KR101778818B1 - 복합재 플라이의 안정화 기구 및 방법 - Google Patents

복합재 플라이의 안정화 기구 및 방법 Download PDF

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Publication number
KR101778818B1
KR101778818B1 KR1020127014195A KR20127014195A KR101778818B1 KR 101778818 B1 KR101778818 B1 KR 101778818B1 KR 1020127014195 A KR1020127014195 A KR 1020127014195A KR 20127014195 A KR20127014195 A KR 20127014195A KR 101778818 B1 KR101778818 B1 KR 101778818B1
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South Korea
Prior art keywords
grip strip
core
laminate
composite structure
tool
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KR1020127014195A
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Korean (ko)
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KR20120115240A (ko
Inventor
도안 디. 팸
마크 더블유. 톨란
리차드 엠. 아우트젠
존 씨. 락리어
크리스토퍼 지. 해리스
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더 보잉 컴파니
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    • 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
    • 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
    • B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
    • 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
    • B29D99/0021—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with plain or filled structures, e.g. cores, placed between two or more plates or sheets, e.g. in a matrix
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/10—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1089—Methods of surface bonding and/or assembly therefor of discrete laminae to single face of additional lamina
    • Y10T156/1092—All laminae planar and face to face
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/31504—Composite [nonstructural laminate]

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Structural Engineering (AREA)
  • Civil Engineering (AREA)
  • Architecture (AREA)
  • Textile Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
KR1020127014195A 2009-12-15 2010-11-12 복합재 플라이의 안정화 기구 및 방법 Active KR101778818B1 (ko)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/638,947 2009-12-15
US12/638,947 US8491743B2 (en) 2009-12-15 2009-12-15 Composite ply stabilizing method
PCT/US2010/056470 WO2011081726A1 (en) 2009-12-15 2010-11-12 Composite ply stabilizing mechanism and method

Publications (2)

Publication Number Publication Date
KR20120115240A KR20120115240A (ko) 2012-10-17
KR101778818B1 true KR101778818B1 (ko) 2017-09-14

Family

ID=43778432

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Application Number Title Priority Date Filing Date
KR1020127014195A Active KR101778818B1 (ko) 2009-12-15 2010-11-12 복합재 플라이의 안정화 기구 및 방법

Country Status (10)

Country Link
US (2) US8491743B2 (enExample)
EP (1) EP2512784B1 (enExample)
JP (1) JP5728492B2 (enExample)
KR (1) KR101778818B1 (enExample)
CN (1) CN102686382B (enExample)
BR (1) BR112012014516B1 (enExample)
CA (1) CA2777849C (enExample)
ES (1) ES2451524T3 (enExample)
PT (1) PT2512784E (enExample)
WO (1) WO2011081726A1 (enExample)

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US9079674B1 (en) * 2009-09-18 2015-07-14 Blue Origin, Llc Composite structures for aerospace vehicles, and associated systems and methods
US20120199292A1 (en) * 2011-02-03 2012-08-09 Sikorsky Aircraft Corporation Ply locking for honeycomb panels
US8826957B2 (en) * 2012-08-31 2014-09-09 General Electric Company Methods and systems for automated ply layup for composites
US9149991B2 (en) * 2012-10-01 2015-10-06 The Boeing Company Bond assembly jig and method
US9517594B2 (en) * 2012-10-04 2016-12-13 The Boeing Company Composite structure having a stabilizing element
US20170276160A1 (en) * 2014-04-15 2017-09-28 Changize Sadr Structural assembly and method
CN105539809A (zh) * 2014-10-28 2016-05-04 哈尔滨飞机工业集团有限责任公司 一种分段式蜂窝夹层结构
US10569481B2 (en) 2017-06-26 2020-02-25 General Electric Company Shaped composite ply layups and methods for shaping composite ply layups
US10654208B2 (en) * 2017-09-20 2020-05-19 Bell Helicopter Textron Inc. Assembly fixture with anisotropic thermal properties
US10677075B2 (en) 2018-05-04 2020-06-09 General Electric Company Composite airfoil assembly for an interdigitated rotor
US10941665B2 (en) 2018-05-04 2021-03-09 General Electric Company Composite airfoil assembly for an interdigitated rotor
US10934854B2 (en) 2018-09-11 2021-03-02 General Electric Company CMC component cooling cavities
US11040915B2 (en) 2018-09-11 2021-06-22 General Electric Company Method of forming CMC component cooling cavities
US12330214B1 (en) 2019-02-11 2025-06-17 Blue Origin Manufacturing, LLC Printed porous media, such as for use in aerospace parts, and associated systems and methods
GB201913332D0 (en) 2019-09-16 2019-10-30 Blade Dynamics Ltd A container comprising fibre material for a fibre-reinforced composite component
US11156110B1 (en) 2020-08-04 2021-10-26 General Electric Company Rotor assembly for a turbine section of a gas turbine engine
US11655719B2 (en) 2021-04-16 2023-05-23 General Electric Company Airfoil assembly
US20220402828A1 (en) * 2021-06-18 2022-12-22 Goodrich Corporation Shape forming opf preform
US11845699B2 (en) 2021-09-07 2023-12-19 Blue Origin, Llc Methods for manufacturing coated composite materials
US12485575B2 (en) * 2022-08-16 2025-12-02 Rohr, Inc. Forming a preform into a shaped body
CN118082237B (zh) * 2024-04-29 2024-08-09 成都飞机工业（集团）有限责任公司 改善蜂窝夹芯构件表面质量成型方法

Citations (3)

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WO1996022878A1 (en) 1995-01-27 1996-08-01 Sikorsky Aircraft Corporation Method for making honeycomb core composite articles
WO2001047695A1 (en) 1999-12-23 2001-07-05 Saab Ab A holding device for holding an article and a plant for heat treatment of an article
US20050051262A1 (en) 2003-09-09 2005-03-10 Erickson Dave G. Mandrel and method for manufacturing composite structures

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JPH03130064A (ja) 1986-07-31 1991-06-03 Kirin Brewery Co Ltd 酵母入りビール
US5290167A (en) * 1990-10-08 1994-03-01 Sumitomo Heavy Industries, Ltd. Method of manufacturing three-dimensional parts using sheets of thermoplastic resin high-performance fiber-reinforced composite material and apparatus therefor
JP3130064B2 (ja) * 1991-02-19 2001-01-31 新明和工業株式会社 ハニカムサンドイッチ複合材構造物の製造方法及び該方法に使用する端部押え具
US6045651A (en) * 1993-09-07 2000-04-04 The Boeing Company Hand assisted lamination system
JP3267789B2 (ja) * 1994-02-07 2002-03-25 富士重工業株式会社 ハニカムサンドイッチ構造物の製造方法および成形装置
CN1101751C (zh) * 1996-01-11 2003-02-19 波音公司 复合蜂窝夹层结构及制造方法
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BR9911045B1 (pt) * 1998-05-22 2009-08-11 uso de um tecido tratado quanto à rigidez, método para produzir um tecido tratado quanto à rigidez, tecido tratado quanto à rigidez, uso de uma matéria-prima de tecido tratado quanto à rigidez, método para produzir uma matéria-prima de tecido tratado quanto à rigidez, uso de uma camada pré-impregnada tratada quanto à rigidez, método para produzir uma camada pré-impregnada tratada quanto à rigidez para um precursor de estrutra em sanduìche alveolada tratada quanto à rigidez, estrutura em sanduìche alveolada tratada quanto à rigidez, método de produzir um precursor de estrutura em sanduìche alveolada tratada quanto à rigidez e método de produzir uma estrutura em sanduìche alveolada tratada quanto à rigidez.
GB9828368D0 (en) * 1998-12-22 1999-02-17 British Aerospace Forming reinforcing components
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Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1996022878A1 (en) 1995-01-27 1996-08-01 Sikorsky Aircraft Corporation Method for making honeycomb core composite articles
WO2001047695A1 (en) 1999-12-23 2001-07-05 Saab Ab A holding device for holding an article and a plant for heat treatment of an article
US20020192327A1 (en) 1999-12-23 2002-12-19 Roger Amnered Holding device for holding an article and a plant for heat treatment of an article
US20050051262A1 (en) 2003-09-09 2005-03-10 Erickson Dave G. Mandrel and method for manufacturing composite structures

Also Published As

Publication number Publication date
EP2512784B1 (en) 2014-01-08
BR112012014516B1 (pt) 2021-03-16
US8978729B2 (en) 2015-03-17
CA2777849C (en) 2015-02-17
WO2011081726A1 (en) 2011-07-07
US20110143140A1 (en) 2011-06-16
CN102686382B (zh) 2014-09-10
ES2451524T3 (es) 2014-03-27
BR112012014516A2 (pt) 2020-08-25
US8491743B2 (en) 2013-07-23
KR20120115240A (ko) 2012-10-17
CN102686382A (zh) 2012-09-19
JP5728492B2 (ja) 2015-06-03
JP2013513501A (ja) 2013-04-22
CA2777849A1 (en) 2011-07-07
US20130276987A1 (en) 2013-10-24
PT2512784E (pt) 2014-01-22
EP2512784A1 (en) 2012-10-24

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