BRPI0713560A2 - método para fabricar um componente de fibra compósita utilizando um núcleo de moldagem dobrável, e o dito núcleo de moldagem - Google Patents

método para fabricar um componente de fibra compósita utilizando um núcleo de moldagem dobrável, e o dito núcleo de moldagem Download PDF

Info

Publication number
BRPI0713560A2
BRPI0713560A2 BRPI0713560-2A BRPI0713560A BRPI0713560A2 BR PI0713560 A2 BRPI0713560 A2 BR PI0713560A2 BR PI0713560 A BRPI0713560 A BR PI0713560A BR PI0713560 A2 BRPI0713560 A2 BR PI0713560A2
Authority
BR
Brazil
Prior art keywords
molding core
composite fiber
fiber component
segments
constructed
Prior art date
Application number
BRPI0713560-2A
Other languages
English (en)
Inventor
Jacob Torben
Original Assignee
Airbus Deutschland 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 Deutschland Gmbh filed Critical Airbus Deutschland Gmbh
Publication of BRPI0713560A2 publication Critical patent/BRPI0713560A2/pt

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
    • B29C70/30—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
    • 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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
    • B29C33/46—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles using fluid pressure
    • 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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
    • B29C33/48—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling
    • B29C33/485—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling cores or mandrels
    • 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
    • B29C70/44—Shaping 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
    • B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

MéTODO PARA FABRICAR UM COMPONENTE DE FIBRA COMPóSITA UTILIZANDO UM NúCLEO DE MOLDAGEM DOBRáVEL, E O DITO NúCLEO DE MOLDAGEM. A presente invenção refere-se a um método para fabricar um componente de fibra compósita (1), o método compreendendo as seguintes etapas de método: formar um núcleo de moldagem (4) que compreende um perfil oco (15) feito de segmentos (16a...d) de modo a estabelecer uma geometria externa do núcleo de moldagem (4), em que os segmentos (16a...d) do núcleo de moldagem (4), cada um, estendem-se na direção do eixo geométrico longitudinal do núcleo de moldagem (4) e estão, cada um, construídos de modo a serem articuláveis ao redor de um eixo geométrico que corre na direção longitudinal do núcleo de moldagem (4), entre uma posição dobrada (A) e uma posição desdobrada (6) do perfil oco (15) do núcleo de moldagem (4), em que os segmentos (16a...d) são construídos de modo a serem acoplados uns nos outros através de conexões (1 8a. . .d, 1 9a. . .c) em uma peça de modo a formar o perfil oco (15); pelo menos um produto semi-acabado de fibra (3) é posicionado pelo menos em certas seções sobre o núcleo de moldagem (4) construído de modo a formar pelo menos uma seção moldada (14) do componente de fibra compósita (1) a ser fabricado; e calor e/ou pressão é aplicada na pelo menos uma seção moldada (14) de modo a fabricar o componente de fibra compósita (1).
BRPI0713560-2A 2006-07-06 2007-07-05 método para fabricar um componente de fibra compósita utilizando um núcleo de moldagem dobrável, e o dito núcleo de moldagem BRPI0713560A2 (pt)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US81877106P 2006-07-06 2006-07-06
DE102006031335A DE102006031335B4 (de) 2006-07-06 2006-07-06 Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE1020060313356 2006-07-06
US60/818,771 2006-07-06
PCT/EP2007/056855 WO2008003767A1 (en) 2006-07-06 2007-07-05 Method for manufacturing a composite fibre component using a foldable moulding core, and said moulding core

Publications (1)

Publication Number Publication Date
BRPI0713560A2 true BRPI0713560A2 (pt) 2012-03-13

Family

ID=38806035

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0713560-2A BRPI0713560A2 (pt) 2006-07-06 2007-07-05 método para fabricar um componente de fibra compósita utilizando um núcleo de moldagem dobrável, e o dito núcleo de moldagem

Country Status (9)

Country Link
US (1) US8500085B2 (pt)
EP (1) EP2038099A1 (pt)
JP (1) JP5583969B2 (pt)
CN (1) CN101466514B (pt)
BR (1) BRPI0713560A2 (pt)
CA (1) CA2651498A1 (pt)
DE (1) DE102006031335B4 (pt)
RU (1) RU2437762C2 (pt)
WO (1) WO2008003767A1 (pt)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006031326B4 (de) * 2006-07-06 2010-09-23 Airbus Deutschland Gmbh Formkern und Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031325B4 (de) * 2006-07-06 2010-07-01 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031323B4 (de) * 2006-07-06 2010-07-15 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031334A1 (de) * 2006-07-06 2008-01-10 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031336B4 (de) 2006-07-06 2010-08-05 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils in der Luft- und Raumfahrt
DE102006031335B4 (de) 2006-07-06 2011-01-27 Airbus Operations Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102008001498B3 (de) * 2008-04-30 2009-08-27 Airbus Deutschland Gmbh Verfahren und Umformvorrichtung zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102008032834B4 (de) * 2008-07-14 2013-08-08 Airbus Operations Gmbh Omega-Stringer zum Versteifen eines flächigen Bauteils und Verfahren zum Herstellen eines Faserverbundbauteils für Schalensegmente
DE102008049359B4 (de) * 2008-09-29 2015-10-08 Airbus Helicopters Deutschland GmbH Herstellungsverfahren für Hohlbauteile aus Faserverbundwerkstoffen in Schlauchbauweise, Folienschlauch und Herstellungsverfahren für einen Folienschlauch
ES2338084B1 (es) * 2008-10-30 2011-03-14 Airbus Operations, S.L. Metodo de fabricacion de un panel de geometria compleja en material compuesto preimpregnado.
US9296187B2 (en) * 2008-12-10 2016-03-29 The Boeing Company Bagging process and mandrel for fabrication of elongated composite structure
US8293051B2 (en) * 2008-12-10 2012-10-23 The Boeing Company Method for producing composite laminates using a collapsible mandrel
DE102009027049B4 (de) 2009-06-19 2011-09-15 Cotesa Gmbh Verfahren zur Integration hohlraumbildender Strukturen in Faserverbundschalen
DE102009040528A1 (de) 2009-09-08 2011-04-07 Premium Aerotec Gmbh Verfahren zur Herstellung eines zumindest ein Hohlprofil aufweisenden Bauteils und Hohlkörper zur Durchführung dieses Verfahrens
JP5588645B2 (ja) * 2009-09-15 2014-09-10 川崎重工業株式会社 横断面に肉厚部位を有する複合材料構造物製造用治具
US8430984B2 (en) * 2010-05-11 2013-04-30 The Boeing Company Collapsible mandrel employing reinforced fluoroelastomeric bladder
EP2593294A1 (en) 2010-07-13 2013-05-22 Learjet Inc. Composite structure and method of forming same
US8997642B2 (en) * 2011-08-08 2015-04-07 The Boeing Company Method for transporting, placing and compacting composite stiffeners
US9931807B2 (en) 2011-08-08 2018-04-03 The Boeing Company Flexible compactor with reinforcing spine
DE102012207950A1 (de) 2012-05-11 2013-11-14 Airbus Operations Gmbh Verfahren zur Herstellung eines Faserverbundbauteils, Stützkern sowie Faserverbundbauteil
US9097602B2 (en) 2013-01-23 2015-08-04 Lawrence Livermore National Security, Llc Systems and methods for determining strength of cylindrical structures by internal pressure loading
US9120246B2 (en) 2013-03-01 2015-09-01 Bell Helicopter Textron Inc. Pressure tunable expandable mandrel for manufacturing a composite structure
GB201305122D0 (en) * 2013-03-20 2013-05-01 Xeros Ltd New cleaning apparatus and method
US9272767B2 (en) 2013-04-19 2016-03-01 The Boeing Company Compacting uncured composite members on contoured mandrel surfaces
DE102013020872B4 (de) * 2013-12-11 2016-03-03 Audi Ag Verfahren zur Herstellung eines faserverstärkten Kunststoffbauteils mit einer Hohlstruktur
US10293559B2 (en) 2014-03-04 2019-05-21 Bombardier Inc. Method and apparatus for forming a composite laminate stack using a breathable polyethylene vacuum film
FR3018719B1 (fr) * 2014-03-24 2016-04-29 Airbus Operations Sas Procede de consolidation d'elements en materiau composite pour former une piece en materiau composite comprenant une cavite debouchante et noyau utilise pour la mise en oeuvre dudit procede
JP6335712B2 (ja) * 2014-08-05 2018-05-30 株式会社Ｓｕｂａｒｕ 複合材の成形治具及び複合材の成形方法
DE102014012602B4 (de) 2014-08-26 2019-09-19 Audi Ag Verfahren zur Herstellung eines Strukturbauteils mit Versteifung
US10807280B2 (en) * 2015-06-22 2020-10-20 The Boeing Company Method of extracting a tooling mandrel from a composite laminate cavity
US10723085B2 (en) 2015-12-17 2020-07-28 Rohr, Inc. Method of extracting mandrel for hollow-hat panel production
DE102017100621A1 (de) 2017-01-13 2018-07-19 Teufelberger Ges.M.B.H. Formstück
US10744727B2 (en) 2017-03-21 2020-08-18 Textron Innovations Inc. Methods of making a specimen with a predetermined wrinkle defect
US10746640B2 (en) 2017-03-21 2020-08-18 Textron Innovations Inc. Methods of making a tubular specimen with a predetermined wrinkle defect
JP6774571B2 (ja) * 2017-07-25 2020-10-28 株式会社Ｓｕｂａｒｕ 複合材成形治具及び複合材成形方法
JP6715226B2 (ja) 2017-10-25 2020-07-01 株式会社Ｓｕｂａｒｕ 複合材成形治具及び複合材成形方法
JP6663409B2 (ja) 2017-11-09 2020-03-11 株式会社Ｓｕｂａｒｕ 連結構造
CN109352875B (zh) * 2018-11-19 2021-06-18 苏州银禧新能源复合材料有限公司 电池壳体阳模及热压工艺
CN110128158B (zh) * 2019-04-22 2021-11-02 湖南远辉复合材料有限公司 防热/隔热/承载一体化陶瓷基轻质夹芯结构及其制备方法
JP7180011B2 (ja) * 2019-11-14 2022-11-29 三菱重工業株式会社 治具
CN112248307B (zh) * 2020-09-14 2021-11-19 大连理工大学 一种结构可调的折叠结构复材成型模具
CN114506095B (zh) * 2020-11-16 2024-01-26 中国商用飞机有限责任公司 一种用于制作帽型增强构件的芯模
DE102021107582A1 (de) 2021-03-25 2022-09-29 Hochschule Bremen, Körperschaft des öffentlichen Rechts Kollabierbarer Wickeldorn für die Herstellung von Faserverbundwerkstoffen sowie ein entsprechendes Verfahren
DE102021112516A1 (de) 2021-05-12 2022-11-17 Isar Aerospace Technologies GmbH Herstellung eines Faserverbundkörpers

Family Cites Families (98)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US103918A (en) * 1870-06-07 Improvement in cultivators
US216805A (en) * 1879-06-24 Improvement in detergent compounds
US56788A (en) * 1866-07-31 Improvement in wood-bending machines
US2269A (en) * 1841-09-25 John a
US2244107A (en) * 1937-10-15 1941-06-03 Hayes Econocrete Corp Of Ameri Collapsible core
US3143306A (en) * 1960-08-12 1964-08-04 Preload Corp Panel making apparatus
US3279739A (en) * 1965-07-19 1966-10-18 Long Construction Co Expandable core-former
US3279741A (en) * 1965-07-19 1966-10-18 Long Construction Co Expandable core-former
DE1604528A1 (de) 1966-06-16 1970-11-12 Bayer Ag Formkern zur Herstellung von Hohlkoerpern aller Art
US3551237A (en) * 1967-04-18 1970-12-29 Aerojet General Co Method of preparing filament-wound open beam structures
NL141121B (nl) 1967-11-02 1974-02-15 Eigenmann Ludwig Werkwijze voor de continue vervaardiging van buisvormige textielhouders voor buiselektroden.
US3629030A (en) * 1968-06-12 1971-12-21 Alvin G Ash Method for forming a mandrel and fabricating a duct thereabout
SU433038A1 (ru) 1971-02-10 1974-06-25 р СПШОБ НЕПРЕРЫВНОГО МЗГО'ЮВЛЕШЯ РЕЗИНОВЫХ РУКАВОВ НА ВЫПЛАВЛЯЕМОМДОРНЕ
US3754717A (en) * 1971-07-12 1973-08-28 Dana Corp Collapsible mandrel
JPS5044264A (pt) * 1973-08-23 1975-04-21
US3995081A (en) * 1974-10-07 1976-11-30 General Dynamics Corporation Composite structural beams and method
US4094688A (en) * 1975-08-21 1978-06-13 Wolf Franz Josef Method and molding core for making a flexible hollow molded body which is open on a number of sides
DE2609006B2 (de) * 1976-03-04 1979-10-31 Helios Apparatebau Kg, Mueller & Co, 7220 Schwenningen Aus faserverstärktem Kunststoff gegossener, hohler Ventilatorflügel
GB1522432A (en) 1976-10-21 1978-08-23 Ruggeri V Method of moulding hollow stiffeners or lightweight laminates or wholly box girdered laminates in fibre reinforced plastics
US4155970A (en) * 1977-11-04 1979-05-22 Mcdonnell Douglas Corporation Method for making a hollow composite using a destructible core
DE2757473A1 (de) 1977-12-22 1979-07-05 Bayer Ag Verfahren zum entformen eines auf einem kern aufgebauten kunststoff-formteils
GB2067455A (en) * 1979-02-20 1981-07-30 Rolls Royce Composite structure
JPS5818240A (ja) 1981-07-28 1983-02-02 Dainichi Nippon Cables Ltd 狭口容器の製造方法
JPS59121172U (ja) * 1983-02-04 1984-08-15 ミネソタ・マイニング・アンド・マニユフアクチユアリング・コンパニ− ケーブル電線被覆の剥離部分のカバー装置
JPS59157807A (ja) * 1983-02-28 1984-09-07 Nec Home Electronics Ltd ビデオテ−プレコ−ダ
JPS59157807U (ja) * 1983-04-07 1984-10-23 三菱重工業株式会社 繊維強化プラスチツクの中空構造物
RU1123235C (ru) 1983-08-19 1993-02-15 Всесоюзный Научно-Исследовательский Институт Резинотехнического Машиностроения Диафрагменный узел дл формовани и вулканизации покрышек
US4520988A (en) * 1984-04-23 1985-06-04 Harsco Corporation Concrete core-wall form and stripping assembly therefor
DE3421364A1 (de) * 1984-06-08 1985-12-12 Bayer Ag, 5090 Leverkusen Verfahren und vorrichtung zum kontinuierlichen herstellen von laenglichen hohlkoerpern, insbesondere von schlaeuchen, rohren oder innenlinern fuer solche, aus einem fluessigen material, wie reaktionsgemisch oder schmelze
JPS61188425A (ja) 1985-02-18 1986-08-22 Toyota Motor Corp 摩擦材の製造方法
EP0212140B1 (en) 1985-08-22 1990-05-02 The Budd Company Method of making a hollow fiber reinforced structure
US4675061A (en) 1985-09-24 1987-06-23 Grumman Aerospace Corporation Method for forming corrugated materials using memory metal cores
US4943334A (en) 1986-09-15 1990-07-24 Compositech Ltd. Method for making reinforced plastic laminates for use in the production of circuit boards
DE3715915A1 (de) 1987-05-13 1988-12-08 Minnesota Mining & Mfg Stuetzwendel fuer einen radial gedehnten huelsenkoerper
US5045251A (en) * 1987-06-15 1991-09-03 Ford Motor Company Method of resin transfer molding a composite article
DE8711336U1 (de) 1987-08-20 1987-10-22 Ems-Inventa AG, Zürich Formkern zur Herstellung von Hohlkörpern
DD277234A1 (de) * 1988-11-21 1990-03-28 Staaken Plastverarbeitung Vorrichtung zur herstellung von rohren aus glasfaserverstaerkten ungesaettigten kunstharzen
JPH0722977B2 (ja) 1989-03-22 1995-03-15 三ツ星ベルト株式会社 ローエッジベルトの製造方法および成形型
DE3911312C1 (en) 1989-04-07 1990-04-19 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De Mould core (former) for winding a fibre-reinforced body of plastic
US5041315A (en) * 1989-05-15 1991-08-20 Zircoa Inc. Flexible ceramic member and method of production thereof
US5176864A (en) * 1989-06-12 1993-01-05 Aluminum Company Of America Lost wax process utilizing a high temperature wax-based material
JPH03277532A (ja) 1990-03-28 1991-12-09 Nippon Steel Chem Co Ltd 繊維強化プラスチック曲管の製造方法
CA2056224A1 (en) 1990-12-19 1992-06-20 Terry Martin Boustead Conformal composite molding
JPH0767704B2 (ja) 1991-02-21 1995-07-26 川崎重工業株式会社 中空複合部材の製造方法
US5262121A (en) * 1991-12-18 1993-11-16 Goodno Kenneth T Method of making and using flexible mandrel
US5387098A (en) * 1992-04-23 1995-02-07 The Boeing Company Flexible reusable mandrels
DE4224526A1 (de) 1992-07-24 1994-01-27 Siemens Ag Kaltschrumpf-Schlauch
JPH06106632A (ja) 1992-09-30 1994-04-19 Sakura Rubber Kk 複合材製品の成形方法
US5354195A (en) * 1992-12-23 1994-10-11 United Technologies Corporation Composite molding apparatus for high pressure co-cure molding of lightweight honeycomb core composite articles having ramped surfaces utilizing low density, stabilized ramped honeycomb cores
GB2284173A (en) 1993-02-06 1995-05-31 Alan Harper Collapsible core tool for lost-core moulding
RU2143341C1 (ru) 1993-07-21 1999-12-27 Э.Хашогги Индастриз Изделие, изготовленное из неорганически наполненного материала, способ его изготовления и устройство для его осуществления (варианты)
AU1194595A (en) 1993-11-26 1995-06-13 Alan Roger Harper Casting method and apparatus and products thereof
US5505492A (en) * 1994-02-09 1996-04-09 Radius Engineering, Inc. Composite pole and manufacturing process for composite poles of varying non-circular cross-sections and curved center lines
GB2292332B (en) 1994-04-22 1999-04-28 Alan Roger Harper Moulding process and apparatus therefor
JPH08142060A (ja) 1994-11-21 1996-06-04 Sumino Kogyo Kk 中子の製造方法とその中子及び成形金型
JP2951561B2 (ja) 1995-01-27 1999-09-20 太陽誘電株式会社 電子機器用コイル部品
JP2640338B2 (ja) 1995-02-02 1997-08-13 富士夫 坂本 成型金型および成型方法
IT1275976B1 (it) 1995-03-27 1997-10-24 Pirelli Cavi S P A Ora Pirelli Supporto per un manicotto elastico
US6013125A (en) * 1995-09-13 2000-01-11 Quraishi; Mashallah M. Investment of powders and method for rapid preparation of investment molds
US5931830A (en) * 1995-12-07 1999-08-03 Sarcos L.C. Hollow coil guide wire apparatus for catheters
FR2745745B1 (fr) 1996-03-07 1998-04-10 Snecma Procede de fabrication d'une piece en materiau composite comportant une cavite revetue d'une protection de surface
US5989481A (en) * 1996-06-18 1999-11-23 You; Daniel H. Golf club shaft manufacturing process
US6692681B1 (en) * 1997-01-29 2004-02-17 Raytheon Aircraft Company Method and apparatus for manufacturing composite structures
US6340509B1 (en) * 1997-04-23 2002-01-22 Radius Engineering, Inc. Composite bicycle frame and method of construction thereof
SE509503C2 (sv) 1997-05-12 1999-02-01 Volvo Ab Arrangemang, förfarande och hålkropp vid formning av plastdetaljer
JPH1190979A (ja) 1997-09-19 1999-04-06 Tokai Rubber Ind Ltd 曲形ホースの製造方法
US6458309B1 (en) * 1998-06-01 2002-10-01 Rohr, Inc. Method for fabricating an advanced composite aerostructure article having an integral co-cured fly away hollow mandrel
WO2000001520A1 (en) 1998-07-03 2000-01-13 Bonus Energy A/S Method for producing closed composite structures and moulding apparatus to be used by the method
US6889937B2 (en) 1999-11-18 2005-05-10 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
AU3789801A (en) * 1999-12-07 2001-06-18 Boeing Company, The Double bag vacuum infusion process and system for low cost, advanced composite fabrication
WO2001062495A2 (en) * 2000-02-25 2001-08-30 The Boeing Company Laminated composite radius filler
DE10013409C1 (de) 2000-03-17 2000-11-23 Daimler Chrysler Ag Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen mittels eines Injektionsverfahrens
EP1190828A1 (en) 2000-09-26 2002-03-27 Recticel Method and mould for manufacturing polyurethane articles
EP1197309B1 (de) * 2000-10-04 2004-04-07 Alcan Technology & Management AG Verfahren zur Herstellung von Bauteilen aus Faserverbundkunststoffen
US6823578B2 (en) 2000-11-15 2004-11-30 Toyota Motor Sales, U.S.A., Inc. One-piece closed-shape structure and method of forming same
US6638466B1 (en) * 2000-12-28 2003-10-28 Raytheon Aircraft Company Methods of manufacturing separable structures
JP4721251B2 (ja) 2001-09-03 2011-07-13 富士重工業株式会社 複合材補強板の製造方法
JP4690613B2 (ja) 2001-09-28 2011-06-01 富士重工業株式会社 複合材製中空体の製造方法
US7344670B2 (en) 2002-03-28 2008-03-18 Build A Mold Limited Lost core plastic molding process for transferring, positioning and molding inserts into a plastic part
US7559332B2 (en) 2002-07-02 2009-07-14 Toyota Motor Sales U.S.A., Inc. Media removal apparatus and methods of removing media
US7217380B2 (en) 2002-07-22 2007-05-15 Toyota Motor Sales, Usa, Inc. Vibration apparatus and methods of vibration
US7101453B2 (en) 2002-09-04 2006-09-05 Toyota Motor Sales U.S.A., Inc. Pre-filled contained media volumes and methods of media filling using pre-filled contained media volumes
RU2242369C1 (ru) 2003-05-19 2004-12-20 Федеральное государственное унитарное предприятие "Обнинское научно-производственное предприятие "Технология" Опорный узел трехслойной панели
DE10342867B4 (de) 2003-09-15 2008-05-29 Eurocopter Deutschland Gmbh Verfahren zur Herstellung eines wasserlöslichen Formkerns
US7294220B2 (en) * 2003-10-16 2007-11-13 Toyota Motor Sales, U.S.A., Inc. Methods of stabilizing and/or sealing core material and stabilized and/or sealed core material
US7293737B2 (en) * 2004-04-20 2007-11-13 The Boeing Company Co-cured stringers and associated mandrel and fabrication method
US7531058B2 (en) * 2005-02-24 2009-05-12 The Boeing Company Reinforced rampdown for composite structural member and method for same
RU2285613C1 (ru) 2005-05-18 2006-10-20 Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") Способ изготовления многослойного изделия из полимерных композиционных материалов
US7633040B2 (en) * 2005-11-14 2009-12-15 The Boeing Company Bulk resin infusion system apparatus and method
ATE485188T1 (de) 2005-12-02 2010-11-15 Haldex Traction Ab Verfahren und system zur fahrdynamikregelung
FR2898539B1 (fr) 2006-03-20 2008-05-23 Eads Ccr Groupement D Interet Procede de realisation de panneaux raidis en materiau composite et panneaux ainsi realises
WO2008003733A1 (en) 2006-07-06 2008-01-10 Airbus Deutschland Gmbh Method and moulding core for producing a fibre composite component for aviation and spaceflight and fibre composite component obtained thereby
DE102006031326B4 (de) 2006-07-06 2010-09-23 Airbus Deutschland Gmbh Formkern und Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031325B4 (de) 2006-07-06 2010-07-01 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031336B4 (de) 2006-07-06 2010-08-05 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils in der Luft- und Raumfahrt
DE102006031323B4 (de) 2006-07-06 2010-07-15 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031334A1 (de) * 2006-07-06 2008-01-10 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031335B4 (de) 2006-07-06 2011-01-27 Airbus Operations Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt

Also Published As

Publication number Publication date
US20090166921A1 (en) 2009-07-02
DE102006031335B4 (de) 2011-01-27
DE102006031335A1 (de) 2008-01-10
CN101466514B (zh) 2013-01-09
EP2038099A1 (en) 2009-03-25
JP2009542460A (ja) 2009-12-03
WO2008003767A1 (en) 2008-01-10
RU2437762C2 (ru) 2011-12-27
US8500085B2 (en) 2013-08-06
CN101466514A (zh) 2009-06-24
JP5583969B2 (ja) 2014-09-03
RU2009102870A (ru) 2010-08-20
CA2651498A1 (en) 2008-01-10

Similar Documents

Publication Publication Date Title
BRPI0713560A2 (pt) método para fabricar um componente de fibra compósita utilizando um núcleo de moldagem dobrável, e o dito núcleo de moldagem
BR112017020233A2 (pt) núcleo cerâmico, uso de um núcleo cerâmico, método de fabricação para fabricar uma pá de turbina oca para um motor de turbina, e, motor de turbina
BR112013017815A2 (pt) módulo sublaminado, estrutura de compósito laminado e método para fabricar os mesmos
BR112012008606A2 (pt) luva multiusos
BRPI0809212B8 (pt) processo de purificação abreviado para a produção de polissacarídeos capsulares de streptococcus pneumoniae
BR112012007424A2 (pt) máquina para a fabriação de formas de dosagem utilizando energia de radiofrequência.
BR112017017389A2 (pt) método para fabricação de uma lâmina de motor de turbina.
ATE522701T1 (de) Turbinenschaufel
BR112016014911A8 (pt) fibra inorgânica com encolhimento e resistência aumentados
BR112012029740A2 (pt) estrutura de junção e método para produzir uma junção
BR112018009047A8 (pt) processo para fabricação de uma peça de material compósito.
FR2983428B1 (fr) Procede de fabrication d'une aube de turbomachine en materiau composite a plates-formes integrees
NO20080482L (no) Arrangement av avstandsstykke med smeltbart forbindelsesstykke for isolerglassenheter
BR112014032147A2 (pt) processo para a preparação de um derivado de polissacarídeo, e, derivado de polissacarídeo
EA200870277A1 (ru) Профильный сегмент и способ его изготовления
BR112013020426A2 (pt) processo e sistema para fabricação de produtos de material compósito, assim como produtos fabricados com este processo ou sistema
BR112014009659A2 (pt) célula de transdutor micro-usinado, capacitivo, pré-colapsada; e método de fabricação de uma célula de transdutor micro-usinado, capacitivo, pré-colapsada
BR112014005409B8 (pt) método de fabricação de um setor a partir de um material compósito para um bocal de turbina ou um difusor de compressor de um motor de turbina, turbina e compressor para um motor de turbina, e, motor de turbina
BR112013022365A2 (pt) processo para a produção de um componente de compósito de fibras e um conjunto de ferramentas para o mesmo
BR112015009105A2 (pt) esfera, polímero de hialuronato e glucomanana, usos de um polímero de hialuronato e glucomanana e de uma esfera, composição cosmética ou dermatológica para administração tópica, e, processo para sintetizar uma esfera
BRPI0823214A8 (pt) dobradura para embalagem de artigos higiênicos descartáveis que possuem cintos
BR112015006777A2 (pt) fabricação de uma vidraça laminada munida de um condutor elétrico
BR112015006380A2 (pt) palheta de motor de turbina, e, motor de turbina
BR112015007950A2 (pt) processo de fabricação de uma biela por enrolamento filamentar e biela
WO2014173671A3 (de) Werkzeug zur herstellung eines faser-kunststoff-verbund-bauteils mit wenigstens einer entlüftungsbohrung und darin angeordnetem auswerferstift

Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: AIRBUS OPERATIONS GMBH (DE)

B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]