CA2974245C - Method of repairing damage to fuselage barrel and associated apparatus and system - Google Patents

Method of repairing damage to fuselage barrel and associated apparatus and system Download PDF

Info

Publication number
CA2974245C
CA2974245C CA2974245A CA2974245A CA2974245C CA 2974245 C CA2974245 C CA 2974245C CA 2974245 A CA2974245 A CA 2974245A CA 2974245 A CA2974245 A CA 2974245A CA 2974245 C CA2974245 C CA 2974245C
Authority
CA
Canada
Prior art keywords
fuselage barrel
section
splice
fuselage
splice plate
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
CA2974245A
Other languages
English (en)
French (fr)
Other versions
CA2974245A1 (en
Inventor
Remmelt Andrew STAAL
Narbeh Nersessian
Gary D. Oakes
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of CA2974245A1 publication Critical patent/CA2974245A1/en
Application granted granted Critical
Publication of CA2974245C publication Critical patent/CA2974245C/en
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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B64C1/069—Joining arrangements therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/40—Maintaining or repairing aircraft
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Working Measures On Existing Buildindgs (AREA)
  • Moulding By Coating Moulds (AREA)
CA2974245A 2016-09-07 2017-07-19 Method of repairing damage to fuselage barrel and associated apparatus and system Active CA2974245C (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/258,919 2016-09-07
US15/258,919 US10308342B2 (en) 2016-09-07 2016-09-07 Method of repairing damage to fuselage barrel and associated apparatus and system

Publications (2)

Publication Number Publication Date
CA2974245A1 CA2974245A1 (en) 2018-03-07
CA2974245C true CA2974245C (en) 2021-09-28

Family

ID=59315470

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2974245A Active CA2974245C (en) 2016-09-07 2017-07-19 Method of repairing damage to fuselage barrel and associated apparatus and system

Country Status (5)

Country Link
US (2) US10308342B2 (enExample)
EP (1) EP3293105B1 (enExample)
JP (1) JP7012483B2 (enExample)
CN (1) CN107792390B (enExample)
CA (1) CA2974245C (enExample)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
FR3089946B1 (fr) * 2018-12-18 2021-01-08 Airbus Operations Sas structure d’un FUSELAGE D’UN aeronef présentant un panneau renforcé par un treillis
US11427351B2 (en) 2019-12-06 2022-08-30 The Boeing Company Carrier and operational frame system and methods of assembling a structure
EP3978358B1 (en) * 2020-09-30 2024-11-06 The Boeing Company Aircraft fuselage longitudinal splice for joining half barrel fuselage sections and other spliced fuselage sections
US11801576B2 (en) 2020-11-18 2023-10-31 The Boeing Company Aircraft assembly formed of mating half barrel sections and the method of assembling the same
US11724346B2 (en) * 2020-11-18 2023-08-15 The Boeing Company Moving line assembly of airframes
NL2027402B1 (en) * 2021-01-26 2022-08-19 Boeing Co Aircraft assembly formed of mating half barrel sections and the method of assembling the same
US11919617B2 (en) 2020-12-17 2024-03-05 The Boeing Company Circumferential lap splices for sections of fuselage
US12420954B2 (en) * 2023-04-12 2025-09-23 The Boeing Company Composite repair components with customizable shims
US12686486B2 (en) * 2024-05-29 2026-07-21 The Boeing Company Panel assembly for converting passenger aircraft to cargo aircraft
CN119525315B (zh) * 2024-11-14 2025-10-28 中航西安飞机工业集团股份有限公司 一种弱刚性结构飞机钣金框缘偏移修复工装及方法

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US6849150B1 (en) * 2001-01-16 2005-02-01 Lockheed Martin Corporation System and method of forming structural assemblies with 3-D woven joint pre-forms
US7325771B2 (en) 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
FR2901246B1 (fr) * 2006-05-19 2008-06-20 Airbus France Sas Procede de reparation d'une zone endommagee d'un fuselage d'aeronef
US7871040B2 (en) 2006-11-10 2011-01-18 The Boeing Company Composite aircraft structures with hat stiffeners
US8047469B2 (en) * 2008-03-01 2011-11-01 The Boeing Company Airframe attachment fitting
US7967250B2 (en) * 2008-05-12 2011-06-28 EMBRAER—Empresa Brasileira de Aeronáutica Hybrid aircraft fuselage structural components and methods of making same
DE102009009491A1 (de) 2009-02-18 2010-09-09 Airbus Deutschland Gmbh Verfahren zum Herstellen eines Schalenkörpers
FR2953812B1 (fr) * 2009-12-11 2012-09-07 Airbus Operations Sas Procede de reparation d'un fuselage d'aeronef
ES2395604B1 (es) 2010-10-29 2013-12-26 Airbus Operations, S.L. Reparación interior doblada.
US8567722B2 (en) * 2010-12-15 2013-10-29 The Boeing Company Splice and associated method for joining fuselage sections
US8616500B2 (en) 2011-03-04 2013-12-31 The Boeing Company Diamond shaped window for composite and/or metallic airframe
US8844108B2 (en) * 2011-07-12 2014-09-30 The Boeing Company Large area repair of composite aircraft
US8914979B2 (en) * 2011-07-21 2014-12-23 Spirit AcroSystems, Inc. System and method for assembling aircraft components
US8684311B2 (en) * 2012-03-07 2014-04-01 The Boeing Company Bonded splice joint
US8939406B2 (en) * 2012-07-02 2015-01-27 The Boeing Company Joining composite fuselage sections along window belts
US8985512B1 (en) * 2012-09-21 2015-03-24 The Boeing Company Aircraft, fuselages, and associated methods
US8960606B2 (en) 2012-10-31 2015-02-24 The Boeing Company Circumference splice for joining shell structures
GB2517954B (en) 2013-09-05 2018-07-04 Airbus Operations Ltd Repair of a damaged composite aircraft wing
EP2873620B1 (en) 2013-11-14 2018-05-16 Airbus Operations GmbH Repair method for fuselage components of aircraft or spacecraft
FR3037558B1 (fr) * 2015-06-19 2017-05-26 Airbus Operations Sas Procede de fabrication d'un panneau de fuselage par surmoulage et panneau de fuselage ainsi obtenu

Also Published As

Publication number Publication date
CN107792390B (zh) 2022-11-11
JP2018070141A (ja) 2018-05-10
BR102017019045A2 (pt) 2018-05-02
US11104412B2 (en) 2021-08-31
JP7012483B2 (ja) 2022-01-28
CA2974245A1 (en) 2018-03-07
EP3293105B1 (en) 2019-09-04
US10308342B2 (en) 2019-06-04
US20180065761A1 (en) 2018-03-08
CN107792390A (zh) 2018-03-13
US20190248463A1 (en) 2019-08-15
EP3293105A1 (en) 2018-03-14

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