DE602005022305D1 - Fensterrahmen für luftfahrzeuge - Google Patents

Fensterrahmen für luftfahrzeuge

Info

Publication number
DE602005022305D1
DE602005022305D1 DE602005022305T DE602005022305T DE602005022305D1 DE 602005022305 D1 DE602005022305 D1 DE 602005022305D1 DE 602005022305 T DE602005022305 T DE 602005022305T DE 602005022305 T DE602005022305 T DE 602005022305T DE 602005022305 D1 DE602005022305 D1 DE 602005022305D1
Authority
DE
Germany
Prior art keywords
window frame
aircraft
flange
flanges
vertical flange
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.)
Active
Application number
DE602005022305T
Other languages
English (en)
Inventor
Jens Bold
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 GmbH
Original Assignee
Airbus Operations GmbH
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 GmbH filed Critical Airbus Operations GmbH
Publication of DE602005022305D1 publication Critical patent/DE602005022305D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • 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
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1476—Canopies; Windscreens or similar transparent elements
    • B64C1/1492—Structure and mounting of the transparent elements in the window or windscreen
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/001—Profiled members, e.g. beams, sections
    • B29L2031/003—Profiled members, e.g. beams, sections having a profiled transverse cross-section
    • B29L2031/005—Profiled members, e.g. beams, sections having a profiled transverse cross-section for making window frames
    • 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)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)
  • Injection Moulding Of Plastics Or The Like (AREA)
  • Wing Frames And Configurations (AREA)
  • Window Of Vehicle (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Liquid Crystal Substances (AREA)
DE602005022305T 2004-05-24 2005-05-24 Fensterrahmen für luftfahrzeuge Active DE602005022305D1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102004025377A DE102004025377B4 (de) 2004-05-24 2004-05-24 Fensterrahmen für Flugzeuge
US60011204P 2004-08-09 2004-08-09
PCT/EP2005/005602 WO2005115836A1 (en) 2004-05-24 2005-05-24 Window frame for aircraft

Publications (1)

Publication Number Publication Date
DE602005022305D1 true DE602005022305D1 (de) 2010-08-26

Family

ID=35433003

Family Applications (2)

Application Number Title Priority Date Filing Date
DE102004025377A Expired - Lifetime DE102004025377B4 (de) 2004-05-24 2004-05-24 Fensterrahmen für Flugzeuge
DE602005022305T Active DE602005022305D1 (de) 2004-05-24 2005-05-24 Fensterrahmen für luftfahrzeuge

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE102004025377A Expired - Lifetime DE102004025377B4 (de) 2004-05-24 2004-05-24 Fensterrahmen für Flugzeuge

Country Status (10)

Country Link
US (1) US7988093B2 (de)
EP (1) EP1748925B1 (de)
JP (1) JP2008500229A (de)
CN (1) CN100471757C (de)
AT (1) ATE473915T1 (de)
BR (1) BRPI0510635A (de)
CA (1) CA2563441A1 (de)
DE (2) DE102004025377B4 (de)
RU (1) RU2369523C2 (de)
WO (1) WO2005115836A1 (de)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080078876A1 (en) * 2006-08-15 2008-04-03 Baggette Phillip D Composite resin window frame constructions for airplanes
US20100096063A1 (en) * 2006-11-13 2010-04-22 Friddell S Douglas Inspectability of composite items
EP2117925B1 (de) 2007-01-12 2017-07-19 THE NORDAM GROUP, Inc. Flugzeugfenster-erosionsschutz
US8449709B2 (en) 2007-05-25 2013-05-28 The Boeing Company Method of fabricating fiber reinforced composite structure having stepped surface
FR2928343B1 (fr) 2008-03-10 2010-08-20 Airbus France Panneau du hublot et procede de fabrication d'un tel panneau aeronef comprenant un panneau de hublot
JP6125427B2 (ja) 2010-11-16 2017-05-10 ザ・ノーダム・グループ・インコーポレーテッドＴｈｅ Ｎｏｒｄａｍ Ｇｒｏｕｐ，Ｉｎｃ． ハイブリッド構成のフレーム共成形製造
RU2500535C1 (ru) * 2012-06-07 2013-12-10 Открытое акционерное общество "Национальный институт авиационных технологий" (ОАО НИАТ) Оснастка для формования рамы иллюминатора
CN103121264A (zh) * 2013-03-13 2013-05-29 健大电业制品（昆山）有限公司 一种埋入式二次注塑模具
EP2842865B1 (de) * 2013-08-28 2019-12-18 Airbus Operations GmbH Fensterscheibe für ein flugwerk und verfahren zur herstellung davon
CN104070688B (zh) * 2014-06-09 2016-08-24 中航复合材料有限责任公司 一种用于模压技术成型的飞机复合材料舷窗框模具
CN105366073B (zh) * 2015-11-24 2017-04-12 江苏恒神股份有限公司 纤维铺缝窗框预制体的制造方法
CN109533272A (zh) * 2018-11-23 2019-03-29 江苏恒神股份有限公司 一种碳纤维复合材料飞机窗框及其制造方法
US11952099B2 (en) 2021-07-07 2024-04-09 The Boeing Company Aircraft window assemblies and related methods

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0089337B1 (de) * 1981-09-30 1987-08-12 The Boeing Company Zusammengestelltes fensterband, sowie herstellungsverfahren
FR2632604B1 (fr) 1988-06-08 1991-07-12 Aerospatiale Cadre en materiau composite notamment pour fuselage d'aeronef, et son procede de fabrication
US5945356A (en) * 1996-10-10 1999-08-31 Pott; Richard Reinforcing web and production thereof
FR2761380B1 (fr) * 1997-03-28 1999-07-02 Europ Propulsion Procede et machine pour la realisation de nappes fibreuses multiaxiales
GB0113916D0 (en) * 2001-06-07 2001-08-01 Bae Systems Plc Adding glass to composite bonding surfaces
DE10251579B4 (de) * 2002-03-08 2012-02-02 Airbus Operations Gmbh Verfahren zur Herstellung einer umlaufenden dreidimensionalen Faserverstärkungsstruktur
EP1342553B1 (de) * 2002-03-08 2016-05-18 Airbus Operations GmbH Verfahren zum Herstellen eines Fensterrahmens für Flugzeuge aus faserverstärktem Kunststoff und Vorrichtung zur Durchführung des Verfahrens
DE10251580B4 (de) * 2002-03-08 2013-01-10 Airbus Operations Gmbh Verfahren zum Herstellen eines Bauelementes aus faserverstärktem Kunststoff
GB0213161D0 (en) * 2002-06-07 2002-07-17 Short Brothers Plc A fibre reinforced composite component
US7138167B2 (en) * 2002-08-12 2006-11-21 Shikibo Ltd. Preform precursor for fiber-reinforced composite material, preform for fiber-reinforced composite material, and method of manufacturing the precursor and the preform
JP4309748B2 (ja) * 2003-11-25 2009-08-05 シキボウ株式会社 航空機に用いられるｆｒｐ製窓枠用のドライプリフォーム

Also Published As

Publication number Publication date
EP1748925B1 (de) 2010-07-14
RU2369523C2 (ru) 2009-10-10
BRPI0510635A (pt) 2007-11-13
DE102004025377A1 (de) 2005-12-22
JP2008500229A (ja) 2008-01-10
US7988093B2 (en) 2011-08-02
ATE473915T1 (de) 2010-07-15
CA2563441A1 (en) 2005-12-08
RU2006143856A (ru) 2008-06-27
EP1748925A1 (de) 2007-02-07
US20080078878A1 (en) 2008-04-03
CN1956884A (zh) 2007-05-02
WO2005115836B1 (en) 2006-02-02
WO2005115836A1 (en) 2005-12-08
CN100471757C (zh) 2009-03-25
DE102004025377B4 (de) 2013-02-14

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