FR3102149B1 - ASSEMBLY FOR AN AIRCRAFT, LEDIT ASSEMBLY CONSISTING OF A MAST, A WING AND A FIXATION SYSTEM BETWEEN THE MAST AND THE WING - Google Patents

ASSEMBLY FOR AN AIRCRAFT, LEDIT ASSEMBLY CONSISTING OF A MAST, A WING AND A FIXATION SYSTEM BETWEEN THE MAST AND THE WING Download PDF

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Publication number
FR3102149B1
FR3102149B1 FR1911701A FR1911701A FR3102149B1 FR 3102149 B1 FR3102149 B1 FR 3102149B1 FR 1911701 A FR1911701 A FR 1911701A FR 1911701 A FR1911701 A FR 1911701A FR 3102149 B1 FR3102149 B1 FR 3102149B1
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FR
France
Prior art keywords
wing
mast
assembly
aircraft
starboard
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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
FR1911701A
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French (fr)
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FR3102149A1 (en
Inventor
Michael Berjot
Julien Cayssials
Jean Geliot
Germain Gueneau
Martin Alberto Merchan
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
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Airbus Operations SAS
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Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1911701A priority Critical patent/FR3102149B1/en
Publication of FR3102149A1 publication Critical patent/FR3102149A1/en
Application granted granted Critical
Publication of FR3102149B1 publication Critical patent/FR3102149B1/en
Active legal-status Critical Current
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Classifications

    • B64D27/40—
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • B64D27/402—

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) pour aéronef comportant un mât (106) avec un longeron inférieur (202) et une nervure arrière (205), une aile (104), et un système de fixation (250) comportant une ferrure voilure (252) fixée sous l’aile (104), une ferrure mât (254) fixée sous le longeron inférieur (202), une bielle (260) à trois alésages, des axe bâbord et tribord (262a-b), où la ferrure voilure (252) comporte des chapes bâbord et tribord (256a-b), où un alésage se fixe dans la chape bâbord (256a) grâce à l’axe bâbord (262a), où un alésage se fixe dans la chape tribord (256b) grâce à l’axe tribord (262b), et où la ferrure mât (254) comporte un arbre (258) qui s’étend vers l’arrière et s’emmanche dans un alésage. Un tel ensemble permet de limiter la distance entre le mât et l’aile tout en conservant une distance importante pour intégrer les éléments du système de fixation. Fig. 2ASSEMBLY FOR AN AIRCRAFT, SAID ASSEMBLY COMPRISING A MAST, A WING AND A FIXING SYSTEM BETWEEN THE MAST AND THE WING The invention relates to an assembly (200) for an aircraft comprising a mast (106) with a lower spar (202) and a rear rib (205), a wing (104), and a fixing system (250) comprising a wing fitting (252) fixed under the wing (104), a mast fitting (254) fixed under the lower spar (202 ), a connecting rod (260) with three bores, port and starboard axles (262a-b), where the sail fitting (252) has port and starboard yokes (256a-b), where a bore is fixed in the port yoke (256a) thanks to the port axis (262a), where a bore is fixed in the starboard yoke (256b) thanks to the starboard axis (262b), and where the mast fitting (254) comprises a shaft (258) which extends rearward and fits into a bore. Such an assembly makes it possible to limit the distance between the mast and the wing while maintaining a significant distance to integrate the elements of the fixing system. Fig. 2

FR1911701A 2019-10-18 2019-10-18 ASSEMBLY FOR AN AIRCRAFT, LEDIT ASSEMBLY CONSISTING OF A MAST, A WING AND A FIXATION SYSTEM BETWEEN THE MAST AND THE WING Active FR3102149B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1911701A FR3102149B1 (en) 2019-10-18 2019-10-18 ASSEMBLY FOR AN AIRCRAFT, LEDIT ASSEMBLY CONSISTING OF A MAST, A WING AND A FIXATION SYSTEM BETWEEN THE MAST AND THE WING

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1911701 2019-10-18
FR1911701A FR3102149B1 (en) 2019-10-18 2019-10-18 ASSEMBLY FOR AN AIRCRAFT, LEDIT ASSEMBLY CONSISTING OF A MAST, A WING AND A FIXATION SYSTEM BETWEEN THE MAST AND THE WING

Publications (2)

Publication Number Publication Date
FR3102149A1 FR3102149A1 (en) 2021-04-23
FR3102149B1 true FR3102149B1 (en) 2021-11-12

Family

ID=69810961

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1911701A Active FR3102149B1 (en) 2019-10-18 2019-10-18 ASSEMBLY FOR AN AIRCRAFT, LEDIT ASSEMBLY CONSISTING OF A MAST, A WING AND A FIXATION SYSTEM BETWEEN THE MAST AND THE WING

Country Status (1)

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FR (1) FR3102149B1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5054715A (en) * 1988-11-10 1991-10-08 The Boeing Company Apparatus and methods for reducing aircraft lifting surface flutter
FR2878229B1 (en) * 2004-11-23 2008-04-18 Airbus France Sas SYSTEM FOR ATTACHING A MOTOR MAT TO THE WING OF AN AIRCRAFT
FR2909973B1 (en) * 2006-12-13 2009-03-20 Airbus France Sa AIRBORNE TURBOBOREACTER HANDLING MACHINE HAVING REDUCED CROSS-BODY REAR STRUCTURE
FR3065441B1 (en) * 2017-04-19 2019-07-05 Airbus Operations AIRCRAFT ASSEMBLY COMPRISING A PRIMARY STRUCTURE OF A COUPLING MAT FIXED TO A SAILBOX USING A BOLT CONNECTION

Also Published As

Publication number Publication date
FR3102149A1 (en) 2021-04-23

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