FR2927061B1 - LATCHING SYSTEM FOR AIR INTAKE STRUCTURE OF A TURBOJET NACELLE - Google Patents

LATCHING SYSTEM FOR AIR INTAKE STRUCTURE OF A TURBOJET NACELLE

Info

Publication number
FR2927061B1
FR2927061B1 FR0800560A FR0800560A FR2927061B1 FR 2927061 B1 FR2927061 B1 FR 2927061B1 FR 0800560 A FR0800560 A FR 0800560A FR 0800560 A FR0800560 A FR 0800560A FR 2927061 B1 FR2927061 B1 FR 2927061B1
Authority
FR
France
Prior art keywords
air intake
intake structure
latching system
turbojet nacelle
turbojet
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
FR0800560A
Other languages
French (fr)
Other versions
FR2927061A1 (en
Inventor
Guy Vauchel
Jean Philippe Dauguet
Stephane Beilliard
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 FR0800560A priority Critical patent/FR2927061B1/en
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to EP08879343A priority patent/EP2252511A1/en
Priority to CA2711830A priority patent/CA2711830A1/en
Priority to US12/865,842 priority patent/US20110014044A1/en
Priority to CN2008801253791A priority patent/CN101925515A/en
Priority to BRPI0821929-0A priority patent/BRPI0821929A2/en
Priority to PCT/FR2008/001631 priority patent/WO2009101273A1/en
Priority to RU2010135894/11A priority patent/RU2500586C2/en
Publication of FR2927061A1 publication Critical patent/FR2927061A1/en
Application granted granted Critical
Publication of FR2927061B1 publication Critical patent/FR2927061B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/08Inspection panels for power plants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/06Attaching of nacelles, fairings or cowlings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0800560A 2008-02-01 2008-02-01 LATCHING SYSTEM FOR AIR INTAKE STRUCTURE OF A TURBOJET NACELLE Expired - Fee Related FR2927061B1 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR0800560A FR2927061B1 (en) 2008-02-01 2008-02-01 LATCHING SYSTEM FOR AIR INTAKE STRUCTURE OF A TURBOJET NACELLE
CA2711830A CA2711830A1 (en) 2008-02-01 2008-11-21 Locking system for air intake structure for turbojet engine nacelle
US12/865,842 US20110014044A1 (en) 2008-02-01 2008-11-21 Locking system for air intake structure for turbojet engine nacelle
CN2008801253791A CN101925515A (en) 2008-02-01 2008-11-21 The locking system that is used for air intake structure for turbojet engine nacelle
EP08879343A EP2252511A1 (en) 2008-02-01 2008-11-21 Locking system for air intake structure for turbojet engine nacelle
BRPI0821929-0A BRPI0821929A2 (en) 2008-02-01 2008-11-21 Turbojet engine nacelle
PCT/FR2008/001631 WO2009101273A1 (en) 2008-02-01 2008-11-21 Locking system for air intake structure for turbojet engine nacelle
RU2010135894/11A RU2500586C2 (en) 2008-02-01 2008-11-21 Turbojet nacelle air intake lock system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0800560A FR2927061B1 (en) 2008-02-01 2008-02-01 LATCHING SYSTEM FOR AIR INTAKE STRUCTURE OF A TURBOJET NACELLE

Publications (2)

Publication Number Publication Date
FR2927061A1 FR2927061A1 (en) 2009-08-07
FR2927061B1 true FR2927061B1 (en) 2010-02-12

Family

ID=39731653

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0800560A Expired - Fee Related FR2927061B1 (en) 2008-02-01 2008-02-01 LATCHING SYSTEM FOR AIR INTAKE STRUCTURE OF A TURBOJET NACELLE

Country Status (8)

Country Link
US (1) US20110014044A1 (en)
EP (1) EP2252511A1 (en)
CN (1) CN101925515A (en)
BR (1) BRPI0821929A2 (en)
CA (1) CA2711830A1 (en)
FR (1) FR2927061B1 (en)
RU (1) RU2500586C2 (en)
WO (1) WO2009101273A1 (en)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8181905B2 (en) 2008-12-17 2012-05-22 Rohr, Inc. Aircraft engine nacelle with translating inlet cowl
FR2942457B1 (en) * 2009-02-24 2011-04-22 Snecma TURBOREACTOR NACELLE WITH REMOVABLE AIR INTAKE STRUCTURE
DE102011103163A1 (en) * 2011-06-01 2012-12-06 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine engine with telescopic air intake of the engine cowling
FR2978494B1 (en) * 2011-07-25 2013-08-02 Aircelle Sa DEVICE FOR CONNECTING A FRAME FRONT TO A BLOWER HOUSING
US9702375B2 (en) 2013-07-16 2017-07-11 United Technologies Corporation Liner attaching scheme
FR3020040B1 (en) * 2014-04-17 2018-06-29 Societe Lorraine De Construction Aeronautique PROPULSIVE ASSEMBLY FOR AIRCRAFT
US9963237B2 (en) * 2014-04-25 2018-05-08 Rohr, Inc. Latch hooks, latch housings, and latch assemblies
US10221764B2 (en) * 2014-08-19 2019-03-05 Pratt & Whitney Canada Corp. Variable geometry inlet system
US9708073B2 (en) 2014-08-22 2017-07-18 Rohr, Inc. Automatic deflection limiting latches for a thrust reverser
FR3031341B1 (en) * 2015-01-07 2017-07-14 Aircelle Sa PROPULSIVE ASSEMBLY FOR AIRCRAFT
US10508566B2 (en) 2015-03-29 2019-12-17 Rohr, Inc. Inner fixed structure leading edge latch
US20170283081A1 (en) * 2016-04-05 2017-10-05 Rohr, Inc. Securing a translating fanlet for an aircraft propulsion system nacelle
FR3052809B1 (en) * 2016-06-17 2019-05-03 Safran Nacelles AXIAL GUIDING SYSTEM FOR THRUST INVERTER COILS COMPRISING A SAFETY FINGER
US10738737B2 (en) 2016-11-18 2020-08-11 Rohr, Inc. Self-locking alignment at a nacelle interface
US10543927B2 (en) * 2016-11-18 2020-01-28 Rohr, Inc. Lockable track system for a translating nacelle structure
FR3075761A1 (en) * 2017-12-21 2019-06-28 Airbus Operations ANTERIOR PLATFORM PART OF A NACELLE COMPRISING AN INCLINE RIGIDIFICATION FRAME
CN107985599A (en) * 2017-12-27 2018-05-04 天机智汇科技(深圳)有限公司 Automatic load-carrying device, unmanned plane and loading cabin
US11525372B2 (en) * 2018-03-27 2022-12-13 Rohr, Inc. Diaphragm latch
FR3085353A1 (en) * 2018-09-04 2020-03-06 Airbus Operations AIRCRAFT TURBOMACHINE ASSEMBLY WITH ARTICULATED HOOD
US11441514B2 (en) * 2018-10-02 2022-09-13 Woodward, Inc. Tertiary lock
FR3095416B1 (en) * 2019-04-26 2021-04-23 Safran Nacelles Turbojet nacelle air inlet
US11414200B2 (en) * 2019-04-29 2022-08-16 Rohr, Inc. Fan cowl securement retainers
EP3733525B1 (en) * 2019-04-29 2023-08-09 Rohr, Inc. Fan cowl securement retainers
US11441482B2 (en) * 2019-06-04 2022-09-13 Rohr, Inc. Single track translating inlet
FR3101854A1 (en) * 2019-10-15 2021-04-16 Institut Superieur De L Aeronautique Et De L Espace TURBOMACHINE NACELLE

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1488393A (en) * 1923-03-31 1924-03-25 Fred W Jackson Plug retainer
US2284180A (en) * 1938-04-27 1942-05-26 Havilland Aireraft Company Ltd Securing device, particularly for such parts as aircraft cowlings and the like
US2919569A (en) * 1955-03-30 1960-01-05 Gen Dynamics Corp Fastening device having a rotatable latch
GB1526224A (en) * 1975-10-28 1978-09-27 Rolls Royce Gas turbine engine cowls
FR2379434A1 (en) * 1977-02-08 1978-09-01 Snecma TURBOREACTOR NACELLE SLIDING COVER LOCKING SYSTEM
US4320912A (en) * 1979-09-10 1982-03-23 Rohr Industries, Inc. Cowl door latch adjustment fitting assembly
US5011200A (en) * 1989-11-21 1991-04-30 The Boeing Company Latch with preload indication
US5152559A (en) * 1989-12-04 1992-10-06 The Hartwell Corporation Latching mechanism
GB9301457D0 (en) * 1993-01-26 1993-03-17 Short Brothers Plc An aircraft propulsuve power unit
RU2099252C1 (en) * 1996-03-20 1997-12-20 Анатолий Дмитриевич Гагарин Clamping cowl fastener
FR2756323B1 (en) * 1996-11-28 1998-12-31 Hispano Suiza Sa DEVICE FOR CONNECTING A DRIVE INVERTER TO A TURBOMOTOR
FR2761734B1 (en) * 1997-04-03 1999-06-11 Hispano Suiza Sa DEVICE FOR CLOSING AND LOCKING THE SHUTTERS OF A PUSH INVERTER
US6279971B1 (en) * 1999-10-05 2001-08-28 Hartwell Corporation Latch with sensor
US6854774B2 (en) * 2003-03-21 2005-02-15 Southco, Inc. Locking device
US7252311B2 (en) * 2003-09-17 2007-08-07 Hartwell Corporation Motor driven latch
US7513458B2 (en) * 2005-04-22 2009-04-07 Rohr, Inc. Aircraft engine nacelle inlet having electrical ice protection system
DE102006028408A1 (en) * 2006-04-10 2007-10-31 Franz Haimer Maschinenbau Kg Tool holder has tool holding fixture, preferably chuck, where shank of a tool particularly rotary tool, is accommodated in tool holding fixture
FR2906568B1 (en) * 2006-10-02 2012-01-06 Aircelle Sa DEPOSITABLE AIR INTAKE STRUCTURE FOR TURBOJET NACELLE.

Also Published As

Publication number Publication date
US20110014044A1 (en) 2011-01-20
CA2711830A1 (en) 2009-08-20
BRPI0821929A2 (en) 2015-06-16
RU2500586C2 (en) 2013-12-10
EP2252511A1 (en) 2010-11-24
CN101925515A (en) 2010-12-22
FR2927061A1 (en) 2009-08-07
WO2009101273A1 (en) 2009-08-20
RU2010135894A (en) 2012-03-10

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Effective date: 20151030