FR3045570B1 - Ensemble moteur pour aeronef, comprenant un dispositif d'accrochage du moteur equipe d'une enveloppe structurale fixee sur un caisson central - Google Patents

Ensemble moteur pour aeronef, comprenant un dispositif d'accrochage du moteur equipe d'une enveloppe structurale fixee sur un caisson central

Info

Publication number
FR3045570B1
FR3045570B1 FR1562540A FR1562540A FR3045570B1 FR 3045570 B1 FR3045570 B1 FR 3045570B1 FR 1562540 A FR1562540 A FR 1562540A FR 1562540 A FR1562540 A FR 1562540A FR 3045570 B1 FR3045570 B1 FR 3045570B1
Authority
FR
France
Prior art keywords
device equipped
aircraft engine
engine assembly
attaching device
structural envelope
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
FR1562540A
Other languages
English (en)
Other versions
FR3045570A1 (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 FR1562540A priority Critical patent/FR3045570B1/fr
Priority to GB1621379.5A priority patent/GB2546879B/en
Priority to US15/381,821 priority patent/US10562639B2/en
Publication of FR3045570A1 publication Critical patent/FR3045570A1/fr
Application granted granted Critical
Publication of FR3045570B1 publication Critical patent/FR3045570B1/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
    • B64D27/02—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
    • 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
    • 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
    • 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
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1562540A 2015-12-16 2015-12-16 Ensemble moteur pour aeronef, comprenant un dispositif d'accrochage du moteur equipe d'une enveloppe structurale fixee sur un caisson central Active FR3045570B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1562540A FR3045570B1 (fr) 2015-12-16 2015-12-16 Ensemble moteur pour aeronef, comprenant un dispositif d'accrochage du moteur equipe d'une enveloppe structurale fixee sur un caisson central
GB1621379.5A GB2546879B (en) 2015-12-16 2016-12-15 Aircraft engine assembly, comprising an attachment device for the engine equipped with a structural cover attached on a central box
US15/381,821 US10562639B2 (en) 2015-12-16 2016-12-16 Aircraft engine assembly, comprising an attachment device for the engine equipped with a structural cover attached on a central box

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1562540A FR3045570B1 (fr) 2015-12-16 2015-12-16 Ensemble moteur pour aeronef, comprenant un dispositif d'accrochage du moteur equipe d'une enveloppe structurale fixee sur un caisson central

Publications (2)

Publication Number Publication Date
FR3045570A1 FR3045570A1 (fr) 2017-06-23
FR3045570B1 true FR3045570B1 (fr) 2017-12-22

Family

ID=55451361

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1562540A Active FR3045570B1 (fr) 2015-12-16 2015-12-16 Ensemble moteur pour aeronef, comprenant un dispositif d'accrochage du moteur equipe d'une enveloppe structurale fixee sur un caisson central

Country Status (3)

Country Link
US (1) US10562639B2 (fr)
FR (1) FR3045570B1 (fr)
GB (1) GB2546879B (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3047973B1 (fr) * 2016-02-23 2018-03-09 Airbus Operations Ensemble moteur pour aeronef, comprenant un dispositif d'accrochage du moteur equipe de capots mobiles structuraux relies au caisson central
CN107512399B (zh) * 2017-07-28 2020-04-21 中国航空工业集团公司西安飞机设计研究所 盒形梁式发动机主安装接头
GB201804962D0 (en) * 2018-03-28 2018-05-09 Rolls Royce Plc A geared turbofan engine mount arrangement

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2661213B1 (fr) * 1990-04-19 1992-07-03 Snecma Moteur d'aviation a tres grand taux de dilution et du type dit contrafan avant.
US5226288A (en) * 1991-06-21 1993-07-13 Rohr, Inc. Torque link fan jet engine support for reducing engine bending
GB9120658D0 (en) * 1991-09-27 1991-11-06 Short Brothers Plc Ducted fan turbine engine
GB9407632D0 (en) * 1994-04-18 1994-06-08 Short Brothers Plc An aircraft propulsive power unit
US6340135B1 (en) * 2000-05-30 2002-01-22 Rohr, Inc. Translating independently mounted air inlet system for aircraft turbofan jet engine
FR2873988B1 (fr) * 2004-08-05 2007-12-21 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2873987B1 (fr) * 2004-08-05 2006-11-24 Airbus France Sas Ensemble moteur pour aeronef
FR2885877B1 (fr) 2005-05-23 2008-12-12 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2903076B1 (fr) * 2006-06-30 2009-05-29 Aircelle Sa Nacelle structurante
FR2906568B1 (fr) * 2006-10-02 2012-01-06 Aircelle Sa Structure d'entree d'air deposable pour nacelle de turboreacteur.
EP2076438A2 (fr) * 2006-10-11 2009-07-08 Aircelle Nacelle pour turboréacteur double flux
FR2907098B1 (fr) * 2006-10-11 2010-04-16 Aircelle Sa Nacelle pour turboreacteur double flux
FR2925877B1 (fr) * 2007-12-26 2009-12-04 Aircelle Sa Installation de systeme de guidage sur une nacelle d'aeronef.
FR2969700B1 (fr) * 2010-12-23 2015-05-15 Snecma Systeme propulsif pour aeronef
US9783315B2 (en) * 2012-02-24 2017-10-10 Rohr, Inc. Nacelle with longitudinal translating cowling and rotatable sleeves
FR3012793B1 (fr) 2013-11-05 2017-05-05 Airbus Operations Sas Ensemble pour aeronef comprenant une ferrure fixee sur la partie extrados d'un caisson de voilure, pour le montage d'un mat d'accrochage sur ce caisson de voilure
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

Also Published As

Publication number Publication date
GB201621379D0 (en) 2017-02-01
US20170197724A1 (en) 2017-07-13
GB2546879B (en) 2021-02-03
GB2546879A (en) 2017-08-02
FR3045570A1 (fr) 2017-06-23
US10562639B2 (en) 2020-02-18

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