FR2972997B1 - Raccordement d'un fuselage a une voilure d'aeronef - Google Patents

Raccordement d'un fuselage a une voilure d'aeronef

Info

Publication number
FR2972997B1
FR2972997B1 FR1152493A FR1152493A FR2972997B1 FR 2972997 B1 FR2972997 B1 FR 2972997B1 FR 1152493 A FR1152493 A FR 1152493A FR 1152493 A FR1152493 A FR 1152493A FR 2972997 B1 FR2972997 B1 FR 2972997B1
Authority
FR
France
Prior art keywords
fuselage
rib
line
panel
aerofoil
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
FR1152493A
Other languages
English (en)
Other versions
FR2972997A1 (fr
Inventor
Dominique Guittard
Olivier Eve
Frederic Fort
Jerome Colmagro
Francois Loyant
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 FR1152493A priority Critical patent/FR2972997B1/fr
Priority to US13/428,291 priority patent/US8770518B2/en
Publication of FR2972997A1 publication Critical patent/FR2972997A1/fr
Application granted granted Critical
Publication of FR2972997B1 publication Critical patent/FR2972997B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/10—Wings
    • B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
FR1152493A 2011-03-25 2011-03-25 Raccordement d'un fuselage a une voilure d'aeronef Active FR2972997B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1152493A FR2972997B1 (fr) 2011-03-25 2011-03-25 Raccordement d'un fuselage a une voilure d'aeronef
US13/428,291 US8770518B2 (en) 2011-03-25 2012-03-23 Connection of a fuselage to an aircraft wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1152493A FR2972997B1 (fr) 2011-03-25 2011-03-25 Raccordement d'un fuselage a une voilure d'aeronef

Publications (2)

Publication Number Publication Date
FR2972997A1 FR2972997A1 (fr) 2012-09-28
FR2972997B1 true FR2972997B1 (fr) 2013-05-10

Family

ID=44548494

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1152493A Active FR2972997B1 (fr) 2011-03-25 2011-03-25 Raccordement d'un fuselage a une voilure d'aeronef

Country Status (2)

Country Link
US (1) US8770518B2 (fr)
FR (1) FR2972997B1 (fr)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9180956B1 (en) 2012-04-11 2015-11-10 The Boeing Company Methods and apparatus for attaching an aircraft wing assembly to an aircraft body
FR2991228B1 (fr) 2012-05-29 2015-03-06 Airbus Operations Sas Procede et dispositif de realisation d'un panneau composite auto-raidi
US10118686B2 (en) * 2012-09-27 2018-11-06 The Boeing Company Wing root insert system for an aircraft family
US8857765B2 (en) * 2012-10-16 2014-10-14 The Boeing Company Method and apparatus for attaching an aircraft fuselage frame to a wing box
US9527575B2 (en) * 2012-11-26 2016-12-27 The Boeing Company Multi-box wing spar and skin
US9580164B2 (en) 2013-07-10 2017-02-28 The Boeing Company Apparatus and methods for joining aircraft composite structures
US9475570B2 (en) * 2013-08-23 2016-10-25 The Boeing Company Upper joints between outboard wing boxes and wing center sections of aircraft wing assemblies
RU2621925C1 (ru) * 2016-01-28 2017-06-08 Публичное акционерное Общество "Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева" (ПАО "ТАНТК им. Г.М. Бериева") Стык консоли крыла с центропланом самолета
CN110582446B (zh) 2017-05-01 2023-03-31 庞巴迪公司 具有压力翼刀的飞机机翼单元
US11661170B2 (en) 2017-05-01 2023-05-30 Bombardier Inc. Aircraft wing unit with upper wing skin defining pressure floor
FR3078682A1 (fr) 2018-03-09 2019-09-13 Airbus Operations Caisson de torsion pour aeronef forme d'elements soudes deux-a-deux et procede de fabrication de celui-ci
US11401024B2 (en) * 2019-10-09 2022-08-02 The Boeing Company Fuselage sections having tapered wing rib interfaces
US11305862B2 (en) * 2019-12-20 2022-04-19 The Boeing Company Joint joining an aircraft wing to an aircraft body
CN114802698A (zh) 2021-01-27 2022-07-29 波音公司 在飞机中用于连接中央翼盒和隔舱的接头
EP4035993A1 (fr) * 2021-01-27 2022-08-03 The Boeing Company Connecteur pour connecter un caisson de voilure central à une cloison d'un aéronef

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE323283C (de) * 1920-07-19 Flugzeugwerke G M B H Deutsche Flugzeug
FR2901240B1 (fr) * 2006-05-17 2009-01-09 Airbus France Sas Poutre interne composite pour renforcer la structure d'un aeronef
GB0619512D0 (en) * 2006-10-03 2006-11-15 Airbus Uk Ltd Fitting
FR2916417B1 (fr) * 2007-05-23 2009-07-24 Airbus France Sas Element structural d'aeronef situe a l'interface entre une aile et le fuselage
FR2936489B1 (fr) 2008-09-30 2012-07-20 Airbus France Troncon central d'aeronef avec carenage ventral travaillant
FR2948099B1 (fr) * 2009-07-16 2012-05-11 Airbus Operations Sas Procede de fabrication d'un aeronef a voilure fixe

Also Published As

Publication number Publication date
US20120286090A1 (en) 2012-11-15
FR2972997A1 (fr) 2012-09-28
US8770518B2 (en) 2014-07-08

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