DE69300554D1 - Formverfahren und Vorrichtung zur Herstellung von aus zwei Sektoren bestehenden Verbundwerkstoffteilen. - Google Patents

Formverfahren und Vorrichtung zur Herstellung von aus zwei Sektoren bestehenden Verbundwerkstoffteilen.

Info

Publication number
DE69300554D1
DE69300554D1 DE69300554T DE69300554T DE69300554D1 DE 69300554 D1 DE69300554 D1 DE 69300554D1 DE 69300554 T DE69300554 T DE 69300554T DE 69300554 T DE69300554 T DE 69300554T DE 69300554 D1 DE69300554 D1 DE 69300554D1
Authority
DE
Germany
Prior art keywords
sectors
molding process
composite parts
manufacturing composite
parts consisting
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
DE69300554T
Other languages
English (en)
Other versions
DE69300554T2 (de
Inventor
Eric Philippe Georges Celerier
Philippe Henrio
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of DE69300554D1 publication Critical patent/DE69300554D1/de
Application granted granted Critical
Publication of DE69300554T2 publication Critical patent/DE69300554T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B29C70/34—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/342—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic 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
    • B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32—Component parts, details or accessories; Auxiliary operations
    • B29C43/36—Moulds for making articles of definite length, i.e. discrete articles
    • 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
    • B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/10—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
    • B29C43/12—Isostatic 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
DE69300554T 1992-06-03 1993-06-03 Formverfahren und Vorrichtung zur Herstellung von aus zwei Sektoren bestehenden Verbundwerkstoffteilen. Expired - Lifetime DE69300554T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9206697A FR2691922B1 (fr) 1992-06-03 1992-06-03 Procede et dispositif de moulage de piece en materiau composite constituee de deux secteurs.

Publications (2)

Publication Number Publication Date
DE69300554D1 true DE69300554D1 (de) 1995-11-02
DE69300554T2 DE69300554T2 (de) 1996-03-21

Family

ID=9430381

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69300554T Expired - Lifetime DE69300554T2 (de) 1992-06-03 1993-06-03 Formverfahren und Vorrichtung zur Herstellung von aus zwei Sektoren bestehenden Verbundwerkstoffteilen.

Country Status (5)

Country Link
US (2) US5304057A (de)
EP (1) EP0585144B1 (de)
JP (1) JP2949008B2 (de)
DE (1) DE69300554T2 (de)
FR (1) FR2691922B1 (de)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5814259A (en) * 1994-08-12 1998-09-29 The United States Of America As Represented By The United States National Aeronautics And Space Administration Method for molding structural parts utilizing modified silicone rubber
DE19717014A1 (de) * 1997-04-23 1998-10-29 Inst Mikrotechnik Mainz Gmbh Verfahren und Form zur Herstellung miniaturisierter Formenkörper
US6337102B1 (en) * 1997-11-17 2002-01-08 The Trustees Of Princeton University Low pressure vapor phase deposition of organic thin films
SE512507C2 (sv) * 1997-11-27 2000-03-27 Linlan Induction Ab Pressformverktyg samt sätt att förse ett sådant med ett gasevakueringsorgan
US6540954B1 (en) * 1999-07-30 2003-04-01 Resolute Racing Shells, Inc. Process for fabricating a rowing shell
US7622066B2 (en) * 2004-07-26 2009-11-24 The Boeing Company Methods and systems for manufacturing composite parts with female tools
US7306450B2 (en) * 2004-09-29 2007-12-11 The Boeing Company Apparatuses, systems, and methods for manufacturing composite parts
US7527759B2 (en) 2005-04-13 2009-05-05 The Boeing Company Method and apparatus for forming structural members
US8601694B2 (en) 2008-06-13 2013-12-10 The Boeing Company Method for forming and installing stringers
US8557165B2 (en) 2008-10-25 2013-10-15 The Boeing Company Forming highly contoured composite parts
US7655168B2 (en) * 2006-01-31 2010-02-02 The Boeing Company Tools for manufacturing composite parts and methods for using such tools
US7810666B2 (en) * 2006-07-07 2010-10-12 Kautex Textron Gmbh & Co. Kg Fuel tank seam with lead-through means
US7963098B2 (en) * 2007-06-12 2011-06-21 United Technologies Corporation Composite duct assembly
US8465613B2 (en) 2011-08-24 2013-06-18 The Boeing Company Method and apparatus for fabricating variable gauge, contoured composite stiffeners
US9254619B2 (en) 2008-05-28 2016-02-09 The Boeing Company Method and apparatus for fabricating variable gauge, contoured composite stiffeners
US8025499B2 (en) 2008-11-03 2011-09-27 Rohr, Inc. Multi-segment tool and method for composite formation
GB0903805D0 (en) * 2009-03-05 2009-04-22 Airbus Uk Ltd Method of manufacturing composite parts
EP2531341B1 (de) * 2010-02-05 2016-03-30 Learjet Inc. Vorrichtung und verfahren zur herstellung eines bauteiles aus komposit-material
US9387628B2 (en) 2011-08-24 2016-07-12 The Boeing Company Method and apparatus for fabricating composite stringers
US9248587B2 (en) * 2012-07-05 2016-02-02 General Electric Company Apparatus for manufacturing a flanged composite component and methods of manufacturing the same
US9523431B2 (en) 2013-05-31 2016-12-20 The Boeing Company Sealing and testing segmented tools
CN103358570A (zh) * 2013-07-30 2013-10-23 无锡乘风新能源设备有限公司 兆瓦级叶片合模过程中防止产品脱膜的方法
US9475218B2 (en) * 2014-03-21 2016-10-25 General Electric Company Apparatus and method for forming flanges on components
US9895848B2 (en) * 2015-04-22 2018-02-20 The Boeing Company Systems and tooling for manufacturing composite parts and related methods
US10369740B2 (en) 2015-07-09 2019-08-06 The Boeing Company Method of forming a contoured hat stiffener
CN110591356B (zh) * 2019-09-11 2022-02-22 长春长光宇航复合材料有限公司 一种透波复合材料半罩及其制备方法

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1616958A (en) * 1923-02-19 1927-02-08 Kurt Roehll Tube-splicing device
US1935535A (en) * 1931-03-14 1933-11-14 Ziegler Herman Artificial marble or stone
US2722962A (en) * 1951-12-04 1955-11-08 Goodyear Aircraft Corp Apparatus for making void-free fabric laminates
US3431331A (en) * 1965-02-16 1969-03-04 Kay Mfg Corp Anticlogging breathable mold and method
DE1913463A1 (de) * 1968-04-01 1969-11-13 Goodyear Tire & Rubber Verbundstruktur
US3814653A (en) * 1972-01-20 1974-06-04 Nasa Method of laminating structural members
DE2544664C2 (de) * 1975-10-06 1982-08-26 The Upjohn Co., 49001 Kalamazoo, Mich. Verfahren zur Herstellung eines Gegenstandes aus einem Grundkörper aus aufgeschäumtem Kunststoff und einer Oberflächenbeschichtung
US4310372A (en) * 1979-04-19 1982-01-12 Certain-Teed Corporation Method of making a well screen
US4518556A (en) * 1980-07-01 1985-05-21 Hitachi Shipbuilding & Engineering Co. Ltd. Method for molding bent pipes made up of composite material
FR2490993A3 (fr) * 1980-10-01 1982-04-02 Aerospatiale Procede et dispositif pour la realisation de corps creux en matiere stratifiee et corps creux ainsi obtenus
SU1243956A1 (ru) * 1985-02-05 1986-07-15 Предприятие П/Я Г-4913 Устройство дл изготовлени резиновых оболочек
GB2184053B (en) * 1985-12-12 1989-10-18 Rolls Royce Method of manufacturing an article form a fibre reinforced composite material
US4693678A (en) * 1986-01-15 1987-09-15 The Boeing Company Male layup-female molding system for fabricating reinforced composite structures
US4681651A (en) * 1986-08-07 1987-07-21 Lockheed Corporation Vacuum bag sealing system
FR2638673B1 (fr) * 1988-11-08 1991-03-22 Aerospatiale Outillage pour le moulage de panneaux auto-raidis en materiau composite
US5256366A (en) * 1991-01-08 1993-10-26 Richard Wejrock Method of molding fiberglass

Also Published As

Publication number Publication date
EP0585144A1 (de) 1994-03-02
FR2691922A1 (fr) 1993-12-10
FR2691922B1 (fr) 1994-07-22
EP0585144B1 (de) 1995-09-27
US5443784A (en) 1995-08-22
JP2949008B2 (ja) 1999-09-13
US5304057A (en) 1994-04-19
JPH0647824A (ja) 1994-02-22
DE69300554T2 (de) 1996-03-21

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SNECMA MOTEURS, PARIS, FR

8327 Change in the person/name/address of the patent owner

Owner name: SNECMA, PARIS, FR