RU2500586C2 - Замковая система для воздухозаборника гондолы турбореактивного двигателя - Google Patents

Замковая система для воздухозаборника гондолы турбореактивного двигателя Download PDF

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Publication number
RU2500586C2
RU2500586C2 RU2010135894/11A RU2010135894A RU2500586C2 RU 2500586 C2 RU2500586 C2 RU 2500586C2 RU 2010135894/11 A RU2010135894/11 A RU 2010135894/11A RU 2010135894 A RU2010135894 A RU 2010135894A RU 2500586 C2 RU2500586 C2 RU 2500586C2
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RU
Russia
Prior art keywords
air intake
inner panel
lip
nacelle
hook
Prior art date
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RU2010135894/11A
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English (en)
Russian (ru)
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RU2010135894A (ru
Inventor
Ги ВОШЕЛЬ
Жан-Филипп ДОГЕ
Стефан БЕЙАР
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Эрсель
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Publication date
Application filed by Эрсель filed Critical Эрсель
Publication of RU2010135894A publication Critical patent/RU2010135894A/ru
Application granted granted Critical
Publication of RU2500586C2 publication Critical patent/RU2500586C2/ru

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/08—Inspection panels for power plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286—Arrangement 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

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  • 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)
RU2010135894/11A 2008-02-01 2008-11-21 Замковая система для воздухозаборника гондолы турбореактивного двигателя RU2500586C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0800560A FR2927061B1 (fr) 2008-02-01 2008-02-01 Systeme de verrouillage pour structure d'entree d'air d'une nacelle de turboreacteur
FR08/00560 2008-02-01
PCT/FR2008/001631 WO2009101273A1 (fr) 2008-02-01 2008-11-21 Système de verrouillage pour structure d'entrée d'air d'une nacelle de turboréacteur

Publications (2)

Publication Number Publication Date
RU2010135894A RU2010135894A (ru) 2012-03-10
RU2500586C2 true RU2500586C2 (ru) 2013-12-10

Family

ID=39731653

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2010135894/11A RU2500586C2 (ru) 2008-02-01 2008-11-21 Замковая система для воздухозаборника гондолы турбореактивного двигателя

Country Status (8)

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

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US8181905B2 (en) * 2008-12-17 2012-05-22 Rohr, Inc. Aircraft engine nacelle with translating inlet cowl
FR2942457B1 (fr) * 2009-02-24 2011-04-22 Snecma Nacelle de turboreacteur a structure d'entree d'air amovible
DE102011103163A1 (de) * 2011-06-01 2012-12-06 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinentriebwerk mit teleskopartigem Lufteinlass der Triebwerksverkleidung
FR2978494B1 (fr) * 2011-07-25 2013-08-02 Aircelle Sa Dispositif de liaison d'un cadre avant a un carter de soufflante
US9702375B2 (en) 2013-07-16 2017-07-11 United Technologies Corporation Liner attaching scheme
FR3020040B1 (fr) 2014-04-17 2018-06-29 Societe Lorraine De Construction Aeronautique Ensemble propulsif pour aeronef
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 (fr) * 2015-01-07 2017-07-14 Aircelle Sa Ensemble propulsif pour aeronef
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 (fr) * 2016-06-17 2019-05-03 Safran Nacelles Systeme de guidage axial pour des capots d'inverseur de poussee comprenant un doigt de securite
US10543927B2 (en) * 2016-11-18 2020-01-28 Rohr, Inc. Lockable track system for a translating nacelle structure
US10738737B2 (en) 2016-11-18 2020-08-11 Rohr, Inc. Self-locking alignment at a nacelle interface
FR3075761A1 (fr) * 2017-12-21 2019-06-28 Airbus Operations Partie anterieure de nacelle d'un ensemble propulsif comportant un cadre de rigidification incline
CN107985599B (zh) * 2017-12-27 2024-09-06 天机智汇科技（深圳）有限公司 自动载货装置、无人机及载货舱
US11525372B2 (en) * 2018-03-27 2022-12-13 Rohr, Inc. Diaphragm latch
FR3085353A1 (fr) * 2018-09-04 2020-03-06 Airbus Operations Ensemble turbomachine d'aeronef comportant un capot articule
US11441514B2 (en) * 2018-10-02 2022-09-13 Woodward, Inc. Tertiary lock
FR3095416B1 (fr) * 2019-04-26 2021-04-23 Safran Nacelles Entrée d’air de nacelle de turboréacteur
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
FR3101854B1 (fr) * 2019-10-15 2024-05-31 Inst Superieur De L Aeronautique Et De L Espace Nacelle de turbomachine

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2284180A (en) * 1938-04-27 1942-05-26 Havilland Aireraft Company Ltd Securing device, particularly for such parts as aircraft cowlings and the like
US4174609A (en) * 1977-02-08 1979-11-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Locking system for sliding cowlings of turbojet engine nacelles
US5011200A (en) * 1989-11-21 1991-04-30 The Boeing Company Latch with preload indication
GB2274490A (en) * 1993-01-26 1994-07-27 Short Brothers Plc Nacelle for an aircraft propulsive power unit
RU2099252C1 (ru) * 1996-03-20 1997-12-20 Анатолий Дмитриевич Гагарин Замок стяжной капотный
US5997054A (en) * 1997-04-03 1999-12-07 Societe Hispano-Suiza Aerostructures Device for closing and locking the shutters of a thrust reverser
US6032901A (en) * 1996-11-28 2000-03-07 Societe Hispano-Suiza Linkage system for an aircraft turbojet engine
EP1091059A2 (en) * 1999-10-05 2001-04-11 Hartwell Corporation Latch with sensor providing visual indication of the latch position
EP1715160A1 (en) * 2005-04-22 2006-10-25 Rohr, Inc. Aircraft engine nacelle inlet having electrical ice protection system
WO2007118626A1 (de) * 2006-04-10 2007-10-25 Franz Haimer Maschinenbau Kg Auszugssicherung von werkzeugen aus werkzeughaltern mit einer werkzeugaufnahme

Family Cites Families (8)

* 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
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
US4320912A (en) * 1979-09-10 1982-03-23 Rohr Industries, Inc. Cowl door latch adjustment fitting assembly
US5152559A (en) * 1989-12-04 1992-10-06 The Hartwell Corporation Latching mechanism
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
FR2906568B1 (fr) * 2006-10-02 2012-01-06 Aircelle Sa Structure d'entree d'air deposable pour nacelle de turboreacteur.

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2284180A (en) * 1938-04-27 1942-05-26 Havilland Aireraft Company Ltd Securing device, particularly for such parts as aircraft cowlings and the like
US4174609A (en) * 1977-02-08 1979-11-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Locking system for sliding cowlings of turbojet engine nacelles
US5011200A (en) * 1989-11-21 1991-04-30 The Boeing Company Latch with preload indication
GB2274490A (en) * 1993-01-26 1994-07-27 Short Brothers Plc Nacelle for an aircraft propulsive power unit
RU2099252C1 (ru) * 1996-03-20 1997-12-20 Анатолий Дмитриевич Гагарин Замок стяжной капотный
US6032901A (en) * 1996-11-28 2000-03-07 Societe Hispano-Suiza Linkage system for an aircraft turbojet engine
US5997054A (en) * 1997-04-03 1999-12-07 Societe Hispano-Suiza Aerostructures Device for closing and locking the shutters of a thrust reverser
EP1091059A2 (en) * 1999-10-05 2001-04-11 Hartwell Corporation Latch with sensor providing visual indication of the latch position
EP1715160A1 (en) * 2005-04-22 2006-10-25 Rohr, Inc. Aircraft engine nacelle inlet having electrical ice protection system
WO2007118626A1 (de) * 2006-04-10 2007-10-25 Franz Haimer Maschinenbau Kg Auszugssicherung von werkzeugen aus werkzeughaltern mit einer werkzeugaufnahme

Also Published As

Publication number Publication date
FR2927061A1 (fr) 2009-08-07
EP2252511A1 (fr) 2010-11-24
CN101925515A (zh) 2010-12-22
CA2711830A1 (fr) 2009-08-20
RU2010135894A (ru) 2012-03-10
FR2927061B1 (fr) 2010-02-12
BRPI0821929A2 (pt) 2015-06-16
WO2009101273A1 (fr) 2009-08-20
US20110014044A1 (en) 2011-01-20

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20151122