FR2907098B1 - Nacelle pour turboreacteur double flux - Google Patents

Nacelle pour turboreacteur double flux

Info

Publication number
FR2907098B1
FR2907098B1 FR0608892A FR0608892A FR2907098B1 FR 2907098 B1 FR2907098 B1 FR 2907098B1 FR 0608892 A FR0608892 A FR 0608892A FR 0608892 A FR0608892 A FR 0608892A FR 2907098 B1 FR2907098 B1 FR 2907098B1
Authority
FR
France
Prior art keywords
nacelle
double flow
turbojet
turbojet double
flow
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
FR0608892A
Other languages
English (en)
Other versions
FR2907098A1 (fr
Inventor
Guy Vauchel
Jerome Collier
Patrice Dhainault
Francois Conte
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 FR0608892A priority Critical patent/FR2907098B1/fr
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to CA002665425A priority patent/CA2665425A1/fr
Priority to BRPI0717730-5A2A priority patent/BRPI0717730A2/pt
Priority to EP07858402A priority patent/EP2076438A2/fr
Priority to CN2007800379069A priority patent/CN101522524B/zh
Priority to PCT/FR2007/001633 priority patent/WO2008043903A2/fr
Priority to US12/445,421 priority patent/US8523516B2/en
Priority to RU2009117418/11A priority patent/RU2453477C2/ru
Publication of FR2907098A1 publication Critical patent/FR2907098A1/fr
Application granted granted Critical
Publication of FR2907098B1 publication Critical patent/FR2907098B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0608892A 2006-10-11 2006-10-11 Nacelle pour turboreacteur double flux Expired - Fee Related FR2907098B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR0608892A FR2907098B1 (fr) 2006-10-11 2006-10-11 Nacelle pour turboreacteur double flux
BRPI0717730-5A2A BRPI0717730A2 (pt) 2006-10-11 2007-10-05 Nacela para motor turbojato de contorno, conjunto de propulsão e avião
EP07858402A EP2076438A2 (fr) 2006-10-11 2007-10-05 Nacelle pour turboréacteur double flux
CN2007800379069A CN101522524B (zh) 2006-10-11 2007-10-05 旁路涡轮喷气发动机的发动机舱
CA002665425A CA2665425A1 (fr) 2006-10-11 2007-10-05 Nacelle pour turboreacteur double flux
PCT/FR2007/001633 WO2008043903A2 (fr) 2006-10-11 2007-10-05 Nacelle pour turboréacteur double flux
US12/445,421 US8523516B2 (en) 2006-10-11 2007-10-05 Bypass turbojet engine nacelle
RU2009117418/11A RU2453477C2 (ru) 2006-10-11 2007-10-05 Гондола для двухконтурного турбореактивного двигателя

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0608892A FR2907098B1 (fr) 2006-10-11 2006-10-11 Nacelle pour turboreacteur double flux

Publications (2)

Publication Number Publication Date
FR2907098A1 FR2907098A1 (fr) 2008-04-18
FR2907098B1 true FR2907098B1 (fr) 2010-04-16

Family

ID=37983653

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0608892A Expired - Fee Related FR2907098B1 (fr) 2006-10-11 2006-10-11 Nacelle pour turboreacteur double flux

Country Status (2)

Country Link
CN (1) CN101522524B (fr)
FR (1) FR2907098B1 (fr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2950322B1 (fr) * 2009-09-22 2012-05-25 Airbus Operations Sas Element d'accrochage d'un moteur d'aeronef, ensemble d'aeronef comprenant cet element et aeronef associe
FR2950323B1 (fr) 2009-09-22 2011-11-04 Airbus Operations Sas Mat d'accrochage de moteur d'aeronef, ensemble comprenant ce mat et aeronef associe
FR2950860B1 (fr) 2009-10-01 2011-12-09 Airbus Operations Sas Dispositif d'accrochage d'un moteur a un mat d'aeronef
FR2952126B1 (fr) * 2009-11-04 2011-12-23 Snecma Turbomachine a double flux pour aeronef, comprenant des moyens structuraux de rigidification du carter central
US8876042B2 (en) 2009-12-21 2014-11-04 General Electric Company Integrated nacelle assembly
FR2978494B1 (fr) 2011-07-25 2013-08-02 Aircelle Sa Dispositif de liaison d'un cadre avant a un carter de soufflante
CN103112595B (zh) * 2013-02-06 2016-01-27 中国商用飞机有限责任公司 推进系统一体化的吊挂结构
CA2916522C (fr) 2013-07-29 2021-05-11 Bombardier Inc. Procede de fixation d'un ensemble groupe propulseur et mat pre-assemble sur un avion
FR3010147B1 (fr) 2013-08-28 2015-08-21 Snecma Suspension isostatique d'un turboreacteur par double support arriere
FR3023325B1 (fr) * 2014-07-04 2016-07-15 Aircelle Sa Cadre arriere pour une structure d'inverseur de poussee a grilles de deviation
FR3032180B1 (fr) * 2015-01-30 2018-05-18 Airbus Operations Ensemble propulsif comportant un turboreacteur et un mat d'accrochage permettant une nouvelle distribution des efforts entre le turboreacteur et la voilure
US10144525B2 (en) * 2015-09-24 2018-12-04 Embraer S.A. Aircraft engine pylon to wing mounting assembly
FR3045570B1 (fr) * 2015-12-16 2017-12-22 Airbus Operations Sas Ensemble moteur pour aeronef, comprenant un dispositif d'accrochage du moteur equipe d'une enveloppe structurale fixee sur un caisson central
FR3074225B1 (fr) * 2017-11-27 2019-12-13 Safran Nacelles Nacelle de turboreacteur comportant un cadre mobile unique d’inverseur de poussee a grilles et des passages de servitudes
FR3095194B1 (fr) * 2019-04-17 2021-08-13 Safran Aircraft Engines Entrée d’air de nacelle de turboréacteur comprenant un dispositif de déviation pour favoriser une phase d’inversion de poussée
FR3095418B1 (fr) * 2019-04-26 2021-09-24 Safran Nacelles Entrée d’air de nacelle et nacelle comportant une telle entrée d’air
FR3097260B1 (fr) * 2019-06-12 2021-06-11 Safran Aircraft Engines Carter de soufflante de turboréacteur
CN111828197A (zh) * 2020-07-23 2020-10-27 林睿 一种航空发动机尾喷管

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9116986D0 (en) * 1991-08-07 1991-10-09 Rolls Royce Plc Gas turbine engine nacelle assembly
US5277382A (en) * 1992-10-13 1994-01-11 General Electric Company Aircraft engine forward mount
GB2275308B (en) * 1993-02-20 1997-02-26 Rolls Royce Plc A mounting for coupling a turbofan gas turbine engine to an aircraft structure
US5524847A (en) * 1993-09-07 1996-06-11 United Technologies Corporation Nacelle and mounting arrangement for an aircraft engine
FR2732074B1 (fr) * 1995-03-21 1997-06-06 Aerospatiale Turboreacteur a double flux a nacelle flottante
GB9602130D0 (en) * 1996-02-02 1996-04-03 Rolls Royce Plc Improved method of combining ducted fan gas turbine engine modules and aircraft structure
FR2764644B1 (fr) 1997-06-12 1999-07-16 Hispano Suiza Sa Turboreacteur a double flux associe a un inverseur de poussee avec un carenage rapporte dans la veine fluide
GB9723022D0 (en) * 1997-11-01 1998-01-07 Rolls Royce Plc Gas turbine apparatus
CN1269308A (zh) * 2000-03-21 2000-10-11 贾龙 一种飞行器的升空和飞行方法及其装置
GB2375513B (en) * 2001-05-19 2005-03-23 Rolls Royce Plc A mounting arrangement for a gas turbine engine
FR2873988B1 (fr) * 2004-08-05 2007-12-21 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef

Also Published As

Publication number Publication date
CN101522524B (zh) 2012-08-29
FR2907098A1 (fr) 2008-04-18
CN101522524A (zh) 2009-09-02

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20160630