SG11201400299WA - An aircraft structure - Google Patents

An aircraft structure

Info

Publication number
SG11201400299WA
SG11201400299WA SG11201400299WA SG11201400299WA SG11201400299WA SG 11201400299W A SG11201400299W A SG 11201400299WA SG 11201400299W A SG11201400299W A SG 11201400299WA SG 11201400299W A SG11201400299W A SG 11201400299WA SG 11201400299W A SG11201400299W A SG 11201400299WA
Authority
SG
Singapore
Prior art keywords
aircraft structure
aircraft
Prior art date
Application number
SG11201400299WA
Inventor
David Tighe
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
Publication of SG11201400299WA publication Critical patent/SG11201400299WA/en

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0016—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings of aircraft wings or blades
    • 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
    • B29C73/10—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 using patches sealing on the surface of the article
    • 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
    • B64C3/00—Wings
    • 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
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/187—Ribs
    • 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
    • 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
    • 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
    • B64F5/60—Testing or inspecting aircraft components or systems
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49718—Repairing
    • Y10T29/49732—Repairing by attaching repair preform, e.g., remaking, restoring, or patching
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
SG11201400299WA 2011-09-01 2012-08-07 An aircraft structure SG11201400299WA (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB1115080.2A GB201115080D0 (en) 2011-09-01 2011-09-01 An aircraft structure
PCT/GB2012/051914 WO2013030527A1 (en) 2011-09-01 2012-08-07 An aircraft structure

Publications (1)

Publication Number Publication Date
SG11201400299WA true SG11201400299WA (en) 2014-03-28

Family

ID=44882033

Family Applications (1)

Application Number Title Priority Date Filing Date
SG11201400299WA SG11201400299WA (en) 2011-09-01 2012-08-07 An aircraft structure

Country Status (6)

Country Link
US (1) US9810601B2 (en)
EP (1) EP2750974B1 (en)
CN (1) CN103917450B (en)
GB (1) GB201115080D0 (en)
SG (1) SG11201400299WA (en)
WO (1) WO2013030527A1 (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0715303D0 (en) * 2007-08-08 2007-09-19 Airbus Uk Ltd Composite laminate structure
GB201511402D0 (en) 2015-06-30 2015-08-12 Short Brothers Plc Repair including a chamfered bracket and a chamfered bracket component for reinforcing a damaged structural element made from composite materials
GB2566960A (en) * 2017-09-28 2019-04-03 Airbus Operations Ltd Wing box inspection
US11001363B2 (en) * 2018-11-08 2021-05-11 The Boeing Company Composite spar for aircraft wing
US11180238B2 (en) * 2018-11-19 2021-11-23 The Boeing Company Shear ties for aircraft wing
US10633119B1 (en) * 2018-12-05 2020-04-28 The Boeing Company Methods of testing a monument that is to be attached to a floor of an aircraft
CN110920860A (en) * 2019-12-16 2020-03-27 中国商用飞机有限责任公司 Composite material wing
GB2606009A (en) * 2021-04-22 2022-10-26 Airbus Operations Ltd Aerofoil structures

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2241410B1 (en) 1973-05-18 1976-05-07 Dassault Avions
US4576849A (en) * 1983-06-06 1986-03-18 Hercules Incorporated Curved composite beam
DE3739753A1 (en) 1987-11-24 1989-06-08 Dornier Gmbh Process for producing components from fibre-reinforced plastics
JP2615234B2 (en) 1990-02-13 1997-05-28 防衛庁技術研究本部長 Integrally molded structure with reinforcing body made of fiber reinforced resin composite material
FR2718074B1 (en) * 1994-04-01 1996-04-26 Snecma Method for manufacturing a complex part made of composite material.
US7681835B2 (en) * 1999-11-18 2010-03-23 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
GB0003029D0 (en) 2000-02-11 2000-03-29 British Aerospace A method of reinforcing a laminated member such as a skin for an aircraft
US6638466B1 (en) * 2000-12-28 2003-10-28 Raytheon Aircraft Company Methods of manufacturing separable structures
JP3550104B2 (en) 2001-03-30 2004-08-04 川崎重工業株式会社 Wing reinforcement
JP4713780B2 (en) 2001-07-27 2011-06-29 富士重工業株式会社 Reinforcing panel manufacturing method
JP4574086B2 (en) * 2001-09-03 2010-11-04 富士重工業株式会社 Method for manufacturing composite wing and composite wing
US7159822B2 (en) * 2004-04-06 2007-01-09 The Boeing Company Structural panels for use in aircraft fuselages and other structures
FR2913747B1 (en) 2007-03-16 2009-04-24 Messier Dowty Sa Sa METHOD FOR PRODUCING STIFFENERS IN COMPOSITE MATERIAL
US20080277531A1 (en) 2007-05-11 2008-11-13 The Boeing Company Hybrid Composite Panel Systems and Methods
DE102007029500B4 (en) * 2007-06-25 2013-02-14 Airbus Operations Gmbh Method for coupling stiffening profile elements and structural component

Also Published As

Publication number Publication date
EP2750974A1 (en) 2014-07-09
US20140224043A1 (en) 2014-08-14
WO2013030527A1 (en) 2013-03-07
US9810601B2 (en) 2017-11-07
EP2750974B1 (en) 2017-10-04
CN103917450A (en) 2014-07-09
GB201115080D0 (en) 2011-10-19
CN103917450B (en) 2017-10-24

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