CA2789438A1 - Articulating slider track - Google Patents

Articulating slider track Download PDF

Info

Publication number
CA2789438A1
CA2789438A1 CA2789438A CA2789438A CA2789438A1 CA 2789438 A1 CA2789438 A1 CA 2789438A1 CA 2789438 A CA2789438 A CA 2789438A CA 2789438 A CA2789438 A CA 2789438A CA 2789438 A1 CA2789438 A1 CA 2789438A1
Authority
CA
Canada
Prior art keywords
cowl member
slider track
cowl
stowed position
fan nozzle
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.)
Abandoned
Application number
CA2789438A
Other languages
English (en)
French (fr)
Inventor
Alan Roy Stuart
John Robert Fehrmann
Melanie Zoe Cox
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of CA2789438A1 publication Critical patent/CA2789438A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • 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
    • F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
    • 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
    • F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
    • 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
    • F02K1/10—Varying effective area of jet pipe or nozzle by distorting the jet pipe or nozzle
    • 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
    • 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
    • F02K1/78—Other construction of jet pipes
    • F02K1/80—Couplings or connections

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CA2789438A 2010-02-15 2011-02-11 Articulating slider track Abandoned CA2789438A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US30474110P 2010-02-15 2010-02-15
US61/304,741 2010-02-15
PCT/US2011/024517 WO2011142866A2 (en) 2010-02-15 2011-02-11 Articulating slider track

Publications (1)

Publication Number Publication Date
CA2789438A1 true CA2789438A1 (en) 2011-11-17

Family

ID=44545867

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2789438A Abandoned CA2789438A1 (en) 2010-02-15 2011-02-11 Articulating slider track

Country Status (5)

Country Link
US (1) US20130202402A1 (ja)
EP (1) EP2536941A2 (ja)
JP (1) JP5782463B2 (ja)
CA (1) CA2789438A1 (ja)
WO (1) WO2011142866A2 (ja)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10247136B2 (en) 2015-12-03 2019-04-02 General Electric Company Thrust reverser system for a gas turbine engine

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1234099B (de) * 1965-09-15 1967-02-09 Gen Electric Ringfoermige konvergent-divergente Schubduese
US4132068A (en) * 1975-04-30 1979-01-02 The United States Of America As Represented By The United States National Aeronautics And Space Administration Variable area exhaust nozzle
US4184807A (en) * 1978-07-10 1980-01-22 Berg George W Reversible hydraulic engine
FR2457390A1 (fr) * 1979-05-23 1980-12-19 Europ Propulsion Divergent deployable de tuyere pour propulseur fusee
FR2496766A1 (fr) * 1980-12-23 1982-06-25 Snecma Dispositif de guidage de carenage mobile d'un systeme d'inversion de poussee
EP0109219A3 (en) * 1982-11-12 1985-11-13 LUCAS INDUSTRIES public limited company Thrust reversing apparatus for a gas turbine engine
JPH09195853A (ja) * 1995-12-14 1997-07-29 United Technol Corp <Utc> 可変面積ファンエキゾーストノズル
FR2748779B1 (fr) * 1996-05-15 1998-06-19 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes associees a un panneau amont
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
US6584763B2 (en) * 2001-08-01 2003-07-01 Rohr, Inc. Lock for the translating sleeve of a turbofan engine thrust reverser
FR2868131B1 (fr) * 2004-03-25 2006-06-09 Airbus France Sas Tuyere primaire a chevrons pour turboreacteur a double flux d'aeronef et aeronef comportant une telle tuyere
US7886518B2 (en) * 2006-11-14 2011-02-15 General Electric Company Turbofan engine cowl assembly and method of operating the same
US8127531B2 (en) * 2008-11-11 2012-03-06 The Boeing Company Radially translating fan nozzle nacelle
US8127532B2 (en) * 2008-11-26 2012-03-06 The Boeing Company Pivoting fan nozzle nacelle
US20110120078A1 (en) * 2009-11-24 2011-05-26 Schwark Jr Fred W Variable area fan nozzle track
US8443586B2 (en) * 2009-11-24 2013-05-21 United Technologies Corporation Variable area fan nozzle bearing track
US9303590B2 (en) * 2012-05-22 2016-04-05 Spirit Aerosystems, Inc. Variable area fan nozzle actuation system

Also Published As

Publication number Publication date
WO2011142866A2 (en) 2011-11-17
WO2011142866A3 (en) 2012-01-19
JP5782463B2 (ja) 2015-09-24
EP2536941A2 (en) 2012-12-26
JP2013519823A (ja) 2013-05-30
US20130202402A1 (en) 2013-08-08

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Legal Events

Date Code Title Description
EEER Examination request

Effective date: 20151211

FZDE Discontinued

Effective date: 20180213