FR3103788B1 - ASSEMBLY FOR AN AIRCRAFT, THE SUCH ASSEMBLY COMPRISING A MAST, A WING AND A FIXING SYSTEM BETWEEN THE MAST AND THE WING - Google Patents

ASSEMBLY FOR AN AIRCRAFT, THE SUCH ASSEMBLY COMPRISING A MAST, A WING AND A FIXING SYSTEM BETWEEN THE MAST AND THE WING Download PDF

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Publication number
FR3103788B1
FR3103788B1 FR1913363A FR1913363A FR3103788B1 FR 3103788 B1 FR3103788 B1 FR 3103788B1 FR 1913363 A FR1913363 A FR 1913363A FR 1913363 A FR1913363 A FR 1913363A FR 3103788 B1 FR3103788 B1 FR 3103788B1
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FR
France
Prior art keywords
mast
wing
assembly
clevis
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
FR1913363A
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French (fr)
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FR3103788A1 (en
Inventor
Michael Berjot
Sierra Rosa Angelica Cardenas
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 FR1913363A priority Critical patent/FR3103788B1/en
Publication of FR3103788A1 publication Critical patent/FR3103788A1/en
Application granted granted Critical
Publication of FR3103788B1 publication Critical patent/FR3103788B1/en
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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
    • 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)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Connection Of Plates (AREA)

Abstract

ENSEMBLE POUR UN AERONEF, LEDIT ENSEMBLE COMPORTANT UN MAT, UNE AILE ET UN SYSTEME DE FIXATION ENTRE LE MAT ET L’AILE L’invention concerne un ensemble (200) comportant un mât (106) qui comporte un longeron supérieur (202), une aile comportant un longeron avant (210) et un système de fixation (250) avec une ferrure mât (254) fixée au longeron supérieur (202), et comportant des chapes bâbord et tribord (256a-b), pour chaque chape, une ferrure voilure (252a-b) fixée au longeron avant (210), chacune comportant une chape (259a-b), et pour chaque chape (256a-b) des ferrures mât (254), une bielle (258a-b) articulée entre ladite chape (256a-b) et la chape (259a-b) de la ferrure voilure (252a-b) associée, et pour chaque chape (256a-b, 259a-b), un axe (262) qui s’emmanche à travers ladite chape et un alésage de la bielle (258a-b) correspondante. Un tel ensemble permet de limiter la distance entre le mât et l’aile. Fig. 2ASSEMBLY FOR AN AIRCRAFT, SAID ASSEMBLY COMPRISING A MAST, A WING AND A FIXATION SYSTEM BETWEEN THE MAST AND THE WING The invention relates to an assembly (200) comprising a mast (106) which comprises an upper spar (202), a wing comprising a front spar (210) and a fixing system (250) with a mast fitting (254) fixed to the upper spar (202), and comprising port and starboard clevises (256a-b), for each clevis, a fitting wing (252a-b) fixed to the front spar (210), each comprising a clevis (259a-b), and for each clevis (256a-b) mast fittings (254), a connecting rod (258a-b) articulated between said clevis (256a-b) and the clevis (259a-b) of the associated wing fitting (252a-b), and for each clevis (256a-b, 259a-b), a pin (262) which fits through said yoke and a bore of the connecting rod (258a-b) corresponding. Such a set makes it possible to limit the distance between the mast and the wing. Fig. 2

FR1913363A 2019-11-28 2019-11-28 ASSEMBLY FOR AN AIRCRAFT, THE SUCH ASSEMBLY COMPRISING A MAST, A WING AND A FIXING SYSTEM BETWEEN THE MAST AND THE WING Active FR3103788B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1913363A FR3103788B1 (en) 2019-11-28 2019-11-28 ASSEMBLY FOR AN AIRCRAFT, THE SUCH ASSEMBLY COMPRISING A MAST, A WING AND A FIXING SYSTEM BETWEEN THE MAST AND THE WING

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1913363A FR3103788B1 (en) 2019-11-28 2019-11-28 ASSEMBLY FOR AN AIRCRAFT, THE SUCH ASSEMBLY COMPRISING A MAST, A WING AND A FIXING SYSTEM BETWEEN THE MAST AND THE WING
FR1913363 2019-11-28

Publications (2)

Publication Number Publication Date
FR3103788A1 FR3103788A1 (en) 2021-06-04
FR3103788B1 true FR3103788B1 (en) 2022-09-09

Family

ID=69700103

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1913363A Active FR3103788B1 (en) 2019-11-28 2019-11-28 ASSEMBLY FOR AN AIRCRAFT, THE SUCH ASSEMBLY COMPRISING A MAST, A WING AND A FIXING SYSTEM BETWEEN THE MAST AND THE WING

Country Status (1)

Country Link
FR (1) FR3103788B1 (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2905932B1 (en) * 2006-09-20 2008-12-05 Airbus France Sa ARRANGEMENT FOR ATTACHING DEVICE FOR ATTACHING AN AIRCRAFT ENGINE
FR2915178B1 (en) * 2007-04-23 2009-07-10 Airbus France Sa ATTACHMENT OF A MAT BOX ON A SAIL, PINCING A SIDE PANEL OF THE HOUSING
FR2917713B1 (en) * 2007-06-21 2009-09-25 Airbus France Sas APPARATUS FOR ATTACHING AN AIRCRAFT ENGINE AND AIRCRAFT HAVING AT LEAST ONE SUCH DEVICE.
FR2923459B1 (en) * 2007-11-09 2010-05-21 Snecma ROTATING BLOCKING MEANS FOR A AXIS SUPPORTING A TURBOMOTEUR SUSPENSION MEMBER
FR2964364B1 (en) * 2010-09-03 2012-09-28 Airbus Operations Sas AIRCRAFT TURBOJET ENGINEERING MACHINE COMPRISING FRONT VANE FRONT FASTENERS
FR3012793B1 (en) * 2013-11-05 2017-05-05 Airbus Operations Sas AIRCRAFT ASSEMBLY COMPRISING A FASTENER ATTACHED TO THE EXTRADOS PART OF A SAILBOX, FOR MOUNTING A COUPLING MAT ON THIS SAIL BOX

Also Published As

Publication number Publication date
FR3103788A1 (en) 2021-06-04

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