FR2966125B1 - Ensemble d'accrochage d'une suspension d'un ensemble propulsif d'aeronef - Google Patents

Ensemble d'accrochage d'une suspension d'un ensemble propulsif d'aeronef

Info

Publication number
FR2966125B1
FR2966125B1 FR1058406A FR1058406A FR2966125B1 FR 2966125 B1 FR2966125 B1 FR 2966125B1 FR 1058406 A FR1058406 A FR 1058406A FR 1058406 A FR1058406 A FR 1058406A FR 2966125 B1 FR2966125 B1 FR 2966125B1
Authority
FR
France
Prior art keywords
assembly
suspension
hanging
propulsive
propulsive aircraft
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
FR1058406A
Other languages
English (en)
Other versions
FR2966125A1 (fr
Inventor
Herve Hurlin
Nicolas Dezeustre
Wouter Balk
Gilles Charier
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
Safran Nacelles SAS
Original Assignee
Aircelle SA
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
Priority to FR1058406A priority Critical patent/FR2966125B1/fr
Application filed by Aircelle SA, SNECMA SAS filed Critical Aircelle SA
Priority to PCT/FR2011/052307 priority patent/WO2012049399A1/fr
Priority to RU2013121274/11A priority patent/RU2013121274A/ru
Priority to BR112013007208A priority patent/BR112013007208A2/pt
Priority to CN2011800486141A priority patent/CN103153789A/zh
Priority to CA2812373A priority patent/CA2812373A1/fr
Priority to EP11779788.6A priority patent/EP2627561A1/fr
Publication of FR2966125A1 publication Critical patent/FR2966125A1/fr
Priority to US13/862,724 priority patent/US8839629B2/en
Application granted granted Critical
Publication of FR2966125B1 publication Critical patent/FR2966125B1/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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
FR1058406A 2010-10-15 2010-10-15 Ensemble d'accrochage d'une suspension d'un ensemble propulsif d'aeronef Active FR2966125B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1058406A FR2966125B1 (fr) 2010-10-15 2010-10-15 Ensemble d'accrochage d'une suspension d'un ensemble propulsif d'aeronef
RU2013121274/11A RU2013121274A (ru) 2010-10-15 2011-10-04 Узел крепления подвесных тяг, на которых подвешена силовая установка летательного аппарата
BR112013007208A BR112013007208A2 (pt) 2010-10-15 2011-10-04 unidade de propulsão e conjunto para ligar os ganhos a partir dos quais a mesma é suspensa
CN2011800486141A CN103153789A (zh) 2010-10-15 2011-10-04 用于悬挂飞行器推进单元的挂架的附接组件
PCT/FR2011/052307 WO2012049399A1 (fr) 2010-10-15 2011-10-04 Ensemble d'accrochage d'une suspension d'un ensemble propulsif d'aéronef
CA2812373A CA2812373A1 (fr) 2010-10-15 2011-10-04 Ensemble d'accrochage d'une suspension d'un ensemble propulsif d'aeronef
EP11779788.6A EP2627561A1 (fr) 2010-10-15 2011-10-04 Ensemble d'accrochage d'une suspension d'un ensemble propulsif d'aéronef
US13/862,724 US8839629B2 (en) 2010-10-15 2013-04-15 Assembly for attaching the hangers from which an aircraft propulsion unit is suspended

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1058406A FR2966125B1 (fr) 2010-10-15 2010-10-15 Ensemble d'accrochage d'une suspension d'un ensemble propulsif d'aeronef

Publications (2)

Publication Number Publication Date
FR2966125A1 FR2966125A1 (fr) 2012-04-20
FR2966125B1 true FR2966125B1 (fr) 2013-04-26

Family

ID=44201296

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1058406A Active FR2966125B1 (fr) 2010-10-15 2010-10-15 Ensemble d'accrochage d'une suspension d'un ensemble propulsif d'aeronef

Country Status (8)

Country Link
US (1) US8839629B2 (fr)
EP (1) EP2627561A1 (fr)
CN (1) CN103153789A (fr)
BR (1) BR112013007208A2 (fr)
CA (1) CA2812373A1 (fr)
FR (1) FR2966125B1 (fr)
RU (1) RU2013121274A (fr)
WO (1) WO2012049399A1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3065442B1 (fr) * 2017-04-25 2021-03-19 Airbus Operations Sas Ensemble moteur pour aeronef comprenant une attache moteur avant integree au caisson du mat d'accrochage
US10458281B2 (en) * 2017-06-12 2019-10-29 United Technologies Corporation Resilient mounting assembly for a turbine engine
FR3086924B1 (fr) * 2018-10-08 2021-02-12 Safran Aircraft Engines Turbomachine comportant des moyens de suspension
CN111846251B (zh) * 2020-07-10 2024-03-19 山东太古飞机工程有限公司 一种用于发动机进气口、排气及尾喷嘴的防沙保护装置
FR3121709B1 (fr) * 2021-04-08 2023-05-05 Safran Aircraft Engines Virole extérieure de carter intermédiaire en matériau composite, pour turbomachine d’aéronef

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3844115A (en) * 1973-02-14 1974-10-29 Gen Electric Load distributing thrust mount
US5649417A (en) * 1995-03-24 1997-07-22 The Boeing Company Fail-safe engine mount system
US5620154A (en) * 1995-05-03 1997-04-15 The Boeing Company Three link failsafe engine mount
US6189830B1 (en) * 1999-02-26 2001-02-20 The Boeing Company Tuned engine mounting system for jet aircraft
US6330995B1 (en) * 2000-02-29 2001-12-18 General Electric Company Aircraft engine mount
US6843449B1 (en) * 2004-02-09 2005-01-18 General Electric Company Fail-safe aircraft engine mounting system
FR2867155B1 (fr) * 2004-03-08 2007-06-29 Snecma Moteurs Suspension d'un moteur a la structure d'un avion
FR2868041B1 (fr) * 2004-03-25 2006-05-26 Snecma Moteurs Sa Suspension d'un moteur d'avion
FR2940359B1 (fr) * 2008-12-18 2014-11-28 Snecma Carter d'echappement pour turbomachine, comportant une ferrure d'accrochage dissociee de la virole exterieure.

Also Published As

Publication number Publication date
FR2966125A1 (fr) 2012-04-20
CA2812373A1 (fr) 2012-04-19
CN103153789A (zh) 2013-06-12
RU2013121274A (ru) 2014-11-20
EP2627561A1 (fr) 2013-08-21
US8839629B2 (en) 2014-09-23
WO2012049399A1 (fr) 2012-04-19
US20130227963A1 (en) 2013-09-05
BR112013007208A2 (pt) 2016-06-14

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