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FR2993026B1 - COUPLING AND DISMANTLING MECHANISM FOR AN ONBOARD DEVICE OF A TURBOREACTOR NACELLE - Google Patents

COUPLING AND DISMANTLING MECHANISM FOR AN ONBOARD DEVICE OF A TURBOREACTOR NACELLE

Info

Publication number
FR2993026B1
FR2993026B1 FR1256438A FR1256438A FR2993026B1 FR 2993026 B1 FR2993026 B1 FR 2993026B1 FR 1256438 A FR1256438 A FR 1256438A FR 1256438 A FR1256438 A FR 1256438A FR 2993026 B1 FR2993026 B1 FR 2993026B1
Authority
FR
France
Prior art keywords
coupling
onboard device
dismantling mechanism
turboreactor
nacelle
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.)
Expired - Fee Related
Application number
FR1256438A
Other languages
French (fr)
Other versions
FR2993026A1 (en
Inventor
Herve Hurlin
Olivier Gilo
Olivier Kerbler
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.)
Safran Nacelles SAS
Original Assignee
Aircelle SA
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
Priority to FR1256438A priority Critical patent/FR2993026B1/en
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to RU2015102973A priority patent/RU2015102973A/en
Priority to BR112014030828A priority patent/BR112014030828A2/en
Priority to CN201380035761.4A priority patent/CN104428520A/en
Priority to EP13744672.0A priority patent/EP2870349B1/en
Priority to PCT/FR2013/051554 priority patent/WO2014006321A1/en
Priority to CA2874578A priority patent/CA2874578A1/en
Publication of FR2993026A1 publication Critical patent/FR2993026A1/en
Application granted granted Critical
Publication of FR2993026B1 publication Critical patent/FR2993026B1/en
Priority to US14/558,833 priority patent/US20150083823A1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02K1/06—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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D11/00—Clutches in which the members have interengaging parts
    • F16D11/14—Clutches in which the members have interengaging parts with clutching members movable only axially
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/403—Transmission of power through the shape of the drive components
    • F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Braking Arrangements (AREA)
FR1256438A 2012-07-05 2012-07-05 COUPLING AND DISMANTLING MECHANISM FOR AN ONBOARD DEVICE OF A TURBOREACTOR NACELLE Expired - Fee Related FR2993026B1 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1256438A FR2993026B1 (en) 2012-07-05 2012-07-05 COUPLING AND DISMANTLING MECHANISM FOR AN ONBOARD DEVICE OF A TURBOREACTOR NACELLE
BR112014030828A BR112014030828A2 (en) 2012-07-05 2013-07-02 mechanism for coupling and uncoupling of an engine intake shaft and turbojet engine nacelle.
CN201380035761.4A CN104428520A (en) 2012-07-05 2013-07-02 Coupling and uncoupling mechanism for a turbojet engine nacelle onboard device
EP13744672.0A EP2870349B1 (en) 2012-07-05 2013-07-02 Clutching and declutching mechanism for an embarqued nacelle of a turbofan engine
RU2015102973A RU2015102973A (en) 2012-07-05 2013-07-02 CONNECTING AND DISCONNECTING MECHANISM FOR THE DEVICE OF THE TURBOREACTIVE ENGINE GONDOLA
PCT/FR2013/051554 WO2014006321A1 (en) 2012-07-05 2013-07-02 Coupling and uncoupling mechanism for a turbojet engine nacelle onboard device
CA2874578A CA2874578A1 (en) 2012-07-05 2013-07-02 Coupling and uncoupling mechanism for a turbojet engine nacelle onboard device
US14/558,833 US20150083823A1 (en) 2012-07-05 2014-12-03 Coupling and uncoupling mechanism for an onboard device of a turbojet engine nacelle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1256438A FR2993026B1 (en) 2012-07-05 2012-07-05 COUPLING AND DISMANTLING MECHANISM FOR AN ONBOARD DEVICE OF A TURBOREACTOR NACELLE

Publications (2)

Publication Number Publication Date
FR2993026A1 FR2993026A1 (en) 2014-01-10
FR2993026B1 true FR2993026B1 (en) 2014-08-22

Family

ID=46826787

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1256438A Expired - Fee Related FR2993026B1 (en) 2012-07-05 2012-07-05 COUPLING AND DISMANTLING MECHANISM FOR AN ONBOARD DEVICE OF A TURBOREACTOR NACELLE

Country Status (1)

Country Link
FR (1) FR2993026B1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3061528B1 (en) * 2016-12-30 2020-06-19 Safran Electronics & Defense PASSIVE LOCKED ACTUATOR
EP3563075B1 (en) * 2016-12-30 2022-01-26 Safran Electronics & Defense Actuator with passive locking

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4567965A (en) * 1982-03-22 1986-02-04 Allied Corporation Propeller brake
US5609020A (en) * 1995-05-15 1997-03-11 The Boeing Company Thrust reverser synchronization shaft lock
US6786039B2 (en) * 2001-09-07 2004-09-07 Honeywell International, Inc. Thrust reverser actuator with an automatic relock and lock drop prevention mechanism
US6487846B1 (en) * 2001-09-07 2002-12-03 Honeywell International, Inc. Thrust reverser actuator including an integrated locking mechanism
CN1501006A (en) * 2002-11-16 2004-06-02 Л Loop for axial and apparatus thereof
US7225607B2 (en) * 2004-08-27 2007-06-05 Pratt & Whitney Canada Corp. Gas turbine braking apparatus and method
FR2959488B1 (en) * 2010-04-28 2012-05-18 Aircelle Sa NACELLE FOR AN AIRCRAFT ENGINE WITH THRUST INVERTER WITH GRIDS AND ADAPTIVE TUBE

Also Published As

Publication number Publication date
FR2993026A1 (en) 2014-01-10

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Legal Events

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Year of fee payment: 5

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Effective date: 20180330