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FR3125020B3 - FRONT ASSEMBLY OF AN AIRCRAFT MAST AND ENGINE - Google Patents

FRONT ASSEMBLY OF AN AIRCRAFT MAST AND ENGINE Download PDF

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Publication number
FR3125020B3
FR3125020B3 FR2107273A FR2107273A FR3125020B3 FR 3125020 B3 FR3125020 B3 FR 3125020B3 FR 2107273 A FR2107273 A FR 2107273A FR 2107273 A FR2107273 A FR 2107273A FR 3125020 B3 FR3125020 B3 FR 3125020B3
Authority
FR
France
Prior art keywords
mast
engine
assembly
aircraft
rib
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
FR2107273A
Other languages
French (fr)
Other versions
FR3125020A3 (en
Inventor
Jean Geliot
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 FR2107273A priority Critical patent/FR3125020B3/en
Publication of FR3125020A3 publication Critical patent/FR3125020A3/en
Application granted granted Critical
Publication of FR3125020B3 publication Critical patent/FR3125020B3/en
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

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

ASSEMBLAGE AVANT D’UN MÂT ET D’UN MOTEUR D’AERONEF L’invention concerne un assemblage d’un moteur (5) avec un mât (3) d’aéronef, le mât (3) s’étendant d’avant en arrière selon un axe longitudinal (X) et comprenant une nervure avant (3d) formant une face avant du mât et s’étendant perpendiculairement à un plan médian longitudinal (V) du mât (3), l’assemblage comprenant une attache moteur avant (10) assurant une liaison mécanique entre le moteur (5) et le mât (3), l’attache moteur avant (10) étant fixée à la nervure avant du mât (3) au moyen d’une potence (30) sous laquelle l’attache moteur avant (10) est suspendue, la potence (30) comprenant une surface plane d’accostage à laquelle l’attache moteur avant (10) est fixée, la surface plane d’accostage s’étendant vers l’avant du mât (3) perpendiculairement à la nervure avant (3d). Fig. 2FRONT ASSEMBLY OF AN AIRCRAFT MAST AND ENGINE The invention relates to an assembly of an engine (5) with an aircraft mast (3), the mast (3) extending from front to rear along a longitudinal axis (X) and comprising a front rib (3d) forming a front face of the mast and extending perpendicular to a longitudinal median plane (V) of the mast (3), the assembly comprising a front engine attachment (10 ) ensuring a mechanical connection between the engine (5) and the mast (3), the front engine attachment (10) being fixed to the front rib of the mast (3) by means of a bracket (30) under which the front engine attachment (10) is suspended, the bracket (30) comprising a flat docking surface to which the front engine attachment (10) is fixed, the flat docking surface extending towards the front of the mast ( 3) perpendicular to the front rib (3d). Fig. 2

FR2107273A 2021-07-06 2021-07-06 FRONT ASSEMBLY OF AN AIRCRAFT MAST AND ENGINE Active FR3125020B3 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2107273A FR3125020B3 (en) 2021-07-06 2021-07-06 FRONT ASSEMBLY OF AN AIRCRAFT MAST AND ENGINE

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2107273 2021-07-06
FR2107273A FR3125020B3 (en) 2021-07-06 2021-07-06 FRONT ASSEMBLY OF AN AIRCRAFT MAST AND ENGINE

Publications (2)

Publication Number Publication Date
FR3125020A3 FR3125020A3 (en) 2023-01-13
FR3125020B3 true FR3125020B3 (en) 2023-08-25

Family

ID=84802169

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2107273A Active FR3125020B3 (en) 2021-07-06 2021-07-06 FRONT ASSEMBLY OF AN AIRCRAFT MAST AND ENGINE

Country Status (1)

Country Link
FR (1) FR3125020B3 (en)

Also Published As

Publication number Publication date
FR3125020A3 (en) 2023-01-13

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