ATE331604T1 - Prozess und werkzeuge zum reduzieren von thermisch induzierten restspannungen und formverzerrungen bei monolithischen verbundstrukturen - Google Patents

Prozess und werkzeuge zum reduzieren von thermisch induzierten restspannungen und formverzerrungen bei monolithischen verbundstrukturen

Info

Publication number
ATE331604T1
ATE331604T1 AT03380292T AT03380292T ATE331604T1 AT E331604 T1 ATE331604 T1 AT E331604T1 AT 03380292 T AT03380292 T AT 03380292T AT 03380292 T AT03380292 T AT 03380292T AT E331604 T1 ATE331604 T1 AT E331604T1
Authority
AT
Austria
Prior art keywords
tooling
subcomponent
monolithic composite
composite structures
tools
Prior art date
Application number
AT03380292T
Other languages
English (en)
Inventor
Martin Jose Manuel Menendez
Pastor Augusto Perez
Original Assignee
Airbus Espana Sl
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 Espana Sl filed Critical Airbus Espana Sl
Application granted granted Critical
Publication of ATE331604T1 publication Critical patent/ATE331604T1/de

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
    • B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
    • B29C37/005—Compensating volume or shape change during moulding, in general
    • 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
    • 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
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • 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
    • B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/0227—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould using pressure vessels, e.g. autoclaves, vulcanising pans
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Polishing Bodies And Polishing Tools (AREA)
  • Ceramic Products (AREA)
AT03380292T 2003-12-16 2003-12-16 Prozess und werkzeuge zum reduzieren von thermisch induzierten restspannungen und formverzerrungen bei monolithischen verbundstrukturen ATE331604T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP03380292A EP1543941B1 (de) 2003-12-16 2003-12-16 Prozess und Werkzeuge zum reduzieren von thermisch induzierten Restspannungen und Formverzerrungen bei monolithischen Verbundstrukturen

Publications (1)

Publication Number Publication Date
ATE331604T1 true ATE331604T1 (de) 2006-07-15

Family

ID=34486522

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03380292T ATE331604T1 (de) 2003-12-16 2003-12-16 Prozess und werkzeuge zum reduzieren von thermisch induzierten restspannungen und formverzerrungen bei monolithischen verbundstrukturen

Country Status (5)

Country Link
US (1) US7780899B2 (de)
EP (1) EP1543941B1 (de)
AT (1) ATE331604T1 (de)
DE (1) DE60306533T2 (de)
ES (1) ES2271513T3 (de)

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DE102007004312B4 (de) * 2007-01-29 2014-08-21 Airbus Operations Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für ein Luft- oder Raumfahrzeug
US7968021B2 (en) 2007-07-31 2011-06-28 The Boeing Company Coefficient of thermal expansion control structure
US20090309260A1 (en) * 2008-06-12 2009-12-17 Kenneth Herbert Keuchel Method of delivering a thermoplastic and/or crosslinking resin to a composite laminate structure
ES2364112B1 (es) * 2008-12-22 2012-07-04 Airbus Operations, S.L. Sistema de posicionamiento, manipulación y desmontaje de útiles para la fabricación de piezas aeronáuticas.
US9073270B2 (en) 2009-01-21 2015-07-07 Vestas Wind Systems A/S Method of manufacturing a wind turbine blade by embedding a layer of pre-cured fibre reinforced resin
ES2378682B1 (es) * 2010-06-18 2013-02-28 Airbus Operations, S.L. Método de fabricación de larguerillos con forma de "t" para un avión y herramienta de curado usada en el mismo.
ES2400129B1 (es) * 2011-05-30 2014-06-18 Airbus Operations, S.L. Método de fabricación de larguerillos con forma de "t" con un ángulo diferente de 90� entre el alma y el pie
DE102011079943A1 (de) * 2011-07-27 2013-01-31 Airbus Operations Gmbh Vorrichtung zur Herstellung eines Klebebauteils mit Faserverbundkunststoffen sowie Verfahren
CN102390121B (zh) * 2011-10-19 2013-12-25 南京航空航天大学 复合材料制件热压罐成型制件温度补偿方法
US8986484B2 (en) 2012-10-10 2015-03-24 The Boeing Company Shape-distorting tooling system and method for curing composite parts
US20160375668A1 (en) * 2014-07-09 2016-12-29 Sikorsky Aircraft Corporation Method of forming a composite structure
US10207788B2 (en) * 2016-04-12 2019-02-19 The Boeing Company Structure having joined unitary structures
CN108466434B (zh) * 2018-02-11 2020-11-20 航天材料及工艺研究所 一种多内腔工形梁及其高精度软模成型与缺陷控制工艺方法
DE102018112684A1 (de) 2018-05-28 2019-11-28 Airbus Operations Gmbh Verfahren und Vorrichtung zum Herstellen eines Bauteils aus Faserverbundwerkstoff
CN110341211B (zh) * 2019-07-30 2020-04-24 中南大学 一种热塑性复合材料工形加筋构件的模压成型模具组件
CN110341210B (zh) * 2019-07-30 2020-04-24 中南大学 带工字形加强筋的热塑性复合材料构件的模压成型方法
DE102019123084A1 (de) * 2019-08-28 2021-03-04 Airbus Operations Gmbh Verfahren und Vorrichtung
CN112454942B (zh) * 2020-11-05 2022-05-10 成都联科航空技术有限公司 一种控制曲面金属蜂窝复合材料固化变形的成型方法
CN118269376A (zh) * 2024-04-10 2024-07-02 中航西安飞机工业集团股份有限公司 一种降低加筋壁板固化变形的工艺方法

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US4350551A (en) * 1980-12-29 1982-09-21 The Boeing Company Fluid slip sheet and method
JPS58203014A (ja) * 1982-05-21 1983-11-26 Mitsubishi Heavy Ind Ltd 複合材料製品の成形法
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
US6045651A (en) * 1993-09-07 2000-04-04 The Boeing Company Hand assisted lamination system
US5817269A (en) * 1996-10-25 1998-10-06 The Boeing Company Composite fabrication method and tooling to improve part consolidation
US6733907B2 (en) * 1998-03-27 2004-05-11 Siemens Westinghouse Power Corporation Hybrid ceramic material composed of insulating and structural ceramic layers
DE19832441C1 (de) * 1998-07-18 2000-01-05 Daimler Chrysler Aerospace Verfahren zur Herstellung einer stringerversteiften Schale in Faserverbundbauweise
US6245275B1 (en) * 1999-05-13 2001-06-12 Vought Aircraft Industries, Inc. Method for fabricating composite structures
ES2185443B1 (es) * 2000-03-07 2004-09-01 Airbus España S.L. Procedimiento de fabricacion de piezas precuradas en material compuesto con rigidizadores aplicados en estado fresco.
ES2184551B1 (es) 2000-03-07 2004-09-01 Airbus España S.L. Procedimiento de fabricacion de estructuras primarias en material compuesto con curado en util hembra.
ES2205961B2 (es) * 2001-02-13 2005-03-01 Eads Construcciones Aeronauticas, S.A. Procedimiento de fabricacion de elementos de material compuesto mediante la tecnoclogia del coencolado.
US6828373B2 (en) * 2001-03-07 2004-12-07 Advanced Ceramics Research, Inc. Water soluble tooling materials for composite structures

Also Published As

Publication number Publication date
ES2271513T3 (es) 2007-04-16
DE60306533T2 (de) 2007-02-01
EP1543941A1 (de) 2005-06-22
US20050127576A1 (en) 2005-06-16
DE60306533D1 (de) 2006-08-10
US7780899B2 (en) 2010-08-24
EP1543941B1 (de) 2006-06-28

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