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FR3047726B1 - Mat d'un aeronef - Google Patents

Mat d'un aeronef Download PDF

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Publication number
FR3047726B1
FR3047726B1 FR1651187A FR1651187A FR3047726B1 FR 3047726 B1 FR3047726 B1 FR 3047726B1 FR 1651187 A FR1651187 A FR 1651187A FR 1651187 A FR1651187 A FR 1651187A FR 3047726 B1 FR3047726 B1 FR 3047726B1
Authority
FR
France
Prior art keywords
mast
aircraft
mat
ball joint
assembly
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
FR1651187A
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English (en)
Other versions
FR3047726A1 (fr
Inventor
Eric Haramburu
Antoine COUSIN
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 FR1651187A priority Critical patent/FR3047726B1/fr
Publication of FR3047726A1 publication Critical patent/FR3047726A1/fr
Application granted granted Critical
Publication of FR3047726B1 publication Critical patent/FR3047726B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pivots And Pivotal Connections (AREA)

Abstract

L'invention concerne un mât (100) d'un aéronef présentant un axe longitudinal. Le mât (100) comporte : - une structure primaire (102), - une structure secondaire (104), et - un ensemble structurel (110), ledit ensemble structurel comprenant deux pièces (112, 114) fixées, d'une part, à la structure primaire (102) par une même liaison rotule (120), et, d'autre part, à la structure secondaire (104) par une même liaison rotule (130). Les liaisons rotules facilitent le réglage du mât lors de son assemblage.
FR1651187A 2016-02-15 2016-02-15 Mat d'un aeronef Active FR3047726B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1651187A FR3047726B1 (fr) 2016-02-15 2016-02-15 Mat d'un aeronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1651187A FR3047726B1 (fr) 2016-02-15 2016-02-15 Mat d'un aeronef
FR1651187 2016-02-15

Publications (2)

Publication Number Publication Date
FR3047726A1 FR3047726A1 (fr) 2017-08-18
FR3047726B1 true FR3047726B1 (fr) 2019-05-03

Family

ID=55953242

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1651187A Active FR3047726B1 (fr) 2016-02-15 2016-02-15 Mat d'un aeronef

Country Status (1)

Country Link
FR (1) FR3047726B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2577540A (en) 2018-09-28 2020-04-01 Airbus Operations Ltd Joint for connecting aircraft structures

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2962976B1 (fr) * 2010-07-22 2013-07-26 Airbus Operations Sas Dispositif de liaison destine a relier un premier corps a un second corps, notamment pour ensemble moteur d'aeronef
FR3012416B1 (fr) * 2013-10-31 2017-06-02 Airbus Operations Sas Aeronef comprenant une liaison souple deportee entre un moteur et une structure primaire de mat moteur

Also Published As

Publication number Publication date
FR3047726A1 (fr) 2017-08-18

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