GB201313636D0 - Aircraft Structure - Google Patents

Aircraft Structure

Info

Publication number
GB201313636D0
GB201313636D0 GBGB1313636.1A GB201313636A GB201313636D0 GB 201313636 D0 GB201313636 D0 GB 201313636D0 GB 201313636 A GB201313636 A GB 201313636A GB 201313636 D0 GB201313636 D0 GB 201313636D0
Authority
GB
United Kingdom
Prior art keywords
aircraft structure
aircraft
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.)
Withdrawn
Application number
GBGB1313636.1A
Other versions
GB2516830A (en
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 Ltd
Original Assignee
Airbus Operations Ltd
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 Ltd filed Critical Airbus Operations Ltd
Priority to GB1313636.1A priority Critical patent/GB2516830A/en
Publication of GB201313636D0 publication Critical patent/GB201313636D0/en
Priority to PCT/GB2014/052008 priority patent/WO2015015152A1/en
Publication of GB2516830A publication Critical patent/GB2516830A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/187—Ribs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/182—Stringers, longerons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
GB1313636.1A 2013-07-31 2013-07-31 Aircraft Structure Withdrawn GB2516830A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB1313636.1A GB2516830A (en) 2013-07-31 2013-07-31 Aircraft Structure
PCT/GB2014/052008 WO2015015152A1 (en) 2013-07-31 2014-07-02 Aircraft structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1313636.1A GB2516830A (en) 2013-07-31 2013-07-31 Aircraft Structure

Publications (2)

Publication Number Publication Date
GB201313636D0 true GB201313636D0 (en) 2013-09-11
GB2516830A GB2516830A (en) 2015-02-11

Family

ID=49167211

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1313636.1A Withdrawn GB2516830A (en) 2013-07-31 2013-07-31 Aircraft Structure

Country Status (2)

Country Link
GB (1) GB2516830A (en)
WO (1) WO2015015152A1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2528076B (en) 2014-07-08 2020-07-29 Airbus Operations Ltd Rib foot
GB2528080A (en) 2014-07-08 2016-01-13 Airbus Operations Ltd Structure
GB2528078B (en) 2014-07-08 2020-07-29 Airbus Operations Ltd Structure
US11180238B2 (en) * 2018-11-19 2021-11-23 The Boeing Company Shear ties for aircraft wing
GB2583940A (en) * 2019-05-14 2020-11-18 Airbus Operations Ltd Aircraft panel assembly
EP4269059A3 (en) 2019-05-14 2023-12-27 Airbus Operations Limited Aircraft wing assembly
CN110406657B (en) * 2019-07-31 2021-06-01 中国商用飞机有限责任公司北京民用飞机技术研究中心 Civil aircraft wing upper wall plate root connecting corner box, connecting structure and wing
CN112193432B (en) * 2020-08-21 2022-04-12 浙江大学 Method for installing aircraft wall panel and method for calculating assembly clearance between aircraft wall panel and framework
CN113428378B (en) * 2021-08-12 2023-10-20 中航西安飞机工业集团股份有限公司 Wing rib positioning and checking method
GB2612958B (en) * 2021-11-08 2023-12-20 Airbus Operations Ltd Panel assembly

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
JP4416900B2 (en) * 2000-03-10 2010-02-17 富士重工業株式会社 Composite panel and method for manufacturing the same
US6386481B1 (en) * 2001-01-08 2002-05-14 Patria Finavicomp Oy Arrangement for fastening stringers to aircraft wing ribs
US7159822B2 (en) * 2004-04-06 2007-01-09 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7635106B2 (en) * 2006-11-30 2009-12-22 The Boeing Company Composite shear tie
FR2923800B1 (en) * 2007-11-16 2010-05-21 Airbus France DEVICE FOR CONNECTING AN INTERNAL STRUCTURE PART OF AN AIRCRAFT AND THE FUSELAGE THEREOF
DE102007055233A1 (en) * 2007-11-20 2009-05-28 Airbus Deutschland Gmbh Coupling device for joining fuselage sections, combination of a coupling device and at least one fuselage section and method for producing the coupling device
FR2970463B1 (en) * 2011-01-17 2013-02-15 Airbus Operations Sas LIGHTING DEVICE WITH IMPROVED MECHANICAL STRENGTH.
FR2970942B1 (en) * 2011-01-28 2013-02-22 Airbus Operations Sas CONNECTING STIFF FRAMES BETWEEN AN AIRCRAFT FUSELAGE AND A VESSEL HOUSING

Also Published As

Publication number Publication date
WO2015015152A1 (en) 2015-02-05
GB2516830A (en) 2015-02-11

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)