GB9312621D0 - Aircraft manufacture - Google Patents

Aircraft manufacture

Info

Publication number
GB9312621D0
GB9312621D0 GB939312621A GB9312621A GB9312621D0 GB 9312621 D0 GB9312621 D0 GB 9312621D0 GB 939312621 A GB939312621 A GB 939312621A GB 9312621 A GB9312621 A GB 9312621A GB 9312621 D0 GB9312621 D0 GB 9312621D0
Authority
GB
United Kingdom
Prior art keywords
fuselage
frame
skins
flying surface
respective upper
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.)
Granted
Application number
GB939312621A
Other versions
GB2268461B (en
GB2268461A (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.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 British Aerospace PLC filed Critical British Aerospace PLC
Publication of GB9312621D0 publication Critical patent/GB9312621D0/en
Publication of GB2268461A publication Critical patent/GB2268461A/en
Application granted granted Critical
Publication of GB2268461B publication Critical patent/GB2268461B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • 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
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces
    • 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
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • 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
    • 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
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic 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)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

A method of manufacturing flying surface and fuselage portions for an aircraft includes the steps of forming respective upper (44) and lower (46, 48) flying surface and fuselage skins at least one of which is an integrated i.e. unitary or one-piece flying surface and fuselage skin; forming a frame (24) including a plurality of transverse integrated fuselage and wing spar elements linked in longitudinal spaced apart relationship by longitudinal support members for supporting the respective upper and lower flying surface fuselage skins; machining the frame so as to match the contours required for the inner surfaces of the upper and lower flying surface skins; and attaching the respective upper and lower flying surface and fuselage skins to said frame. In this way the flying surfaces (wings, for example) and fuselage are both formed from the same structure (frame 24). Thus, the requirement for wing to fuselage attachment points is obviated, therefore saving weight and improving aerodynamic efficiency of the aircraft Frame 24 is of metal. Skins (44, 46, 48) may be of fibre-reinforced composites. <IMAGE>
GB9312621A 1992-06-20 1993-06-18 Aircraft manufacture Expired - Fee Related GB2268461B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB929213211A GB9213211D0 (en) 1992-06-20 1992-06-20 Aircraft manufacture

Publications (3)

Publication Number Publication Date
GB9312621D0 true GB9312621D0 (en) 1993-08-04
GB2268461A GB2268461A (en) 1994-01-12
GB2268461B GB2268461B (en) 1995-07-05

Family

ID=10717510

Family Applications (2)

Application Number Title Priority Date Filing Date
GB929213211A Pending GB9213211D0 (en) 1992-06-20 1992-06-20 Aircraft manufacture
GB9312621A Expired - Fee Related GB2268461B (en) 1992-06-20 1993-06-18 Aircraft manufacture

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB929213211A Pending GB9213211D0 (en) 1992-06-20 1992-06-20 Aircraft manufacture

Country Status (1)

Country Link
GB (2) GB9213211D0 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105644765A (en) * 2014-11-27 2016-06-08 空中客车操作有限责任公司 Aircraft fuselage frame

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2295999A (en) * 1994-12-16 1996-06-19 British Aerospace Aircraft fuselage manufacture
FR2867151B1 (en) * 2004-03-04 2007-05-25 Airbus France FUSELAGE LONGERON FOR AN AIRCRAFT AND CENTRAL BOX EQUIPPED WITH SUCH A LONGERON
FR2901536B1 (en) 2006-05-23 2009-01-30 Airbus France Sas BEAM FOR PRESSURIZED FLOOR OF AIRCRAFT
FR2913412B1 (en) 2007-03-05 2012-12-07 Airbus France CONTAINER FOR AERIAL FREIGHT TRANSPORT AND AIRCRAFT FUSELAGE FOR FREIGHT TRANSPORT.
DE102007019692B4 (en) * 2007-04-26 2011-06-01 Airbus Operations Gmbh Wing-hull section of an airplane
ES2371401B1 (en) * 2008-06-27 2012-11-07 Airbus Operations, S.L. AIRCRAFT SUSTAINER SURFACE STRUCTURE.
FR2946024B1 (en) * 2009-05-27 2011-07-22 Airbus France INSTALLATION FOR CARRYING OUT AN AIRCRAFT FUSELAGE TRUNK
ES2391967B1 (en) * 2010-01-14 2013-10-10 Airbus Operations, S.L. AIRCRAFT ENGINE SUPPORT PILON.
ES2401517B1 (en) 2011-05-31 2014-06-18 Airbus Operations S.L. AIRCRAFT NOTEBOOK IN COMPOSITE MATERIAL.
US9527575B2 (en) 2012-11-26 2016-12-27 The Boeing Company Multi-box wing spar and skin
US9145197B2 (en) * 2012-11-26 2015-09-29 The Boeing Company Vertically integrated stringers
EP4303120A1 (en) * 2022-07-07 2024-01-10 Airbus Operations S.L.U. Composite multi-spar aircraft lifting surface

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105644765A (en) * 2014-11-27 2016-06-08 空中客车操作有限责任公司 Aircraft fuselage frame
CN105644765B (en) * 2014-11-27 2019-04-09 空中客车操作有限责任公司 Aircraft fuselage frame

Also Published As

Publication number Publication date
GB2268461B (en) 1995-07-05
GB2268461A (en) 1994-01-12
GB9213211D0 (en) 1992-08-05

Similar Documents

Publication Publication Date Title
GB2268461B (en) Aircraft manufacture
US20170073078A1 (en) Aircraft engine mounting system
US6726149B2 (en) Derivative aircraft and methods for their manufacture
DE3277502D1 (en) Variable-camber airfoil
WO2008103735A2 (en) Aircraft, and retrofit components therefor
EP0437868A1 (en) Apparatus and methods for reducing aircraft lifting surface flutter
CA2389881A1 (en) Device for recovery of forces generated by an aircraft engine
US4856943A (en) Airfoil incidence angle adjustment method
JPS62501408A (en) Stepped aircraft design and manufacturing methods
Lencus et al. Aircraft wing design automation with ESO and GESO
HUNT High strength aluminum alloys for aerospace application
CN216233067U (en) Repair riveting and shape preserving tool for assembly of middle and rear airframes of airplane
JPS5459798A (en) Aircraft that direction of empennage can be varied
RU2299154C1 (en) Trunk-route aircraft
RU2174931C2 (en) Aircraft antenna fairing
RU2176970C2 (en) Compartment of flying vehicle with external store pylons
RU181678U1 (en) Powerplant - biplane
US20240140610A1 (en) Systems and methods for coupling a strut to a wing of an aircraft
CN209870746U (en) Aircraft with a flight control device
CN110104166B (en) Unmanned aerial vehicle support
CN218537085U (en) Cabin section framework of combined profile structure and cabin body framework
DE50001799D1 (en) aircraft wing
SU1593101A1 (en) Flying vehicle sanitary module
Stefanides For Stiff Aerospace Demands, Aluminum Still Holds the Answer
RU2277058C2 (en) Trunk-route aircraft of variable passenger capacity

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19970618