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BR9510294A - Método para produzir artigos compósitos de núcleo alveolar - Google Patents

Método para produzir artigos compósitos de núcleo alveolar

Info

Publication number
BR9510294A
BR9510294A BR9510294A BR9510294A BR9510294A BR 9510294 A BR9510294 A BR 9510294A BR 9510294 A BR9510294 A BR 9510294A BR 9510294 A BR9510294 A BR 9510294A BR 9510294 A BR9510294 A BR 9510294A
Authority
BR
Brazil
Prior art keywords
composite core
producing composite
core articles
articles
producing
Prior art date
Application number
BR9510294A
Other languages
English (en)
Inventor
William V Forster
Kenneth M Nowak
Larry J Osiecki
Original Assignee
Sikorsky Aircraft 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 Sikorsky Aircraft Corp filed Critical Sikorsky Aircraft Corp
Priority to BR9510294A priority Critical patent/BR9510294A/pt
Publication of BR9510294A publication Critical patent/BR9510294A/pt

Links

Classifications

    • 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
    • B29C70/30Shaping 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
    • B29C70/34Shaping 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
    • B29C70/342Shaping 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
    • 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
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/543Fixing the position or configuration of fibrous reinforcements before or during moulding
    • 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
    • B29D24/00Producing articles with hollow walls
    • B29D24/002Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
    • B29D24/005Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb
    • B29D24/007Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb and a chamfered edge

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Textile Engineering (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Laminated Bodies (AREA)
BR9510294A 1995-01-27 1995-01-27 Método para produzir artigos compósitos de núcleo alveolar BR9510294A (pt)

Priority Applications (1)

Application Number Priority Date Filing Date Title
BR9510294A BR9510294A (pt) 1995-01-27 1995-01-27 Método para produzir artigos compósitos de núcleo alveolar

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
PCT/US1995/001099 WO1996022878A1 (en) 1995-01-27 1995-01-27 Method for making honeycomb core composite articles
BR9510294A BR9510294A (pt) 1995-01-27 1995-01-27 Método para produzir artigos compósitos de núcleo alveolar

Publications (1)

Publication Number Publication Date
BR9510294A true BR9510294A (pt) 1997-11-11

Family

ID=22248575

Family Applications (1)

Application Number Title Priority Date Filing Date
BR9510294A BR9510294A (pt) 1995-01-27 1995-01-27 Método para produzir artigos compósitos de núcleo alveolar

Country Status (11)

Country Link
US (1) US5897739A (pt)
EP (1) EP0805747B1 (pt)
JP (1) JP3403201B2 (pt)
KR (1) KR19980701706A (pt)
AU (1) AU2584095A (pt)
BR (1) BR9510294A (pt)
DE (1) DE69506447T2 (pt)
ES (1) ES2124550T3 (pt)
IL (1) IL116783A (pt)
TW (1) TW421627B (pt)
WO (1) WO1996022878A1 (pt)

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DE102009010621B3 (de) * 2009-02-12 2010-12-02 Mt Aerospace Ag Wabenstabilisierung
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EP2266784A1 (en) * 2009-06-22 2010-12-29 Eurocopter Deutschland GmbH Method for producing a sandwich component having a honeycomb core
ES2423186T3 (es) * 2009-08-20 2013-09-18 Siemens Aktiengesellschaft Estructura de plástico reforzado con fibra y método para producir la estructura de plástico reforzado con fibra
US8491743B2 (en) * 2009-12-15 2013-07-23 The Boeing Company Composite ply stabilizing method
US10369772B2 (en) 2012-07-10 2019-08-06 Textron Innovations Inc. Method of making core-stiffened structure
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GB201200912D0 (en) * 2012-01-19 2012-02-29 Airbus Operations Ltd Fastener receptacle strip
US10357925B2 (en) 2013-12-20 2019-07-23 United Technologies Corporation Enhanced volatile removal for composite layup
EP3089876B1 (en) * 2013-12-20 2020-05-06 United Technologies Corporation Enhanced volatile removal for composite layup
JP6199191B2 (ja) * 2014-01-10 2017-09-20 公益財団法人鉄道総合技術研究所 接合材の製造方法
RU2559446C1 (ru) * 2014-03-05 2015-08-10 Открытое акционерное общество "Обнинское научно-производственное предприятие "Технология" Способ изготовления трехслойной панели из композиционного материала
RU2564952C1 (ru) * 2014-04-14 2015-10-10 Акционерное общество "Обнинское научно-производственное предприятие "Технология" им. А.Г. Ромашина" Способ изготовления трехслойной панели из композиционного материала
GB201514579D0 (en) 2015-08-17 2015-09-30 Invibio Device Component Mfg Ltd A device
CN107627625B (zh) * 2016-07-18 2021-04-09 深圳光启高等理工研究院 复合材料制件的阴模成型方法
RU2685218C1 (ru) * 2017-12-18 2019-04-16 Общество с ограниченной ответственностью "Тулпар Интерьер Групп" Способ изготовления криволинейной трехслойной композитной панели
US11007724B2 (en) * 2018-08-08 2021-05-18 Textron Innovations Inc. Skin-to-core bond line mapping system and method
CN111745999A (zh) * 2020-06-12 2020-10-09 陕西飞机工业(集团)有限公司 一种带r角复合材料件的外观加工方法
CN112223783A (zh) * 2020-09-22 2021-01-15 肇庆市海特复合材料技术研究院 一种复合材料电池包下框的成型模具及制备方法
CN112454938A (zh) * 2020-09-30 2021-03-09 成都飞机工业(集团)有限责任公司 一种碳纤维蜂窝夹心复合材料构件的成型方法
KR102369172B1 (ko) * 2021-05-11 2022-03-03 한국항공우주산업 주식회사 항공기용 복합재 성형 장치
US11413795B1 (en) * 2021-08-12 2022-08-16 King Abdulaziz University Method of making composite from green material
KR102395954B1 (ko) * 2021-11-01 2022-05-12 덕양산업 주식회사 진공압력을 이용한 내장재 제조 장치
CN115302812B (zh) * 2022-06-29 2025-04-08 中航西安飞机工业集团股份有限公司 一种共胶接工艺制造大曲率复合材料零件的封装方法
CN115350976A (zh) * 2022-07-21 2022-11-18 成都飞机工业(集团)有限责任公司 一种芳纶纸蜂窝芯抗侧压预处理方法及芳纶纸蜂窝芯
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Also Published As

Publication number Publication date
KR19980701706A (ko) 1998-06-25
DE69506447T2 (de) 1999-07-01
TW421627B (en) 2001-02-11
DE69506447D1 (de) 1999-01-14
IL116783A0 (en) 1996-05-14
JPH10512820A (ja) 1998-12-08
IL116783A (en) 2000-07-26
EP0805747A1 (en) 1997-11-12
EP0805747B1 (en) 1998-12-02
US5897739A (en) 1999-04-27
WO1996022878A1 (en) 1996-08-01
JP3403201B2 (ja) 2003-05-06
AU2584095A (en) 1996-08-14
ES2124550T3 (es) 1999-02-01

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Legal Events

Date Code Title Description
FB34 Technical and formal requirements: requirement - article 34 of industrial property law
FA14 Dismissal: dismissal - article 34 of industrial property law
B11T Dismissal of application maintained [chapter 11.20 patent gazette]