FR3040076B1 - Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau - Google Patents

Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau

Info

Publication number
FR3040076B1
FR3040076B1 FR1557719A FR1557719A FR3040076B1 FR 3040076 B1 FR3040076 B1 FR 3040076B1 FR 1557719 A FR1557719 A FR 1557719A FR 1557719 A FR1557719 A FR 1557719A FR 3040076 B1 FR3040076 B1 FR 3040076B1
Authority
FR
France
Prior art keywords
arceau
global
parts
shape
primary structure
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.)
Active
Application number
FR1557719A
Other languages
English (en)
Other versions
FR3040076A1 (fr
Inventor
Olivier Pautis
Jean Michel Rogero
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1557719A priority Critical patent/FR3040076B1/fr
Priority to CA2937764A priority patent/CA2937764A1/fr
Priority to US15/231,898 priority patent/US10017267B2/en
Priority to CN201610665530.7A priority patent/CN106428578B/zh
Publication of FR3040076A1 publication Critical patent/FR3040076A1/fr
Application granted granted Critical
Publication of FR3040076B1 publication Critical patent/FR3040076B1/fr
Active 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • 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
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/12—Aircraft characterised by the type or position of power plants of gas-turbine 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • 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
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • F05D2240/00—Components
    • F05D2240/90—Mounting on supporting structures or systems
    • 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
    • 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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1557719A 2015-08-13 2015-08-13 Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau Active FR3040076B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1557719A FR3040076B1 (fr) 2015-08-13 2015-08-13 Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau
CA2937764A CA2937764A1 (fr) 2015-08-13 2016-08-01 Ensemble moteur d'aeronef comportant une premiere structure d'un pylone de montage equipe d'une rallonge de boite comportant deux parties de forme generale courbee
US15/231,898 US10017267B2 (en) 2015-08-13 2016-08-09 Engine assembly for an aircraft comprising a primary structure of a mounting pylon equipped with a box extension comprising two parts in the overall shape of an arch
CN201610665530.7A CN106428578B (zh) 2015-08-13 2016-08-12 用于飞行器的发动机组件和包括此发动机组件的飞行器

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1557719A FR3040076B1 (fr) 2015-08-13 2015-08-13 Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau

Publications (2)

Publication Number Publication Date
FR3040076A1 FR3040076A1 (fr) 2017-02-17
FR3040076B1 true FR3040076B1 (fr) 2017-08-11

Family

ID=54260994

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1557719A Active FR3040076B1 (fr) 2015-08-13 2015-08-13 Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau

Country Status (4)

Country Link
US (1) US10017267B2 (fr)
CN (1) CN106428578B (fr)
CA (1) CA2937764A1 (fr)
FR (1) FR3040076B1 (fr)

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FR2981046B1 (fr) * 2011-10-06 2013-10-25 Aircelle Sa Ensemble propulsif d'aeronef
FR3055669B1 (fr) 2016-09-05 2018-09-28 Airbus Operations Systeme d'inverseur de poussee limitant les perturbations aerodynamiques en configuration inactive
US10414509B2 (en) * 2017-02-23 2019-09-17 United Technologies Corporation Propulsor mounting for advanced body aircraft
FR3065441B1 (fr) * 2017-04-19 2019-07-05 Airbus Operations Ensemble pour aeronef comprenant une structure primaire de mat d'accrochage fixee a un caisson de voilure a l'aide d'une liaison boulonnee
US10723471B2 (en) * 2017-06-14 2020-07-28 General Electric Company Method and system for mounting an aircraft engine
FR3069848B1 (fr) * 2017-08-02 2019-08-30 Airbus Structure primaire allegee pour mat d'accrochage de moteur d'aeronef
FR3071820B1 (fr) 2017-10-03 2020-12-04 Airbus Operations Sas Ensemble moteur d'aeronef
GB201804962D0 (en) * 2018-03-28 2018-05-09 Rolls Royce Plc A geared turbofan engine mount arrangement
FR3084339A1 (fr) * 2018-07-30 2020-01-31 Airbus Operations Ensemble pour un aeronef, l'ensemble comportant un mat et une attache moteur avant
US11008884B2 (en) * 2018-08-10 2021-05-18 Rolls-Royce North American Technologies, Inc. Gensets and methods of producing gensets from an engine and generator for hybrid electric propulsion
FR3089954B1 (fr) * 2018-12-12 2021-01-08 Airbus Operations Sas Ensemble de motorisation pour un aeronef comprenant un support de charge
GB201900609D0 (en) * 2019-01-16 2019-03-06 Rolls Royce Plc Mounting apparatus for gas turbine engine
CN112776993A (zh) * 2019-11-05 2021-05-11 中国航发商用航空发动机有限责任公司 一种飞机及其吊挂结构
EP3950507B1 (fr) * 2020-08-04 2023-11-08 Airbus SAS Procédé d'assemblage d'un mât d'aéronef et mât d'aéronef obtenu à partir de ce procédé
FR3114129B1 (fr) * 2020-09-14 2022-08-05 Safran Aircraft Engines Ensemble comportant une turbomachine d’aeronef et son pylone d’accrochage
FR3122644B1 (fr) * 2021-05-04 2023-06-16 Airbus Operations Sas Assemblage d’une structure primaire d’un mât d’aéronef et d’une attache-moteur arrière comprenant au moins un élément de fixation latéral et aéronef comprenant au moins un tel assemblage
GB202117777D0 (en) * 2021-12-09 2022-01-26 Rolls Royce Plc Support structure for attaching a gas turbine engine to an aircraft pylon

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US5351930A (en) * 1992-08-11 1994-10-04 Lord Corporation Mounting for engines and the like
FR2738034B1 (fr) * 1995-08-23 1997-09-19 Snecma Dispositif de suspension d'un turbopropulseur
GB9602130D0 (en) 1996-02-02 1996-04-03 Rolls Royce Plc Improved method of combining ducted fan gas turbine engine modules and aircraft structure
US6607165B1 (en) * 2002-06-28 2003-08-19 General Electric Company Aircraft engine mount with single thrust link
FR2873985B1 (fr) * 2004-08-04 2006-11-24 Airbus France Sas Ensemble moteur pour aeronef
FR2878229B1 (fr) * 2004-11-23 2008-04-18 Airbus France Sas Systeme de fixation d'un mat de moteur a l'aile d'un aeronef
FR2885877B1 (fr) * 2005-05-23 2008-12-12 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2889163B1 (fr) * 2005-07-29 2007-09-07 Airbus France Sas Ensemble pour aeronef comprenant un element de voilure ainsi qu'un mat d'accrochage
FR2891245B1 (fr) * 2005-09-26 2007-10-26 Airbus France Sas Procede de montage d'un moteur d'aeronef sur une structure rigide d'un mat d'accrochage du moteur
FR2891247B1 (fr) * 2005-09-26 2009-04-03 Airbus France Sas Ensemble pour aeronef comprenant un element de voilure ainsi qu'un mat d'accrochage
FR2891254B1 (fr) * 2005-09-29 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef
FR2891526B1 (fr) * 2005-10-03 2007-11-02 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
US8256707B2 (en) 2007-08-01 2012-09-04 United Technologies Corporation Engine mounting configuration for a turbofan gas turbine engine
FR2920409B1 (fr) * 2007-08-27 2009-12-18 Airbus France Berceau de support de capot de soufflante monte sur le mat d'accrochage et sur l'entree d'air de la nacelle
US8205825B2 (en) * 2008-02-27 2012-06-26 Spirit Aerosystems, Inc. Engine pylon made from composite material
FR2941673B1 (fr) * 2009-02-04 2011-01-14 Aircelle Sa Ensemble de suspension pour turboreacteur d'aeronef
FR2964364B1 (fr) * 2010-09-03 2012-09-28 Airbus Operations Sas Mat d'accrochage de turboreacteur pour aeronef comprenant des attaches voilure avant alignees
US20130074517A1 (en) * 2011-09-23 2013-03-28 United Technologies Corporation Gas turbine engine mount assembly
US9212607B2 (en) * 2012-07-18 2015-12-15 Spirit Aerosystems, Inc. Intermediate structure for independently de-mountable propulsion components
JP6114043B2 (ja) * 2013-01-25 2017-04-12 三菱航空機株式会社 航空機のパイロン、及び、航空機
US9248921B2 (en) * 2013-07-11 2016-02-02 Spirit Aerosystems, Inc. Method for mounting a pylon to an aircraft
EP3049657B1 (fr) * 2013-09-27 2018-10-03 United Technologies Corporation Systèmes de montage pour moteurs à turbine à gaz
FR3014841B1 (fr) * 2013-12-17 2017-12-08 Airbus Operations Sas Ensemble pour aeronef comprenant un corps d'attache moteur en partie realise d'une seule piece avec une nervure interieure de rigidification d'un caisson de mat d'accrochage
FR3027875A1 (fr) * 2014-10-30 2016-05-06 Airbus Operations Sas Dispositif de fixation d'un moteur d'aeronef, et aeronef correspondant

Also Published As

Publication number Publication date
CA2937764A1 (fr) 2017-02-13
US20170043878A1 (en) 2017-02-16
CN106428578A (zh) 2017-02-22
FR3040076A1 (fr) 2017-02-17
CN106428578B (zh) 2021-05-28
US10017267B2 (en) 2018-07-10

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