DE447349T1 - Formen von verbundstrukturen. - Google Patents

Formen von verbundstrukturen.

Info

Publication number
DE447349T1
DE447349T1 DE199191630016T DE91630016T DE447349T1 DE 447349 T1 DE447349 T1 DE 447349T1 DE 199191630016 T DE199191630016 T DE 199191630016T DE 91630016 T DE91630016 T DE 91630016T DE 447349 T1 DE447349 T1 DE 447349T1
Authority
DE
Germany
Prior art keywords
composite structures
shaping composite
shaping
structures
composite
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.)
Pending
Application number
DE199191630016T
Other languages
English (en)
Inventor
Richard Joseph Meriden Connecticut 06450 Us Simkulak
Robert Louis St. Charles Missouri 63303 Us Folts
Terry Martin New Haven Connecticut 06513 Us Boustead
George Nicholas Trumbull Connecticut 06611 Us Sepe
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE447349T1 publication Critical patent/DE447349T1/de
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0025Producing blades or the like, e.g. blades for turbines, propellers, or wings
    • B29D99/0028Producing blades or the like, e.g. blades for turbines, propellers, or wings hollow blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32Component parts, details or accessories; Auxiliary operations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B29C70/446Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/541Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B30PRESSES
    • B30BPRESSES IN GENERAL
    • B30B5/00Presses characterised by the use of pressing means other than those mentioned in the preceding groups
    • B30B5/02Presses characterised by the use of pressing means other than those mentioned in the preceding groups wherein the pressing means is in the form of a flexible element, e.g. diaphragm, urged by fluid pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/10Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
    • B29C43/12Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies using bags surrounding the moulding material or using membranes contacting the moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2024/00Articles with hollow walls
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/30Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076Aircrafts
    • B29L2031/3085Wings
DE199191630016T 1990-03-09 1991-03-07 Formen von verbundstrukturen. Pending DE447349T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/491,408 US5087187A (en) 1990-03-09 1990-03-09 Apparatus for molding hollow composite articles having internal reinforcement structures

Publications (1)

Publication Number Publication Date
DE447349T1 true DE447349T1 (de) 1992-02-27

Family

ID=23952095

Family Applications (1)

Application Number Title Priority Date Filing Date
DE199191630016T Pending DE447349T1 (de) 1990-03-09 1991-03-07 Formen von verbundstrukturen.

Country Status (5)

Country Link
US (1) US5087187A (de)
EP (1) EP0447349A1 (de)
JP (1) JPH04219215A (de)
CA (1) CA2035413A1 (de)
DE (1) DE447349T1 (de)

Families Citing this family (49)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9211263D0 (en) * 1992-05-28 1992-07-15 British Aerospace Manufacture of articles from composite material
US5520532A (en) * 1994-08-01 1996-05-28 United Technologies Corporation Molding assembly for forming airfoil structures
WO1996006776A1 (en) * 1994-08-31 1996-03-07 United Technologies Corporation Fiber reinforced composite spar for a rotary wing aircraft and method of manufacture thereof
US5939007A (en) * 1994-08-31 1999-08-17 Sikorsky Aircraft Corporation Method for manufacture of a fiber reinforced composite spar for rotary wing aircraft
US5547629A (en) * 1994-09-27 1996-08-20 Competition Composites, Inc. Method for manufacturing a one-piece molded composite airfoil
FR2760681B1 (fr) * 1997-03-12 1999-05-14 Alternatives En Procede de fabrication d'une piece de grandes dimensions en materiau composite et pale d'helice, en particulier d'eolienne, fabriquee selon ce procede
FR2774627B1 (fr) * 1998-02-10 2000-03-10 Inst Francais Du Petrole Procede de moulage sans presse et dispositif associe
US6513757B1 (en) * 1999-07-19 2003-02-04 Fuji Jukogyo Kabushiki Kaisha Wing of composite material and method of fabricating the same
US6591197B2 (en) 2000-05-02 2003-07-08 Sikorsky Aircraft Corporation Fiber orientation verification for a composite article
US6593524B1 (en) * 2000-06-15 2003-07-15 Thomas Toedtman Device and method for providing EMI/RFI shielding
US7165945B2 (en) * 2003-08-22 2007-01-23 Sikorsky Aircraft Corporation Braided spar for a rotor blade and method of manufacture thereof
FR2863542B1 (fr) * 2003-12-12 2007-10-26 Jean Margail Procede de fabrication de structures composites a base de tissus pre-impregnes utilisant des sacs gonflables, applicable notamment a la construction de bateaux
US20050186081A1 (en) * 2004-02-24 2005-08-25 Mohamed Mansour H. Wind blade spar cap and method of making
FR2882681B1 (fr) * 2005-03-03 2009-11-20 Coriolis Composites Tete d'application de fibres et machine correspondante
US7824171B2 (en) * 2005-10-31 2010-11-02 The Boeing Company Corner-consolidating inflatable apparatus and method for manufacturing composite structures
GB0616121D0 (en) * 2006-08-14 2006-09-20 Airbus Uk Ltd Moulding tool and method of manufacturing a part
FR2912680B1 (fr) * 2007-02-21 2009-04-24 Coriolis Composites Sa Procede et dispositif de fabrication de pieces en materiau composite, en particulier de troncons de fuselage d'avion
CN101646866B (zh) * 2007-02-27 2012-07-25 维斯塔斯风力系统有限公司 风轮机叶片的加强结构、风轮机叶片及其组装方法和应用
FR2913365B1 (fr) * 2007-03-06 2013-07-26 Coriolis Composites Attn Olivier Bouroullec Tete d'application de fibres avec systemes de coupe de fibres particuliers
FR2913366B1 (fr) * 2007-03-06 2009-05-01 Coriolis Composites Sa Tete d'application de fibres avec systemes de coupe et de blocage de fibres particuliers
US8066504B2 (en) 2008-01-25 2011-11-29 Hexcel Corporation Helicopter blade mandrel with roller assembly
DE102008054293B4 (de) * 2008-11-03 2010-09-23 Mt Aerospace Ag Druckbehälter für den Hochtemperatureinsatz und ein Verfahren zu deren Herstellung
FR2943943A1 (fr) * 2009-04-02 2010-10-08 Coriolis Composites Procede et machine pour l'application d'une bande de fibres sur des surfaces convexes et/ou avec aretes
FR2948058B1 (fr) * 2009-07-17 2011-07-22 Coriolis Composites Machine d'application de fibres comprenant un rouleau de compactage souple avec systeme de regulation thermique
FR2948059B1 (fr) * 2009-07-17 2011-08-05 Coriolis Composites Machine d'application de fibres avec rouleau de compactage transparent au rayonnement du systeme de chauffage
US9505491B2 (en) * 2010-08-19 2016-11-29 Sikorsky Aircraft Corporation Helicopter composite blade spar and method
IT1401996B1 (it) * 2010-09-30 2013-08-28 Wilic Sarl Metodo per realizzare un longherone tubolare di una pala di una turbina eolica
US9017510B2 (en) 2011-12-13 2015-04-28 The Boeing Company Method and apparatus for fabricating large scale integrated airfoils
DE102012000564B4 (de) * 2012-01-16 2015-02-19 Airbus Operations Gmbh Urformwerkzeug und Verfahren für die Fertigung eines aus faserverstärktem Kunststoff bestehenden aerodynamisch geformten Luftfahrzeugbauteils
ITTO20120504A1 (it) * 2012-06-11 2013-12-12 Alenia Aermacchi Spa Metodo di realizzazione di una struttura aeronautica a profilo chiuso provvista di sensori di deformazione
US9145203B2 (en) * 2012-10-31 2015-09-29 The Boeing Company Natural laminar flow wingtip
US9889613B2 (en) 2012-11-01 2018-02-13 Israel Aerospace Industries Ltd. Manufacture of integrated structures formed of composite materials
US9527575B2 (en) * 2012-11-26 2016-12-27 The Boeing Company Multi-box wing spar and skin
US8983171B2 (en) 2012-12-26 2015-03-17 Israel Aerospace Industries Ltd. System and method for inspecting structures formed of composite materials during the fabrication thereof
US9623641B1 (en) * 2013-09-24 2017-04-18 The Boeing Company Method and apparatus for reinforcing a bladder
US10081140B2 (en) * 2014-10-29 2018-09-25 The Boeing Company Apparatus for and method of compaction of a prepreg
FR3034338B1 (fr) 2015-04-01 2017-04-21 Coriolis Composites Tete d'application de fibres avec rouleau d'application particulier
US10035300B2 (en) * 2015-06-23 2018-07-31 The Boeing Company System and method for manufacturing a stiffened composite structure
FR3043010B1 (fr) 2015-10-28 2017-10-27 Coriolis Composites Machine d'application de fibres avec systemes de coupe particuliers
FR3048373B1 (fr) 2016-03-07 2018-05-18 Coriolis Group Procede de realisation de preformes avec application d'un liant sur fibre seche et machine correspondante
CN105965736B (zh) * 2016-06-24 2018-02-06 江苏国信复合材料科技股份有限公司 一种自动上料浇注机
FR3056438B1 (fr) 2016-09-27 2019-11-01 Coriolis Group Procede de realisation de pieces en materiau composite par impregnation d'une preforme particuliere.
RU2636994C1 (ru) * 2016-11-16 2017-11-29 Виктор Степанович Ермоленко Способ формования из композитного материала пустотелых аэродинамических поверхностей - 2
RU2674972C2 (ru) * 2016-11-16 2018-12-13 Общество с ограниченной ответственностью "Фирма "МВЕН" Способ формования из композитного материала пустотелых аэродинамических поверхностей - 1
CN106945215A (zh) * 2017-04-27 2017-07-14 余姚贝思特模具五金有限公司 一种聚四氟乙烯压机
CN109109340B (zh) * 2018-08-07 2020-12-01 株洲时代新材料科技股份有限公司 一种复合材料轴及其制备方法和应用
CN110789129A (zh) * 2019-06-28 2020-02-14 东莞科威医疗器械有限公司 一种增强型医用插管及其制作方法
US11046420B2 (en) * 2019-10-23 2021-06-29 The Boeing Company Trailing edge flap having a waffle grid interior structure
CN113147067B (zh) * 2021-04-12 2022-03-18 西南石油大学 一种质子交换膜燃料电池金属双极板液压成形机

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2945655A (en) * 1956-01-20 1960-07-19 Boeing Co Double skin airfoil structure
US3764431A (en) * 1970-10-22 1973-10-09 Delog Detag Flachglas Ag Method and apparatus for making channelled sheets from deformable materials
FR2234130B1 (de) * 1973-05-14 1976-04-30 Kamov Nikolai
US3962506A (en) * 1974-04-29 1976-06-08 Fiber Science, Inc. Multi-chambered cellular structure and method for manufacture
US4169749A (en) * 1977-09-21 1979-10-02 The United States Of America As Represented By The Secretary Of The Navy Method of making a hollow airfoil
US4292101A (en) * 1979-03-05 1981-09-29 Reichert James B Method of fabricating composite members
US4662587A (en) * 1981-09-30 1987-05-05 The Boeing Company Composite for aircraft wing and method of making
US4565595A (en) * 1981-09-30 1986-01-21 The Boeing Company Method of making composite aircraft wing
EP0146545B1 (de) * 1983-06-06 1987-11-19 The Boeing Company Verfahren zur herstellung von flugzeugflügeln
FR2555501A1 (fr) * 1983-11-28 1985-05-31 Septem Sa Procede de fabrication de structures rigides creuses en fibres impregnees de resine, dispositif pour sa mise en oeuvre et structure obtenue
FR2567805B1 (fr) * 1984-07-23 1987-01-23 Aerospatiale Dispositif de fabrication par bobinage filamentaire d'une enveloppe creuse et enveloppe obtenue a l'aide du dispositif
US4853172A (en) * 1987-12-01 1989-08-01 United Technologies Corporation Method of fabricating tubular composite structures

Also Published As

Publication number Publication date
CA2035413A1 (en) 1991-09-10
EP0447349A1 (de) 1991-09-18
US5087187A (en) 1992-02-11
JPH04219215A (ja) 1992-08-10

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