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MX365743B - Método y aparato para reducir el arrugamiento de capas de láminas compuestas durante su formación. - Google Patents

Método y aparato para reducir el arrugamiento de capas de láminas compuestas durante su formación.

Info

Publication number
MX365743B
MX365743B MX2015011251A MX2015011251A MX365743B MX 365743 B MX365743 B MX 365743B MX 2015011251 A MX2015011251 A MX 2015011251A MX 2015011251 A MX2015011251 A MX 2015011251A MX 365743 B MX365743 B MX 365743B
Authority
MX
Mexico
Prior art keywords
during forming
composite laminates
ply wrinkling
laminates during
charge
Prior art date
Application number
MX2015011251A
Other languages
English (en)
Other versions
MX2015011251A (es
Inventor
T Kline William
G Harris Christopher
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of MX2015011251A publication Critical patent/MX2015011251A/es
Publication of MX365743B publication Critical patent/MX365743B/es

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
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/56—Tensioning reinforcements before or during shaping
    • 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
    • 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
    • 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
    • B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2307/00—Use of elements other than metals as reinforcement
    • B29K2307/04—Carbon
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2309/00—Use of inorganic materials not provided for in groups B29K2303/00 - B29K2307/00, as reinforcement
    • B29K2309/08—Glass
    • 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
    • B29L2009/00—Layered products

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)

Abstract

El arrugamiento de capas durante la formación por drapeado en caliente de una lámina compuesta (28) se reduce en los radios de esquina (25). Un material tensor (52) colocado sobre una carga de lámina compuesta no curada (28) mantiene una fuerza compresiva en la carga de lámina (28) mientras la carga (28) es formada sobre una herramienta (40).
MX2015011251A 2013-03-19 2014-02-25 Método y aparato para reducir el arrugamiento de capas de láminas compuestas durante su formación. MX365743B (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/847,046 US9573301B2 (en) 2013-03-19 2013-03-19 Methodfor reducing ply wrinkling of composite laminates during forming
PCT/US2014/018346 WO2014149428A2 (en) 2013-03-19 2014-02-25 Method and apparatus for reducing ply wrinkling of composite laminates during forming

Publications (2)

Publication Number Publication Date
MX2015011251A MX2015011251A (es) 2015-12-03
MX365743B true MX365743B (es) 2019-06-12

Family

ID=50277361

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2015011251A MX365743B (es) 2013-03-19 2014-02-25 Método y aparato para reducir el arrugamiento de capas de láminas compuestas durante su formación.

Country Status (7)

Country Link
US (2) US9573301B2 (es)
EP (1) EP2976212B1 (es)
JP (1) JP6262842B2 (es)
CN (1) CN105073393B (es)
CA (1) CA2899074C (es)
MX (1) MX365743B (es)
WO (1) WO2014149428A2 (es)

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US10150233B2 (en) * 2013-03-19 2018-12-11 The Boeing Company Method and apparatus for reducing ply wrinkling of composite laminates during forming
JP6543577B2 (ja) * 2016-01-22 2019-07-10 三菱重工業株式会社 複合材の成形方法及び複合材の成形用治具
US10059065B2 (en) * 2016-04-06 2018-08-28 Spirit Aerosystems, Inc. Method for eliminating radius wrinkles in composite laminates
US10105940B2 (en) * 2016-04-18 2018-10-23 The Boeing Company Formation of composite laminates having one or more divergent flanges
US10889072B2 (en) 2016-05-24 2021-01-12 The Boeing Company Method for pre-preg manufacturing
US10308000B2 (en) * 2016-05-24 2019-06-04 The Boeing Company Method for pre-preg manufacturing
US10155062B2 (en) 2016-05-24 2018-12-18 The Boeing Company Thermoresponsive adhesive material, method of making the material and methods of use
JP6785866B2 (ja) 2016-09-07 2020-11-18 三菱重工業株式会社 複合材の成形方法及び複合材の成形用治具
CN106564202B (zh) * 2016-09-23 2019-01-25 中航复合材料有限责任公司 一种真空导入成型制备混杂复合材料u型件的方法
US10875232B2 (en) * 2017-04-04 2020-12-29 The Boeing Company Composite part and method for making composite part
CN108327320B (zh) * 2018-03-07 2020-05-01 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种翼梁模具
CN109624353B (zh) * 2018-12-20 2020-12-22 武汉理工大学 一种改善l型复合材料层合板的固化成型质量的方法
US11318689B2 (en) * 2018-12-21 2022-05-03 The Boeing Company Ply transporting and compacting apparatus and method therefor
ES2961745T3 (es) * 2019-05-31 2024-03-13 Cytec Ind Inc Conformado al vacío con cizallamiento controlado para moldear preformas
US11511500B2 (en) * 2019-10-04 2022-11-29 The Boeing Company Molding system and methods for forming structures
US11518121B2 (en) * 2019-10-14 2022-12-06 The Boeing Company Constrained creep forming of contoured composite stiffeners
US11260607B2 (en) 2020-02-11 2022-03-01 The Boeing Company Forming systems and methods for drape forming a composite charge
US11498288B2 (en) 2020-02-11 2022-11-15 The Boeing Company Forming systems and methods for drape forming a composite charge
US11479002B2 (en) 2020-04-23 2022-10-25 Raytheon Technologies Corporation Compression tool and method of forming gas turbine engine components
JP6764179B1 (ja) * 2020-05-28 2020-09-30 株式会社Ｔｈｅ ＭＯＴ Ｃｏｍｐａｎｙ 金型
US11752711B2 (en) 2021-01-18 2023-09-12 Spirit Aerosystems, Inc. System and method for promoting inter-ply slippage
US11931975B2 (en) 2021-02-19 2024-03-19 The Boeing Company Forming systems and methods for forming an elongate charge of composite material
US20240308156A1 (en) * 2023-03-15 2024-09-19 Spirit Aerosystems, Inc. Method for using expendable flexures for forming composite laminates

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Also Published As

Publication number Publication date
US20140284836A1 (en) 2014-09-25
CA2899074C (en) 2018-01-23
US10307974B2 (en) 2019-06-04
CN105073393B (zh) 2017-09-29
CA2899074A1 (en) 2014-09-25
WO2014149428A3 (en) 2015-01-22
EP2976212A2 (en) 2016-01-27
US9573301B2 (en) 2017-02-21
CN105073393A (zh) 2015-11-18
EP2976212B1 (en) 2018-05-30
JP6262842B2 (ja) 2018-01-17
US20170087782A1 (en) 2017-03-30
WO2014149428A2 (en) 2014-09-25
JP2016514634A (ja) 2016-05-23
MX2015011251A (es) 2015-12-03

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