DE69929089D1 - Verbundwerkstoffe - Google Patents

Verbundwerkstoffe

Info

Publication number
DE69929089D1
DE69929089D1 DE69929089T DE69929089T DE69929089D1 DE 69929089 D1 DE69929089 D1 DE 69929089D1 DE 69929089 T DE69929089 T DE 69929089T DE 69929089 T DE69929089 T DE 69929089T DE 69929089 D1 DE69929089 D1 DE 69929089D1
Authority
DE
Germany
Prior art keywords
composites
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 - Lifetime
Application number
DE69929089T
Other languages
English (en)
Other versions
DE69929089T2 (de
Inventor
Michael John Healey
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 Ltd
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 DE69929089D1 publication Critical patent/DE69929089D1/de
Publication of DE69929089T2 publication Critical patent/DE69929089T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/16—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer formed of particles, e.g. chips, powder or granules
    • 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
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • 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
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/07—Parts immersed or impregnated in a matrix
    • 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
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/08—Reinforcements
    • 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
    • B32B2605/00—Vehicles
    • B32B2605/18—Aircraft
    • 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
    • Y10T156/1089—Methods of surface bonding and/or assembly therefor of discrete laminae to single face of additional lamina
    • Y10T156/1092—All laminae planar and face to face
    • 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
    • Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/30—Woven fabric [i.e., woven strand or strip material]
    • Y10T442/3179—Woven fabric is characterized by a particular or differential weave other than fabric in which the strand denier or warp/weft pick count is specified
    • Y10T442/3187—Triaxially woven fabric
DE69929089T 1998-12-04 1999-11-25 Verbundwerkstoffe Expired - Lifetime DE69929089T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB9826681 1998-12-04
GBGB9826681.0A GB9826681D0 (en) 1998-12-04 1998-12-04 Composite laminates
PCT/GB1999/003909 WO2000034031A1 (en) 1998-12-04 1999-11-25 Composite laminates

Publications (2)

Publication Number Publication Date
DE69929089D1 true DE69929089D1 (de) 2006-01-26
DE69929089T2 DE69929089T2 (de) 2006-07-13

Family

ID=10843646

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69929089T Expired - Lifetime DE69929089T2 (de) 1998-12-04 1999-11-25 Verbundwerkstoffe

Country Status (12)

Country Link
US (1) US6372072B1 (de)
EP (1) EP1154900B1 (de)
JP (1) JP3383646B2 (de)
AU (1) AU762337B2 (de)
BR (1) BR9915901B1 (de)
CA (1) CA2350613A1 (de)
DE (1) DE69929089T2 (de)
ES (1) ES2251239T3 (de)
GB (1) GB9826681D0 (de)
IL (1) IL143460A (de)
NO (1) NO20012761D0 (de)
WO (1) WO2000034031A1 (de)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2359097A (en) * 2000-02-08 2001-08-15 Milliken Europ Nv Hose and pipe reinforcement
GB0003029D0 (en) * 2000-02-11 2000-03-29 British Aerospace A method of reinforcing a laminated member such as a skin for an aircraft
US7432448B2 (en) * 2001-02-15 2008-10-07 Integral Technologies, Inc Low cost aircraft structures and avionics manufactured from conductive loaded resin-based materials
EP1262438B2 (de) † 2001-06-01 2014-04-16 ThyssenKrupp Elevator AG Fahrkorb für einen Aufzug
WO2004098885A2 (en) * 2003-04-30 2004-11-18 Saint-Gobain Performance Plastics Corporation Flexible composites and applications including the flexible composites
US7740932B2 (en) * 2005-03-31 2010-06-22 The Boeing Company Hybrid fiberglass composite structures and methods of forming the same
US20060222837A1 (en) * 2005-03-31 2006-10-05 The Boeing Company Multi-axial laminate composite structures and methods of forming the same
US7721495B2 (en) * 2005-03-31 2010-05-25 The Boeing Company Composite structural members and methods for forming the same
US8444087B2 (en) * 2005-04-28 2013-05-21 The Boeing Company Composite skin and stringer structure and method for forming the same
US20060237588A1 (en) * 2005-03-31 2006-10-26 The Boeing Company Composite structural member having an undulating web and method for forming the same
US8720825B2 (en) * 2005-03-31 2014-05-13 The Boeing Company Composite stiffeners for aerospace vehicles
PL2021243T3 (pl) * 2006-04-27 2019-04-30 Flexsys Inc Wzorzec podatnej struktury do zmiennych konturów powierzchniowych
US7861969B2 (en) * 2007-05-24 2011-01-04 The Boeing Company Shaped composite stringers and methods of making
ES2383863B1 (es) * 2009-05-06 2013-06-10 Airbus Operations, S.L. Pieza de material compuesto con gran cambio de espesor.
ES2385004B1 (es) * 2009-12-31 2013-05-27 Airbus Operations, S.L. Pieza de material compuesto con larguerillo en rampa.
FR2960179A1 (fr) * 2010-05-20 2011-11-25 Airbus Operations Sas Piece structurale composite a rigidite evolutive
GB201103125D0 (en) * 2011-02-23 2011-04-06 Airbus Uk Ltd Composite structure
GB201103122D0 (en) * 2011-02-23 2011-04-06 Airbus Uk Ltd Composite structure
GB201207525D0 (en) * 2012-04-30 2012-06-13 Airbus Operations Ltd Morphing aerofoil
US20140003923A1 (en) * 2012-07-02 2014-01-02 Peter Finnigan Functionally graded composite fan containment case
US9878773B2 (en) 2012-12-03 2018-01-30 The Boeing Company Split resistant composite laminate
US11072565B2 (en) 2015-02-27 2021-07-27 General Electric Company Ceramic matrix composite structures with controlled microstructures fabricated using chemical vapor infiltration (CVI)
JP6980454B2 (ja) * 2017-08-17 2021-12-15 三菱重工業株式会社 複合材の設計方法、複合材の評価方法及び複合材
CN109583040B (zh) * 2018-11-07 2022-11-18 中国航空工业集团公司西安飞机设计研究所 一种考虑复合材料结构参数连续性的优化方法
US10913215B2 (en) * 2019-05-09 2021-02-09 The Boeing Company Composite structure having a variable gage and methods for forming a composite structure having a variable gage
US10919256B2 (en) * 2019-05-09 2021-02-16 The Boeing Company Composite structure having a variable gage and methods for forming a composite structure having a variable gage
US10919260B2 (en) * 2019-05-09 2021-02-16 The Boeing Company Composite structure having a variable gage and methods for forming a composite structure having a variable gage
CN113044203B (zh) * 2021-04-21 2023-11-21 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种用于飞机的牺牲层及铺贴方法

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4438173A (en) * 1983-07-21 1984-03-20 Barber-Colman Company Triaxial fabric
US4606961A (en) * 1984-10-09 1986-08-19 The Boeing Company Discretely stiffened composite panel
US4571355A (en) * 1984-11-28 1986-02-18 The Boeing Company Fiber reinforced resin composites formed of basic ply blankets
AT392525B (de) * 1985-11-14 1991-04-25 Kofler Walter Dr Blattfeder aus faser-kunststoff-verbundwerkstoff
KR890701976A (ko) * 1987-08-03 1989-12-22 로이 에이취.멧신길 충격 저항성 헬멧
GB8822520D0 (en) * 1988-09-26 1988-11-02 Tech Textiles Ltd Process for continuously forming reinforced plastics articles
EP0361376A3 (de) 1988-09-30 1991-09-11 The Boeing Company Automatisierte Schneid- und Verteilanlage für Verbundwerkstoff und Verfahren
GB8910068D0 (en) * 1989-05-03 1989-09-13 Westland Helicopters Method for producing a component from fibre-reinforced plastic materials
US5702993A (en) * 1994-11-04 1997-12-30 Nippon Steel Corporation Triaxial fabric composed of carbon fiber strands and method for production thereof
US5688577A (en) * 1995-07-27 1997-11-18 R. K. Carbon Fibers, Inc. Multi-directional friction materials
US5718212A (en) * 1995-10-02 1998-02-17 Indian Industries Composite bow limb

Also Published As

Publication number Publication date
EP1154900B1 (de) 2005-12-21
US6372072B1 (en) 2002-04-16
EP1154900A1 (de) 2001-11-21
AU1284300A (en) 2000-06-26
BR9915901B1 (pt) 2009-01-13
JP3383646B2 (ja) 2003-03-04
JP2002531299A (ja) 2002-09-24
DE69929089T2 (de) 2006-07-13
ES2251239T3 (es) 2006-04-16
IL143460A (en) 2004-09-27
GB9826681D0 (en) 1999-01-27
IL143460A0 (en) 2002-04-21
CA2350613A1 (en) 2000-06-15
WO2000034031A1 (en) 2000-06-15
NO20012761L (no) 2001-06-05
AU762337B2 (en) 2003-06-26
NO20012761D0 (no) 2001-06-05
BR9915901A (pt) 2001-08-21

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Date Code Title Description
8327 Change in the person/name/address of the patent owner

Owner name: AIRBUS UK LTD., BRISTOL, GB

8364 No opposition during term of opposition
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