FR3015434B1 - Suspension de turbomachine - Google Patents

Suspension de turbomachine

Info

Publication number
FR3015434B1
FR3015434B1 FR1363488A FR1363488A FR3015434B1 FR 3015434 B1 FR3015434 B1 FR 3015434B1 FR 1363488 A FR1363488 A FR 1363488A FR 1363488 A FR1363488 A FR 1363488A FR 3015434 B1 FR3015434 B1 FR 3015434B1
Authority
FR
France
Prior art keywords
turbomachine
suspension
turbomachine suspension
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
FR1363488A
Other languages
English (en)
Other versions
FR3015434A1 (fr
Inventor
Pierrot Guillou
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 Aircraft Engines SAS
Original Assignee
SNECMA 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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1363488A priority Critical patent/FR3015434B1/fr
Priority to US14/577,010 priority patent/US9394057B2/en
Priority to GB1423143.5A priority patent/GB2523245B/en
Publication of FR3015434A1 publication Critical patent/FR3015434A1/fr
Application granted granted Critical
Publication of FR3015434B1 publication Critical patent/FR3015434B1/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
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Transmission Devices (AREA)
FR1363488A 2013-12-23 2013-12-23 Suspension de turbomachine Active FR3015434B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1363488A FR3015434B1 (fr) 2013-12-23 2013-12-23 Suspension de turbomachine
US14/577,010 US9394057B2 (en) 2013-12-23 2014-12-19 Suspension for a turbine engine
GB1423143.5A GB2523245B (en) 2013-12-23 2014-12-23 A suspension for a turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1363488A FR3015434B1 (fr) 2013-12-23 2013-12-23 Suspension de turbomachine

Publications (2)

Publication Number Publication Date
FR3015434A1 FR3015434A1 (fr) 2015-06-26
FR3015434B1 true FR3015434B1 (fr) 2017-12-08

Family

ID=50424517

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1363488A Active FR3015434B1 (fr) 2013-12-23 2013-12-23 Suspension de turbomachine

Country Status (3)

Country Link
US (1) US9394057B2 (fr)
FR (1) FR3015434B1 (fr)
GB (1) GB2523245B (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2981046B1 (fr) * 2011-10-06 2013-10-25 Aircelle Sa Ensemble propulsif d'aeronef
CN108349592B (zh) 2015-09-04 2021-11-26 洛德公司 用于涡轮螺旋桨发动机/涡轮轴发动机的反扭矩后机架系统、装置和方法
FR3056251B1 (fr) * 2016-09-21 2018-09-07 Safran Aircraft Engines Carter d'echappement renforce et procede de fabrication
FR3058986B1 (fr) * 2016-11-21 2021-04-16 Airbus Operations Sas Attache arriere d'un moteur d'aeronef comportant des temoins de rupture
FR3074147B1 (fr) * 2017-11-30 2019-12-20 Airbus Operations Assemblage comportant une chape, une plaque d'accouplement et un systeme de fixation de la plaque d'accouplement a la chape
US11077954B2 (en) * 2017-12-20 2021-08-03 General Electric Company Connection assembly for mounting engine and engine mounting system comprising the same
FR3093704B1 (fr) * 2019-03-11 2021-06-11 Airbus Operations Sas Attache moteur arrière d’un ensemble propulsif d’aéronef
FR3106126B1 (fr) 2020-01-10 2022-01-07 Safran Aircraft Engines Assemblage entre un pylône d’aéronef et une turbomachine
US11697506B2 (en) * 2020-05-15 2023-07-11 General Electric Company Methods and apparatus for gas turbine bending isolation
FR3114801A1 (fr) * 2020-10-02 2022-04-08 Airbus Operations Assemblage d’un mat avec une aile d’un aeronef
US11560840B2 (en) 2020-10-16 2023-01-24 General Electric Company Damper engine mount links
FR3123323B1 (fr) 2021-05-27 2024-05-03 Safran Aircraft Engines Structure de liaison et de support d’une turbomachine a un pylone d’aeronef
FR3128205A1 (fr) * 2021-10-14 2023-04-21 Airbus Operations Assemblage d’un mat avec un moteur d’un aéronef

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1514305A (en) * 1975-09-12 1978-06-14 Rolls Royce Ejector sleeves for aircraft mounted gas turbine engines
GB8300748D0 (en) * 1983-01-12 1983-02-16 British Aerospace Power plant attachment for aircraft wings
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
FR2836672B1 (fr) * 2002-03-04 2004-06-04 Airbus France Mat d'accrochage d'un moteur sous une voilure d'aeronef
US6607165B1 (en) * 2002-06-28 2003-08-19 General Electric Company Aircraft engine mount with single thrust link
FR2862611B1 (fr) * 2003-11-25 2007-03-09 Airbus France Dispositif d'accrochage d'un moteur sous une voilure d'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
FR2883839B1 (fr) * 2005-03-29 2007-06-29 Snecma Moteurs Sa Suspension arriere de turboreacteur
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
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
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
FR2891526B1 (fr) * 2005-10-03 2007-11-02 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2905932B1 (fr) * 2006-09-20 2008-12-05 Airbus France Sa Agencement pour attache de dispositif d'accrochage d'un moteur d'aeronef
FR2920138B1 (fr) * 2007-08-24 2010-03-12 Airbus France Dispositif d'accrochage de moteur d'aeronef comportant un dispositif de reprise des efforts de poussee a encombrement reduit
US8205825B2 (en) * 2008-02-27 2012-06-26 Spirit Aerosystems, Inc. Engine pylon made from composite material
DE102010025488B4 (de) * 2010-06-29 2012-10-25 Martin Thoma Klapptriebwerk für Flugzeuge
US9227734B2 (en) * 2012-08-31 2016-01-05 United Technologies Corporation Secondary load path for gas turbine engine
US20140084129A1 (en) * 2012-09-27 2014-03-27 United Technologies Corporation Assembly for mounting a turbine engine case to a pylon

Also Published As

Publication number Publication date
GB2523245B (en) 2017-03-15
US20150175268A1 (en) 2015-06-25
FR3015434A1 (fr) 2015-06-26
GB2523245A (en) 2015-08-19
US9394057B2 (en) 2016-07-19

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