-02-08 2010-05-25 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system
US7966827B2 (en) 2007-05-31 2011-06-28 United Technologies Corporation Gas turbine engine with fan variable area nozzle having a rotational valve system
US8074440B2 (en) 2007-08-23 2011-12-13 United Technologies Corporation Gas turbine engine with axial movable fan variable area nozzle
US8006479B2 (en) 2007-10-15 2011-08-30 United Technologies Corporation Thrust reversing variable area nozzle
FR2928183A1 (fr) * 2008-02-29 2009-09-04 Aircelle Sa Dispositif de reduction de bruit pour moteur d'aeronef, du type a chevrons mobiles
FR2934875B1 (fr) * 2008-08-06 2010-08-13 Aircelle Sa Nacelle de turboreacteur a chevrons mobiles.
JP5486231B2 (ja) * 2009-07-27 2014-05-07 カヤバ工業株式会社 リニアアクチュエータ

Also Published As

Publication number Publication date
BR102012014640A2 (pt) 2014-01-07
CA2779811C (en) 2019-08-20
US8613398B2 (en) 2013-12-24
BR102012014640A8 (pt) 2018-05-15
EP2535547A3 (en) 2013-08-21
JP2013002447A (ja) 2013-01-07
EP2535547B1 (en) 2016-03-30
CA2779811A1 (en) 2012-12-17
EP2535547B2 (en) 2022-08-24
US20120321456A1 (en) 2012-12-20
CN102828850B (zh) 2016-12-21
EP2535547A2 (en) 2012-12-19
CN102828850A (zh) 2012-12-19

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