FR2954544B1 - Procede de conception de kits de reparation standardises pour fuselage d'aeronef - Google Patents

Procede de conception de kits de reparation standardises pour fuselage d'aeronef

Info

Publication number
FR2954544B1
FR2954544B1 FR0959118A FR0959118A FR2954544B1 FR 2954544 B1 FR2954544 B1 FR 2954544B1 FR 0959118 A FR0959118 A FR 0959118A FR 0959118 A FR0959118 A FR 0959118A FR 2954544 B1 FR2954544 B1 FR 2954544B1
Authority
FR
France
Prior art keywords
repair kits
aircraft fuselage
designing
external
area
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
FR0959118A
Other languages
English (en)
Other versions
FR2954544A1 (fr
Inventor
Gilles Tardu
Andre Galliot
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
Airbus SAS
Original Assignee
Airbus Operations SAS
Airbus 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, Airbus SAS filed Critical Airbus Operations SAS
Priority to FR0959118A priority Critical patent/FR2954544B1/fr
Priority to CN201080062809.7A priority patent/CN102741846B/zh
Priority to PCT/FR2010/052712 priority patent/WO2011073566A1/fr
Priority to US13/516,394 priority patent/US20130024165A1/en
Priority to EP10809008A priority patent/EP2513823A1/fr
Publication of FR2954544A1 publication Critical patent/FR2954544A1/fr
Application granted granted Critical
Publication of FR2954544B1 publication Critical patent/FR2954544B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00—Computer-aided design [CAD]
    • G06F30/10—Geometric CAD
    • G06F30/15—Vehicle, aircraft or watercraft design
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
    • B29C73/04—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F2113/00—Details relating to the application field
    • G06F2113/28—Fuselage, exterior or interior

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Theoretical Computer Science (AREA)
  • Mathematical Optimization (AREA)
  • Computational Mathematics (AREA)
  • Manufacturing & Machinery (AREA)
  • Mathematical Analysis (AREA)
  • Transportation (AREA)
  • Pure & Applied Mathematics (AREA)
  • Computer Hardware Design (AREA)
  • Evolutionary Computation (AREA)
  • General Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)
FR0959118A 2009-12-17 2009-12-17 Procede de conception de kits de reparation standardises pour fuselage d'aeronef Expired - Fee Related FR2954544B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR0959118A FR2954544B1 (fr) 2009-12-17 2009-12-17 Procede de conception de kits de reparation standardises pour fuselage d'aeronef
CN201080062809.7A CN102741846B (zh) 2009-12-17 2010-12-14 航空器机身用的标准化修理包的设计方法
PCT/FR2010/052712 WO2011073566A1 (fr) 2009-12-17 2010-12-14 Procédé de conception de kits de réparation standardisés pour fuselage d'aéronef
US13/516,394 US20130024165A1 (en) 2009-12-17 2010-12-14 Method for designing standardised repair kits for an aircraft fuselage
EP10809008A EP2513823A1 (fr) 2009-12-17 2010-12-14 Procédé de conception de kits de réparation standardisés pour fuselage d'aéronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0959118A FR2954544B1 (fr) 2009-12-17 2009-12-17 Procede de conception de kits de reparation standardises pour fuselage d'aeronef

Publications (2)

Publication Number Publication Date
FR2954544A1 FR2954544A1 (fr) 2011-06-24
FR2954544B1 true FR2954544B1 (fr) 2013-11-22

Family

ID=41819701

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0959118A Expired - Fee Related FR2954544B1 (fr) 2009-12-17 2009-12-17 Procede de conception de kits de reparation standardises pour fuselage d'aeronef

Country Status (5)

Country Link
US (1) US20130024165A1 (fr)
EP (1) EP2513823A1 (fr)
CN (1) CN102741846B (fr)
FR (1) FR2954544B1 (fr)
WO (1) WO2011073566A1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2953812B1 (fr) * 2009-12-11 2012-09-07 Airbus Operations Sas Procede de reparation d'un fuselage d'aeronef
FR3016963B1 (fr) 2014-01-27 2016-01-22 Airbus Dispositif et procede de localisation d'impacts sur une surface externe d'un corps
US9646431B2 (en) * 2014-10-22 2017-05-09 The Boeing Company Augmented reality system for assessing an affected area of an aircraft
CN104386263A (zh) * 2014-11-12 2015-03-04 沈阳航空航天大学 一种飞机上z型长桁的拼接修理方法
CN106275499B (zh) * 2016-08-22 2018-07-13 中国航空工业集团公司西安飞机设计研究所 一种飞机结构死角处防腐蚀设计方法
US11865647B2 (en) * 2020-03-13 2024-01-09 The Boeing Company Utilization of CNC machining in composite part rework

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6219930B1 (en) * 1998-02-27 2001-04-24 Randall M. McPherson Apparatus and method of use for calculating an estimate of damaged surface repair cost
US7707058B2 (en) * 2001-08-31 2010-04-27 Hewlett-Packard Development Company, L.P. Predicting parts needed for an onsite repair using expected waste derived from repair history
CN1361039A (zh) * 2002-01-29 2002-07-31 许陆文 飞行器结构损伤复合材料快速修复技术与设备
US6876950B2 (en) * 2002-04-26 2005-04-05 The Boeing Company System and method for damage evaluation
US20070095457A1 (en) * 2005-11-02 2007-05-03 The Boeing Company Fast line maintenance repair method and system for composite structures
US8560376B2 (en) * 2007-05-31 2013-10-15 Airbus Operations S.A.S. Method, system, and computer program product for a maintenance optimization model
US20090234616A1 (en) * 2008-02-21 2009-09-17 Syncretek Llc Automatic Repair Planning and Part Archival System (ARPPAS)
US8209838B2 (en) * 2008-12-19 2012-07-03 The Boeing Company Repairing composite structures
US8977528B2 (en) * 2009-04-27 2015-03-10 The Boeing Company Bonded rework simulation tool

Also Published As

Publication number Publication date
WO2011073566A1 (fr) 2011-06-23
US20130024165A1 (en) 2013-01-24
CN102741846A (zh) 2012-10-17
FR2954544A1 (fr) 2011-06-24
EP2513823A1 (fr) 2012-10-24
CN102741846B (zh) 2015-09-16

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Effective date: 20190905