JP2013002447A5 - - Google Patents

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Publication number
JP2013002447A5
JP2013002447A5 JP2012135276A JP2012135276A JP2013002447A5 JP 2013002447 A5 JP2013002447 A5 JP 2013002447A5 JP 2012135276 A JP2012135276 A JP 2012135276A JP 2012135276 A JP2012135276 A JP 2012135276A JP 2013002447 A5 JP2013002447 A5 JP 2013002447A5
Authority
JP
Japan
Prior art keywords
chevron
cowl
linear actuator
coupled
housing
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
JP2012135276A
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English (en)
Japanese (ja)
Other versions
JP2013002447A (ja
JP6087068B2 (ja
Filing date
Publication date
Priority claimed from US13/163,463 external-priority patent/US8613398B2/en
Application filed filed Critical
Publication of JP2013002447A publication Critical patent/JP2013002447A/ja
Publication of JP2013002447A5 publication Critical patent/JP2013002447A5/ja
Application granted granted Critical
Publication of JP6087068B2 publication Critical patent/JP6087068B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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 true JP2013002447A5 (enExample) 2015-07-30
JP6087068B2 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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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
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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

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