FR3007735B1 - Liaison d'un element de fuselage d'aeronef et d'un cadre par une entretoise et une cale - Google Patents

Liaison d'un element de fuselage d'aeronef et d'un cadre par une entretoise et une cale

Info

Publication number
FR3007735B1
FR3007735B1 FR1356321A FR1356321A FR3007735B1 FR 3007735 B1 FR3007735 B1 FR 3007735B1 FR 1356321 A FR1356321 A FR 1356321A FR 1356321 A FR1356321 A FR 1356321A FR 3007735 B1 FR3007735 B1 FR 3007735B1
Authority
FR
France
Prior art keywords
thrust
spacer
frame
aircraft fuselage
fuselage member
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.)
Expired - Fee Related
Application number
FR1356321A
Other languages
English (en)
Other versions
FR3007735A1 (fr
Inventor
Philippe Bernadet
Yannick Marin
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 FR1356321A priority Critical patent/FR3007735B1/fr
Priority to US14/313,593 priority patent/US20150001343A1/en
Publication of FR3007735A1 publication Critical patent/FR3007735A1/fr
Application granted granted Critical
Publication of FR3007735B1 publication Critical patent/FR3007735B1/fr
Expired - Fee Related 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064—Stringers; Longerons
    • 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Moulding By Coating Moulds (AREA)
FR1356321A 2013-06-28 2013-06-28 Liaison d'un element de fuselage d'aeronef et d'un cadre par une entretoise et une cale Expired - Fee Related FR3007735B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1356321A FR3007735B1 (fr) 2013-06-28 2013-06-28 Liaison d'un element de fuselage d'aeronef et d'un cadre par une entretoise et une cale
US14/313,593 US20150001343A1 (en) 2013-06-28 2014-06-24 Linking an aircraft fuselage member and a frame by a clip and a spacer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1356321A FR3007735B1 (fr) 2013-06-28 2013-06-28 Liaison d'un element de fuselage d'aeronef et d'un cadre par une entretoise et une cale

Publications (2)

Publication Number Publication Date
FR3007735A1 FR3007735A1 (fr) 2015-01-02
FR3007735B1 true FR3007735B1 (fr) 2015-08-07

Family

ID=49111451

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1356321A Expired - Fee Related FR3007735B1 (fr) 2013-06-28 2013-06-28 Liaison d'un element de fuselage d'aeronef et d'un cadre par une entretoise et une cale

Country Status (2)

Country Link
US (1) US20150001343A1 (fr)
FR (1) FR3007735B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3009274A1 (fr) 2013-08-01 2015-02-06 Airbus Operations Sas Element de cadre de fuselage d'aeronef integrant des languettes pour la fixation de raidisseurs
FR3009351B1 (fr) 2013-08-01 2015-08-07 Airbus Operations Sas Outillage pour le maintien simultane de plusieurs clips de fixation contre un element de cadre de fuselage d'aeronef
FR3009352B1 (fr) * 2013-08-01 2016-01-01 Airbus Operations Sas Outillage pour le maintien simultane de plusieurs clips de fixation contre un element de cadre de fuselage d'aeronef
BR112021001184A2 (pt) * 2018-07-25 2021-04-27 Henkel IP & Holding GmbH calço líquido acrílico epoxídico de cura rápida

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4310132A (en) * 1978-02-16 1982-01-12 Nasa Fuselage structure using advanced technology fiber reinforced composites
US5518208A (en) * 1993-12-28 1996-05-21 The Boeing Company Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices
US6712316B2 (en) * 2002-08-01 2004-03-30 The Boeing Company Snap-on sidewall assembly
DE102006026918B4 (de) * 2006-06-09 2017-01-12 Airbus Operations Gmbh Rumpfstruktur
DE102007044386A1 (de) * 2007-09-18 2009-04-02 Airbus Deutschland Gmbh Strukturbauteil und Verfahren zum Versteifen einer Außenhaut
US8490920B2 (en) * 2007-10-12 2013-07-23 Abe Karem Composite bulkhead and skin construction
US7735780B2 (en) * 2007-12-20 2010-06-15 L-3 Communications Integrated Systems, L.P. Aircraft stringer clip and related methods
DE102008006834A1 (de) * 2008-01-30 2009-10-15 Airbus Deutschland Gmbh Verbindungsanordnung zum Verbinden zweier Versteifungselemente unterschiedlichen Querschnittprofils für ein Luft- oder Raumfahrzeug, und ein Schalenbauteil
DE102008012252B4 (de) * 2008-03-03 2014-07-31 Airbus Operations Gmbh Verbund sowie Luft- oder Raumfahrzeug mit einem derartigen Verbund
ES2352941B1 (es) * 2008-05-16 2012-01-25 Airbus Operations, S.L. Estructura integrada de aeronave en material compuesto
DE102009007730B4 (de) * 2009-02-05 2017-12-14 Mbda Deutschland Gmbh Strukturbauteil

Also Published As

Publication number Publication date
FR3007735A1 (fr) 2015-01-02
US20150001343A1 (en) 2015-01-01

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