FR2993026B1 - Mecanisme d'accouplement et de desaccouplement pour un dispositif embarque d'une nacelle de turboreacteur - Google Patents

Mecanisme d'accouplement et de desaccouplement pour un dispositif embarque d'une nacelle de turboreacteur

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
English (en)
Other versions
FR2993026A1 (fr
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/fr
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to EP13744672.0A priority patent/EP2870349B1/fr
Priority to CA2874578A priority patent/CA2874578A1/fr
Priority to BR112014030828A priority patent/BR112014030828A2/pt
Priority to PCT/FR2013/051554 priority patent/WO2014006321A1/fr
Priority to CN201380035761.4A priority patent/CN104428520A/zh
Priority to RU2015102973A priority patent/RU2015102973A/ru
Publication of FR2993026A1 publication Critical patent/FR2993026A1/fr
Application granted granted Critical
Publication of FR2993026B1 publication Critical patent/FR2993026B1/fr
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 Mecanisme d'accouplement et de desaccouplement pour un dispositif embarque d'une nacelle de turboreacteur Expired - Fee Related FR2993026B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1256438A FR2993026B1 (fr) 2012-07-05 2012-07-05 Mecanisme d'accouplement et de desaccouplement pour un dispositif embarque d'une nacelle de turboreacteur
CA2874578A CA2874578A1 (fr) 2012-07-05 2013-07-02 Mecanisme d'accouplement et de desaccouplement pour un dispositif embarque d'une nacelle de turboreacteur
BR112014030828A BR112014030828A2 (pt) 2012-07-05 2013-07-02 mecanismo para acoplamento e desacoplamento de um eixo de admissão de motor e nacela de motor turbojato.
PCT/FR2013/051554 WO2014006321A1 (fr) 2012-07-05 2013-07-02 Mécanisme d'accouplement et de désaccouplement pour un dispositif embarqué d'une nacelle de turboréacteur
EP13744672.0A EP2870349B1 (fr) 2012-07-05 2013-07-02 Mécanisme d'accouplement et de désaccouplement pour un dispositif embarqué d'une nacelle de turboréacteur
CN201380035761.4A CN104428520A (zh) 2012-07-05 2013-07-02 用于涡轮喷气发动机机舱机载装置的耦合和解耦合机构
RU2015102973A RU2015102973A (ru) 2012-07-05 2013-07-02 Соединительно-разъединительный механизм для устройства гондолы турбореактивного двигателя
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 (fr) 2012-07-05 2012-07-05 Mecanisme d'accouplement et de desaccouplement pour un dispositif embarque d'une nacelle de turboreacteur

Publications (2)

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

Family

ID=46826787

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1256438A Expired - Fee Related FR2993026B1 (fr) 2012-07-05 2012-07-05 Mecanisme d'accouplement et de desaccouplement pour un dispositif embarque d'une nacelle de turboreacteur

Country Status (1)

Country Link
FR (1) FR2993026B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110192046B (zh) 2016-12-30 2022-05-27 赛峰电子与防务公司 带有被动锁定的致动器
FR3061528B1 (fr) * 2016-12-30 2020-06-19 Safran Electronics & Defense Actionneur a verrouillage passif

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 (zh) * 2002-11-16 2004-06-02 Л 轴用活套及装置
US7225607B2 (en) * 2004-08-27 2007-06-05 Pratt & Whitney Canada Corp. Gas turbine braking apparatus and method
FR2959488B1 (fr) * 2010-04-28 2012-05-18 Aircelle Sa Nacelle pour moteur d'aeronef a inverseur de poussee a grilles et a tuyere adaptative

Also Published As

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

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Year of fee payment: 5

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Effective date: 20180330