DE68914547T2 - Träger mit kastenförmiger Struktur. - Google Patents

Träger mit kastenförmiger Struktur.

Info

Publication number
DE68914547T2
DE68914547T2 DE68914547T DE68914547T DE68914547T2 DE 68914547 T2 DE68914547 T2 DE 68914547T2 DE 68914547 T DE68914547 T DE 68914547T DE 68914547 T DE68914547 T DE 68914547T DE 68914547 T2 DE68914547 T2 DE 68914547T2
Authority
DE
Germany
Prior art keywords
carrier
box
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
DE68914547T
Other languages
English (en)
Other versions
DE68914547D1 (de
Inventor
David Stephen
Martin Henry Mansbridge
David John Irwin
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 DE68914547D1 publication Critical patent/DE68914547D1/de
Application granted granted Critical
Publication of DE68914547T2 publication Critical patent/DE68914547T2/de
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
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • 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
    • 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
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • Y10T29/49339—Hollow blade

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Welding Or Cutting Using Electron Beams (AREA)
  • Laminated Bodies (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
DE68914547T 1988-08-17 1989-08-17 Träger mit kastenförmiger Struktur. Expired - Fee Related DE68914547T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB888819535A GB8819535D0 (en) 1988-08-17 1988-08-17 Wing flap track beams for aircraft

Publications (2)

Publication Number Publication Date
DE68914547D1 DE68914547D1 (de) 1994-05-19
DE68914547T2 true DE68914547T2 (de) 1994-07-28

Family

ID=10642264

Family Applications (1)

Application Number Title Priority Date Filing Date
DE68914547T Expired - Fee Related DE68914547T2 (de) 1988-08-17 1989-08-17 Träger mit kastenförmiger Struktur.

Country Status (6)

Country Link
US (1) US4989774A (de)
EP (1) EP0356142B1 (de)
JP (1) JPH02114091A (de)
DE (1) DE68914547T2 (de)
ES (1) ES2050808T3 (de)
GB (1) GB8819535D0 (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5385204A (en) * 1989-08-25 1995-01-31 Rolls-Royce Plc Heat exchanger and methods of manufacture thereof
US5287918A (en) * 1990-06-06 1994-02-22 Rolls-Royce Plc Heat exchangers
US5505256A (en) * 1991-02-19 1996-04-09 Rolls-Royce Plc Heat exchangers and methods of manufacture thereof
GB9121107D0 (en) * 1991-10-04 1991-11-20 British Aerospace Improvements relating to diffusion bonded/superplastically formed cellular structures
GB9304041D0 (en) * 1993-02-27 1993-04-14 British Aerospace Forming of metal articles
ES2197727B1 (es) * 2000-07-27 2005-04-01 Construcciones Aeronauticas, S.A. Borde de ataque de superficies sustentadoras de aeronaves.
AT410656B (de) * 2001-10-24 2003-06-25 Fischer Adv Components Gmbh Trag- bzw. führungsvorrichtung für flugzeugkomponenten
US20030209318A1 (en) * 2002-05-09 2003-11-13 Henthorn John R. Method for manufacturing fabricated OSB studs
DE10257041B3 (de) * 2002-12-06 2004-08-19 Terex Germany Gmbh & Co. Kg Profil für Tieflöffel und -Ladeschaufelausrüstungen eines Baggers sowie Verfahren zur Herstellung desselben
GB2409443A (en) * 2003-12-23 2005-06-29 Airbus Uk Ltd Rib for an aircraft and the manufacture thereof
DE102014106930A1 (de) 2014-05-16 2015-11-19 Airbus Operations Gmbh Lasttragendes Verkleidungselement für eine Klappenverstellmechanik und Flugzeug mit einem solchen Verkleidungselement
DE202017104032U1 (de) * 2017-05-31 2018-09-18 Liebherr-Werk Biberach Gmbh Tragwerk für einen Kran und ähnliche Arbeitsmaschinen, sowie Kran mit einem solchen Tragwerk
CN110480149B (zh) * 2019-08-02 2021-04-20 南阳师范学院 一种Ti2AlNb基合金四层中空结构及其制造方法
CN114799621A (zh) * 2022-02-22 2022-07-29 中铁宝桥（扬州）有限公司 一种大型桥梁钢箱梁块体组焊工艺
US20240002037A1 (en) * 2022-06-29 2024-01-04 The Boeing Company Failsafe determinate flap support underwing attachment

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4087037A (en) * 1976-07-09 1978-05-02 Mcdonnell Douglas Corporation Method of and tools for producing superplastically formed and diffusion bonded structures
US4304821A (en) * 1978-04-18 1981-12-08 Mcdonnell Douglas Corporation Method of fabricating metallic sandwich structure
US4294419A (en) * 1979-01-22 1981-10-13 Vought Corporation Airframe assembly and process
US4292375A (en) * 1979-05-30 1981-09-29 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Superplastically formed diffusion bonded metallic structure
GB8411611D0 (en) * 1984-05-05 1984-06-13 British Aerospace Superplastic forming of panels
GB8428064D0 (en) * 1984-11-06 1984-12-12 British Aerospace Forming complex hollow sectioned members
US4642863A (en) * 1985-04-15 1987-02-17 Ontario Technologies Corporation Manufacturing method for hollow metal airfoil type structure
US4882123A (en) * 1988-03-01 1989-11-21 General Electric Company Hafnium control rod for nuclear reactors

Also Published As

Publication number Publication date
GB8819535D0 (en) 1988-09-21
DE68914547D1 (de) 1994-05-19
US4989774A (en) 1991-02-05
EP0356142A3 (en) 1990-11-28
EP0356142B1 (de) 1994-04-13
JPH02114091A (ja) 1990-04-26
ES2050808T3 (es) 1994-06-01
EP0356142A2 (de) 1990-02-28

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: BAE SYSTEMS PLC, FARNBOROUGH, HAMPSHIRE, GB

8339 Ceased/non-payment of the annual fee