FR2887850B1 - Dispositif d'accrochage d'un moteur interpose entre une voilure d'aeronef et ledit moteur - Google Patents

Dispositif d'accrochage d'un moteur interpose entre une voilure d'aeronef et ledit moteur

Info

Publication number
FR2887850B1
FR2887850B1 FR0551818A FR0551818A FR2887850B1 FR 2887850 B1 FR2887850 B1 FR 2887850B1 FR 0551818 A FR0551818 A FR 0551818A FR 0551818 A FR0551818 A FR 0551818A FR 2887850 B1 FR2887850 B1 FR 2887850B1
Authority
FR
France
Prior art keywords
engine
interposed
sail
aircraft
aircraft sail
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
FR0551818A
Other languages
English (en)
Other versions
FR2887850A1 (fr
Inventor
Stephane Levert
Laurent Lafont
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 FR0551818A priority Critical patent/FR2887850B1/fr
Publication of FR2887850A1 publication Critical patent/FR2887850A1/fr
Application granted granted Critical
Publication of FR2887850B1 publication Critical patent/FR2887850B1/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
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0551818A 2005-06-29 2005-06-29 Dispositif d'accrochage d'un moteur interpose entre une voilure d'aeronef et ledit moteur Expired - Fee Related FR2887850B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0551818A FR2887850B1 (fr) 2005-06-29 2005-06-29 Dispositif d'accrochage d'un moteur interpose entre une voilure d'aeronef et ledit moteur

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0551818A FR2887850B1 (fr) 2005-06-29 2005-06-29 Dispositif d'accrochage d'un moteur interpose entre une voilure d'aeronef et ledit moteur

Publications (2)

Publication Number Publication Date
FR2887850A1 FR2887850A1 (fr) 2007-01-05
FR2887850B1 true FR2887850B1 (fr) 2008-11-07

Family

ID=35764466

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0551818A Expired - Fee Related FR2887850B1 (fr) 2005-06-29 2005-06-29 Dispositif d'accrochage d'un moteur interpose entre une voilure d'aeronef et ledit moteur

Country Status (1)

Country Link
FR (1) FR2887850B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2480382C2 (ru) * 2007-07-09 2013-04-27 Эрбюс Операсьон Конструкция для установки двигателя на самолете с присоединенной в четырех точках траверсой

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2914908B1 (fr) 2007-04-13 2009-10-30 Airbus France Sa Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif.
FR2917713B1 (fr) 2007-06-21 2009-09-25 Airbus France Sas Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif.
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
FR2931800B1 (fr) * 2008-05-29 2010-07-30 Airbus France Dispositif de reprise des efforts de poussee pour mat d'accrochage de moteur d'aeronef, comprenant des bielles laterales a butees de palonnier integrees
GB0810791D0 (en) 2008-06-13 2008-07-23 Rolls Royce Plc Thrust mounting arrangement
CA2918320C (fr) 2013-07-26 2018-05-15 Mra Systems, Inc. Mat d'accrochage de moteur pour aeronef
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
FR3127202A1 (fr) * 2021-09-20 2023-03-24 Airbus Operations (S.A.S.) Ensemble de motorisation d’aéronef comprenant un dispositif de reprise d’efforts de poussée

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1236917A (en) * 1967-06-14 1971-06-23 Rolls Royce Improvements in or relating to means for supporting a gas turbine engine in an aircraft
JPH06105048B2 (ja) * 1991-05-28 1994-12-21 ゼネラル・エレクトリック・カンパニイ コアフレームを静翼フレームに安定中央リングで着脱自在に取付ける装置
FR2677954B1 (fr) * 1991-06-19 1993-09-10 Snecma Structure de suspension arriere du carter d'echappement d'un turboreacteur.
US5725181A (en) * 1996-05-01 1998-03-10 The Boeing Company Aircraft engine thrust mount

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2480382C2 (ru) * 2007-07-09 2013-04-27 Эрбюс Операсьон Конструкция для установки двигателя на самолете с присоединенной в четырех точках траверсой

Also Published As

Publication number Publication date
FR2887850A1 (fr) 2007-01-05

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Legal Events

Date Code Title Description
CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

PLFP Fee payment

Year of fee payment: 16

ST Notification of lapse

Effective date: 20220205