FR2963608B1 - Adaptateur destine a etre interpose entre une structure rigide de mat d'accrochage de turbomoteur d'aeronef et un element de voilure - Google Patents

Adaptateur destine a etre interpose entre une structure rigide de mat d'accrochage de turbomoteur d'aeronef et un element de voilure

Info

Publication number
FR2963608B1
FR2963608B1 FR1056434A FR1056434A FR2963608B1 FR 2963608 B1 FR2963608 B1 FR 2963608B1 FR 1056434 A FR1056434 A FR 1056434A FR 1056434 A FR1056434 A FR 1056434A FR 2963608 B1 FR2963608 B1 FR 2963608B1
Authority
FR
France
Prior art keywords
turboker
interrupting
aircraft
adapter
rigid 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
FR1056434A
Other languages
English (en)
Other versions
FR2963608A1 (fr
Inventor
Daniel Kierbel
Eric Haramburu
Florent Simondin
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
Airbus SAS
Original Assignee
Airbus Operations SAS
Airbus 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, Airbus SAS filed Critical Airbus Operations SAS
Priority to FR1056434A priority Critical patent/FR2963608B1/fr
Publication of FR2963608A1 publication Critical patent/FR2963608A1/fr
Application granted granted Critical
Publication of FR2963608B1 publication Critical patent/FR2963608B1/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
    • B64D27/16—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
FR1056434A 2010-08-04 2010-08-04 Adaptateur destine a etre interpose entre une structure rigide de mat d'accrochage de turbomoteur d'aeronef et un element de voilure Active FR2963608B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1056434A FR2963608B1 (fr) 2010-08-04 2010-08-04 Adaptateur destine a etre interpose entre une structure rigide de mat d'accrochage de turbomoteur d'aeronef et un element de voilure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1056434A FR2963608B1 (fr) 2010-08-04 2010-08-04 Adaptateur destine a etre interpose entre une structure rigide de mat d'accrochage de turbomoteur d'aeronef et un element de voilure

Publications (2)

Publication Number Publication Date
FR2963608A1 FR2963608A1 (fr) 2012-02-10
FR2963608B1 true FR2963608B1 (fr) 2013-08-16

Family

ID=43769193

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1056434A Active FR2963608B1 (fr) 2010-08-04 2010-08-04 Adaptateur destine a etre interpose entre une structure rigide de mat d'accrochage de turbomoteur d'aeronef et un element de voilure

Country Status (1)

Country Link
FR (1) FR2963608B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107054670A (zh) * 2016-01-07 2017-08-18 波音公司 性能增强的喷气发动机安装支柱

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2918320C (fr) 2013-07-26 2018-05-15 Mra Systems, Inc. Mat d'accrochage de moteur pour aeronef
GB2580980A (en) 2019-02-04 2020-08-05 Airbus Operations Ltd Interfaces between components
FR3102151B1 (fr) * 2019-10-21 2021-10-29 Airbus Operations Sas Aéronef comprenant une attache voilure arrière présentant au moins deux bielles latérales et un pion de cisaillement
GB2592268A (en) * 2020-02-24 2021-08-25 Airbus Operations Ltd Aircraft wing-pylon connection

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4555078A (en) * 1983-12-27 1985-11-26 Societe Belge D'exploitation De La Navigation Aerienne (Sabena) Apparatus for the suspension of an aircraft engine cowling
US5127606A (en) * 1990-11-16 1992-07-07 Allied-Signal Inc. Aircraft engine mount adapter and method
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
FR2920408B1 (fr) * 2007-08-30 2010-02-19 Snecma Pylone de suspension d'un moteur sous une aile d'avion

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107054670A (zh) * 2016-01-07 2017-08-18 波音公司 性能增强的喷气发动机安装支柱
CN107054670B (zh) * 2016-01-07 2021-12-21 波音公司 性能增强的喷气发动机安装支柱

Also Published As

Publication number Publication date
FR2963608A1 (fr) 2012-02-10

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