AU2001233835A1 - A method of reinforcing a laminated member such as a skin for an aircraft - Google Patents

A method of reinforcing a laminated member such as a skin for an aircraft

Info

Publication number
AU2001233835A1
AU2001233835A1 AU2001233835A AU3383501A AU2001233835A1 AU 2001233835 A1 AU2001233835 A1 AU 2001233835A1 AU 2001233835 A AU2001233835 A AU 2001233835A AU 3383501 A AU3383501 A AU 3383501A AU 2001233835 A1 AU2001233835 A1 AU 2001233835A1
Authority
AU
Australia
Prior art keywords
skin
reinforcing
aircraft
laminated
laminated member
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.)
Abandoned
Application number
AU2001233835A
Other languages
English (en)
Inventor
Andrew Paul Godbehere
Stephen Williams
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
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
Publication of AU2001233835A1 publication Critical patent/AU2001233835A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
    • B32B3/08—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions characterised by added members at particular parts
    • 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
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • 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
    • B64C1/12—Construction or attachment of skin panels
    • 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
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24752—Laterally noncoextensive components

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
AU2001233835A 2000-02-11 2001-02-06 A method of reinforcing a laminated member such as a skin for an aircraft Abandoned AU2001233835A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB0003029 2000-02-11
GBGB0003029.6A GB0003029D0 (en) 2000-02-11 2000-02-11 A method of reinforcing a laminated member such as a skin for an aircraft
PCT/GB2001/000469 WO2001058680A1 (fr) 2000-02-11 2001-02-06 Procede de renforcement d'un produit stratifie, notamment un revetement d'avion

Publications (1)

Publication Number Publication Date
AU2001233835A1 true AU2001233835A1 (en) 2001-08-20

Family

ID=9885293

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001233835A Abandoned AU2001233835A1 (en) 2000-02-11 2001-02-06 A method of reinforcing a laminated member such as a skin for an aircraft

Country Status (8)

Country Link
US (1) US7780808B2 (fr)
EP (1) EP1263572B1 (fr)
AT (1) ATE249921T1 (fr)
AU (1) AU2001233835A1 (fr)
DE (1) DE60100802T2 (fr)
ES (1) ES2202274T3 (fr)
GB (1) GB0003029D0 (fr)
WO (1) WO2001058680A1 (fr)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ATE293755T1 (de) 2001-07-19 2005-05-15 Neg Micon As Windturbinenblatt
GB0117804D0 (en) 2001-07-21 2001-09-12 Bae Systems Plc Aircraft structural components
GB0329373D0 (en) 2003-12-18 2004-01-21 Airbus Uk Ltd Method of joining structural elements in an aircraft
EP1544099B1 (fr) * 2003-12-18 2009-01-07 Airbus UK Limited Méthode pour joindre des éléments de structure d'avion
ES2347507B1 (es) * 2007-12-27 2011-08-17 Airbus Operations, S.L. Boca de acceso de aeronave optimizada.
FR2933067B1 (fr) * 2008-06-26 2010-10-08 Airbus France Panneau de fuselage d'aeronef renforce et procede de fabrication.
CA2768957C (fr) * 2009-10-08 2014-07-29 Mitsubishi Heavy Industries, Ltd. Structure en materiau composite, ainsi qu'aile et fuselage d'aeronef comportant cette structure
GB201000878D0 (en) 2010-01-20 2010-03-10 Airbus Operations Ltd Sandwich panel
CN101891015B (zh) * 2010-07-20 2013-04-10 中国航空工业集团公司西安飞机设计研究所 一种蒙皮板减重方法
US9108387B2 (en) * 2011-06-30 2015-08-18 The Boeing Company Electrically conductive structure
FR2977186B1 (fr) * 2011-07-01 2014-08-22 Daher Aerospace Procede de renforcement local d'un panneau composite a renfort fibreux et panneau obtenu par un tel procede
ES2401520B1 (es) * 2011-07-28 2014-06-10 Airbus Operations S.L. procedimiento de fabricación de una pieza de material compuesto de un compartimento cerrado con una disposición de acceso integrada
GB201115080D0 (en) 2011-09-01 2011-10-19 Airbus Operations Ltd An aircraft structure
DE102011083162A1 (de) * 2011-09-21 2013-03-21 Bayerische Motoren Werke Aktiengesellschaft Mehrlagiges Faserverbundbauteil und Verfahren zum Herstellen desselben
EP3021695B1 (fr) * 2013-07-19 2018-06-27 Philip Morris Products S.a.s. Emballage de cigarettes hydrophobe
EP2842865B1 (fr) * 2013-08-28 2019-12-18 Airbus Operations GmbH Panneau de fenêtre pour une cellule d'aéronef et son procédé de production
US10479517B2 (en) * 2016-12-05 2019-11-19 The Boeing Company Composite fan cowl with a core having tailored thickness
JP6770987B2 (ja) * 2018-03-12 2020-10-21 株式会社Ｓｕｂａｒｕ 複合材構造体、航空機及び雷電流の誘導方法
US11446884B2 (en) * 2018-10-29 2022-09-20 Airbus Operations Gmbh Process for producing a component which is two-dimensional in regions from a fibre composite material
GB2604126A (en) * 2021-02-24 2022-08-31 Airbus Operations Ltd Reinforced holes

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2154286A (en) 1984-02-13 1985-09-04 Gen Electric Hollow laminated airfoil
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
FR2771330B1 (fr) * 1997-11-26 2004-02-27 Aerospatiale Procede de fabrication d'un panneau composite monolithique articule avec des moyens raidisseurs integres, panneau articule obtenu et capot articule dans un aeronef
GB9826681D0 (en) * 1998-12-04 1999-01-27 British Aerospace Composite laminates

Also Published As

Publication number Publication date
US7780808B2 (en) 2010-08-24
DE60100802D1 (de) 2003-10-23
GB0003029D0 (en) 2000-03-29
ATE249921T1 (de) 2003-10-15
EP1263572B1 (fr) 2003-09-17
WO2001058680A1 (fr) 2001-08-16
US20030021958A1 (en) 2003-01-30
ES2202274T3 (es) 2004-04-01
EP1263572A1 (fr) 2002-12-11
DE60100802T2 (de) 2004-04-08

Similar Documents

Publication Publication Date Title
AU2001233835A1 (en) A method of reinforcing a laminated member such as a skin for an aircraft
GB9504372D0 (en) A composite laminate
AU620931B2 (en) Improved interleaf layer in fiber reinforced resin laminate composites
WO2007001447A3 (fr) Mandrin souple pour raidisseur lisse composite a profil prononce
EP0783960A3 (fr) Laminés hybrides titane-polymère
WO2006118691A3 (fr) Structures composites constituees de lisses et de revetements et procedes de formation de ces dernieres
CA2395888A1 (fr) Ames et panneaux composites renforces par des fibres
WO2005094443A3 (fr) Produit fibreux isolant renforce et procede de renfort de celui-ci
DE69314175T2 (de) Gespleisste laminate für flugzeugrumpf
WO1998010919A3 (fr) Stratifies
CA2355366A1 (fr) Formage d'elements renforces
IT8048611A0 (it) Procedimento di fabbricazione distrutture composite in particolare laminati rinforzati con fibre
FI973659A0 (fi) Vaordande schaberbett och foerfarande foer att framstaella detta
DK1206380T3 (da) Sejllegeme og fremgangsmåde til til fremstilling
ATE403597T1 (de) Blitzschlagschutz und erdung einer verbundflugzeugplatte
AU2639397A (en) Multi-layer reinforced and stabilized cable construction
AU2003274774A1 (en) A fibre reinforced composite component and method to produce such component
DE59803068D1 (de) Feuerfester plattenverbund, ein verfahren zu dessen herstellung sowie dessen verwendung
DE69715787D1 (de) Herstellung einer Verbundlaminat-Schutzvorrichtung für die Streben von Flugzeugfahrgestellen
MY111070A (en) A method of preparing a corrugated board as well as a corrugated board.
DE69609991D1 (de) Linoleum bodenbelag
PL1921414T3 (pl) Pancerz
DE3773443D1 (de) Verkleidungselement.
PL315656A1 (en) Insulating mat incorporating a layer of mineral fibres
WO1999015281A8 (fr) Transducteur magnetostrictif multicouches et matiere composite magnetostrictive utile pour celui-ci