ATE325034T1 - Verbundwerkstoffstruktur - Google Patents

Verbundwerkstoffstruktur

Info

Publication number
ATE325034T1
ATE325034T1 AT02755321T AT02755321T ATE325034T1 AT E325034 T1 ATE325034 T1 AT E325034T1 AT 02755321 T AT02755321 T AT 02755321T AT 02755321 T AT02755321 T AT 02755321T AT E325034 T1 ATE325034 T1 AT E325034T1
Authority
AT
Austria
Prior art keywords
laminated
portions
rib
regions
corner portion
Prior art date
Application number
AT02755321T
Other languages
English (en)
Inventor
Kays Clement Kairouz
Original Assignee
Bae Systems 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 Bae Systems Plc filed Critical Bae Systems Plc
Application granted granted Critical
Publication of ATE325034T1 publication Critical patent/ATE325034T1/de

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
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • 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
    • 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)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
  • Glass Compositions (AREA)
AT02755321T 2001-09-13 2002-09-06 Verbundwerkstoffstruktur ATE325034T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0122050.8A GB0122050D0 (en) 2001-09-13 2001-09-13 Composite material structure

Publications (1)

Publication Number Publication Date
ATE325034T1 true ATE325034T1 (de) 2006-06-15

Family

ID=9921965

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02755321T ATE325034T1 (de) 2001-09-13 2002-09-06 Verbundwerkstoffstruktur

Country Status (9)

Country Link
US (1) US7380753B2 (de)
EP (1) EP1425215B1 (de)
AT (1) ATE325034T1 (de)
CA (1) CA2459167C (de)
DE (1) DE60211185T2 (de)
ES (1) ES2258645T3 (de)
GB (1) GB0122050D0 (de)
NO (1) NO322021B1 (de)
WO (1) WO2003022677A1 (de)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0219451D0 (en) * 2002-08-21 2002-09-25 Bae Systems Plc A bracket
EP1495859B1 (de) * 2003-07-08 2008-09-03 Airbus Deutschland GmbH Leichtbaustruktur
EP1666354B1 (de) * 2004-12-01 2010-09-29 Airbus Operations GmbH Strukturbauteil, Verfahren zum Herstellen eines Strukturbauteils und Verwendung eines Strukturbauteils für eine Flugzeugschale
GB0525691D0 (en) * 2005-12-16 2006-01-25 Airbus Uk Ltd A fastener assembly
US7721995B2 (en) * 2006-12-13 2010-05-25 The Boeing Company Rib support for wing panels
GB0813584D0 (en) 2008-07-25 2008-09-03 Airbus Uk Ltd Method of stiffening a rib
ES2372828B1 (es) * 2008-12-17 2012-12-13 Airbus Operations, S.L. Costilla-herraje.
GB0906952D0 (en) 2009-04-23 2009-06-03 Airbus Uk Ltd Aircraft assembly and spar
BRPI1012058B1 (pt) * 2009-05-28 2020-06-02 Societe Lorraine De Construction Aeronautique Método para fabricar um painel de estruturação composto
US8408493B2 (en) * 2010-05-19 2013-04-02 The Boeing Company Composite stringer end trim
GB201110973D0 (en) * 2011-06-28 2011-08-10 Airbus Operations Ltd Bracket
US8758879B2 (en) * 2012-06-24 2014-06-24 The Boeing Company Composite hat stiffener, composite hat-stiffened pressure webs, and methods of making the same
US9327470B1 (en) * 2012-12-05 2016-05-03 The Boeing Company Variable-radius laminated radius filler and system and method for manufacturing same
EP3100852B1 (de) * 2015-06-03 2017-11-15 Tusas-Türk Havacilik Ve Uzay Sanayii A.S. Gebogene laminierte struktur
CN105151271B (zh) * 2015-09-21 2017-12-22 中国运载火箭技术研究院 一种外形贯穿飞行器机身的复合材料梁结构
US10046525B2 (en) 2016-09-30 2018-08-14 The Boeing Company Advanced variable radius laminated composite radius filler
CN109625245A (zh) * 2018-11-02 2019-04-16 中国航空工业集团公司西安飞机设计研究所 一种通用飞机复合材料方向舵及制作方法
CN109334944B (zh) * 2018-11-12 2021-02-26 中国直升机设计研究所 一种飞机支撑骨架
US11180238B2 (en) * 2018-11-19 2021-11-23 The Boeing Company Shear ties for aircraft wing
CN114261506B (zh) * 2021-12-31 2024-06-07 中国航空工业集团公司西安飞机设计研究所 一种具有整体油箱的复合材料机翼

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4219980A (en) 1977-08-26 1980-09-02 Rockwell International Corporation Reinforced composite structure and method of fabrication thereof
US4657615A (en) 1984-08-20 1987-04-14 The Boeing Company Composite leading edge/spar member for an aircraft control surface
US5358583A (en) 1988-10-19 1994-10-25 E. I. Du Pont De Nemours And Company Apparatus and method for shaping fiber reinforced resin matrix materials and product thereof
US5514448A (en) 1992-07-22 1996-05-07 Mitsui Toatsu Chemicals, Inc. Laminated molding
GB9828368D0 (en) 1998-12-22 1999-02-17 British Aerospace Forming reinforcing components
EP1031406A1 (de) 1999-02-22 2000-08-30 British Aerospace Herstellung von Verstärkungsteilen
US6513757B1 (en) * 1999-07-19 2003-02-04 Fuji Jukogyo Kabushiki Kaisha Wing of composite material and method of fabricating the same
JP4425424B2 (ja) 2000-05-01 2010-03-03 本田技研工業株式会社 繊維強化複合材からなるジョグル付き半硬化物品の製造方法、及びそれを用いた予備成形構造体の製造方法

Also Published As

Publication number Publication date
CA2459167C (en) 2008-11-18
NO322021B1 (no) 2006-08-07
ES2258645T3 (es) 2006-09-01
EP1425215B1 (de) 2006-05-03
DE60211185D1 (de) 2006-06-08
US20040244334A1 (en) 2004-12-09
NO20041174L (no) 2004-03-19
GB0122050D0 (en) 2001-10-31
DE60211185T2 (de) 2006-09-07
US7380753B2 (en) 2008-06-03
EP1425215A1 (de) 2004-06-09
CA2459167A1 (en) 2003-03-20
WO2003022677A1 (en) 2003-03-20

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