KR920700107A - 복합재료 기포질 샌드위치 구조 - Google Patents

복합재료 기포질 샌드위치 구조

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Publication number
KR920700107A
KR920700107A KR1019900701558A KR900701558A KR920700107A KR 920700107 A KR920700107 A KR 920700107A KR 1019900701558 A KR1019900701558 A KR 1019900701558A KR 900701558 A KR900701558 A KR 900701558A KR 920700107 A KR920700107 A KR 920700107A
Authority
KR
South Korea
Prior art keywords
core
thermoplastic
film
sheet
layer
Prior art date
Application number
KR1019900701558A
Other languages
English (en)
Inventor
에드워드 오코노르 제임스
Original Assignee
제이 이이 휘립프스
휘립프스 피트로오리암 캄파니
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 제이 이이 휘립프스, 휘립프스 피트로오리암 캄파니 filed Critical 제이 이이 휘립프스
Publication of KR920700107A publication Critical patent/KR920700107A/ko

Links

Classifications

    • 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
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • 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
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • 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
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • 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
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
    • 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
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/08—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • 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
    • B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/146—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers whereby one or more of the layers is a honeycomb structure
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
    • E04C2/36—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels
    • E04C2/365—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels by honeycomb structures
    • 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
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/02—Cellular or porous
    • B32B2305/024—Honeycomb
    • 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
    • B32B2311/00—Metals, their alloys or their compounds
    • B32B2311/24—Aluminium

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Laminated Bodies (AREA)

Abstract

내용 없음

Description

복합재료 기포질 샌드위치 구조
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음
제 1 도는 본 발명의 복합재료 기포질 샌드위치 구조의 분해 투시도이다.
제 2 도는 투시도로 기포질 구조를 보여준다.
제 3 도는 기포질 샌드위치 구조의 제조 방법을 개략적으로 보여준다.

Claims (26)

  1. 기포질 코어; 및 상기 코어의 면에 인접하게 배치되고, 거기에 열 결합된 열가소성 플라스틱 복합재료층으로 구성되는 복합재료 구조.
  2. 제 1 항에 있어서, 상기 코어가 벌집 모양 형상을 가지는 구조.
  3. 제 1 항에 있어서, 상기 코어가 알루미늄인 구조.
  4. 제 1 항에 있어서, 상기 코어가 폴리아라미드 물질로 만들어지는 구조.
  5. 제 4 항에 있어서, 상기 물질이 고강도, 고온-내성 아라미드 구조인 구조.
  6. 제 1 항에 있어서, 상기 열가소성 플라스틱 복합재료층이 섬유 강화 폴리아릴렌 설피드 물질로 구성되는 구조.
  7. 제 6 항에 있어서, 상기 열가소성 플라스틱이 폴리페닐렌 설피드인 구조.
  8. 제 1 항에 있어서, 상기 복합재료층과 상기 코어 사이에 배치된 열가소성 플라스틱 필름을 포함함을 특징으로 하는 구조.
  9. 제 8 항에 있어서, 상기 필름이 폴리아릴렌 설피드 물질로 구성되는 구조.
  10. 제 9 항에 있어서, 상기 물질이 폴리페닐렌 설피드인 구조.
  11. 열가소성 플라스틱 수지로 구성되고, 하기 수단에 열적으로 결합된, 한쌍의 실질적으로 절취선이 없는 시트; 및 다수의 구획을 형성시키기 위한, 상기 시트사이에 배치된 수단으로 구성되는 복합재료 구조.
  12. 제 11 항에 있어서, 다수의 구획을 형성시키기 위한 상기 수단이 벌집모양 코어에 의해 특징지워지는 구조.
  13. 제 12 항에 있어서, 상기 코어가 금속인 구조.
  14. 제 12 항에 있어서, 상기 코어가 폴리아라미드 물질로 만들어지는 구조.
  15. 제 11 항에 있어서, 상기 수지가 폴리아릴렌 설피드인 구조.
  16. 제 11 항에 있어서, 상기 수지가 강화된 섬유인 구조.
  17. 제 16 항에 있어서, 열가소성 플라스틱 수지로 구성되고, 다수의 구획을 형성시키기 위한 상기 수단과 각각의 상기 시트 사이에 배치된 필름층을 포함함을 특징으로 하는 구조.
  18. 제 17 항에 있어서, 상기 필름 내 상기 열가소성 플라스틱 수지가 폴리페닐렌 설피드인 구조.
  19. 하기 단계로 구성되는 기포질 샌드위치 구조의 형성방법; 기포질 코어부분을 제공하고; 상기 코어 부분의 반대면에 인접한 강화 열가소성 플라스틱 시트를 놓으며; 및 상기 코어부분에 상기 열가소성 플라스틱 시트를 열적으로 결합시키기 위해 열을 적용한다.
  20. 제 19 항에 있어서, 상기 열 적용 단계 이전에, 적어도 하나의 상기 열가소성 플라스틱 시트와 상기 코어 부분사이에 열가소성 플라스틱 필름층을 놓는 단계를 포함함을 특징으로 하는 방법.
  21. 제 20 항에 있어서, 폴리페닐렌 설피드인 상기 필름 및 상기 시트내 상기 열가소성 플라스틱을 제공함을 포함함을 특징으로 하는 방법.
  22. 제 20 항에 있어서, 상기 코어 부분의 실질적으로 연속적인 형태로 제공되고; 필름의 상기 층이 상기 코어 부분상에 실질적으로 연속으로 제공되는 방법.
  23. 제 19 항에 있어서, 열적으로 결합시키기 위한 상기 열 적용 단계동안, 상기 시트에 압력을 적용하는 단계를 포함함을 특징으로 하는 방법.
  24. 제 19 항에 있어서, 상기 코어가 벌집 모양 구조 형태로 제공되는 방법.
  25. 제 19 항에 있어서, 상기 코어가 알루미늄 및 아라미드로 구성되는 군중에서 선택된 물질로부터 제공되는 방법.
  26. 제 19 항에 있어서, 상기 열가소성 플라스틱 시트가 섬유 강화 폴리페닐렌 설피드 물질의 형태로 제공되는 방법.
    ※ 참고사항 : 최초 출원 내용에 의하여 공개하는 것임.
KR1019900701558A 1989-05-30 1990-05-30 복합재료 기포질 샌드위치 구조 KR920700107A (ko)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US35908189A 1989-05-30 1989-05-30
US07/359.081 1989-05-30
PCT/US1990/003012 WO1990014943A1 (en) 1989-05-30 1990-05-30 Composite cellular sandwich structure

Publications (1)

Publication Number Publication Date
KR920700107A true KR920700107A (ko) 1992-02-19

Family

ID=23412230

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1019900701558A KR920700107A (ko) 1989-05-30 1990-05-30 복합재료 기포질 샌드위치 구조

Country Status (5)

Country Link
EP (1) EP0400599A3 (ko)
JP (1) JPH04500339A (ko)
KR (1) KR920700107A (ko)
CA (1) CA2017661A1 (ko)
WO (1) WO1990014943A1 (ko)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5328744A (en) * 1990-10-09 1994-07-12 E. I. Du Pont De Nemours And Company Panel having a core with thermoplastic resin facings
EP0562001A4 (en) * 1990-12-04 1993-10-20 Hexcel Corporation Process for the preparation of thermoplastic honeycomb sandwich structures
US5238725A (en) * 1990-12-21 1993-08-24 E. I. Du Pont De Nemours And Company Method for forming a structural panel with decorative facing and product thereof
AU650769B2 (en) * 1991-08-05 1994-06-30 3A Technology & Management Ltd. Process for the production of a composite sheet comprising a cellular core and at least one outer layer
ATE128070T1 (de) * 1991-09-14 1995-10-15 Eurocopter Deutschland Flächiger gegenstand mit wabenstruktur.
GB9127403D0 (en) * 1991-12-24 1992-02-19 Ncr Co Display and data entry device
FR2726785B1 (fr) * 1994-11-16 1996-12-13 Induplast Sa Procede de realisation d'un element sandwich a ame en nid abeilles
FR2739803B1 (fr) * 1995-10-12 1997-12-05 Induplast Sa Procede et dispositif de fabrication de structures sandwich a ame thermoplastique
IT1282098B1 (it) * 1996-01-29 1998-03-12 Roofing Italiana S R L Impianto automatico in continuo per il confezionamento di pannelli in tessuto di vetro e distanziali cellulari in leghe leggere
WO2000075451A1 (en) * 1999-06-04 2000-12-14 Owl Video Systems Limited Panel and panel system
GB0225937D0 (en) 2002-11-06 2002-12-11 Britax Aircraft Interiors Uk L Composite sheet material
US20120040131A1 (en) 2010-08-10 2012-02-16 Speer Dwaine D Composite Panel Having Perforated Foam Core
JP6022059B2 (ja) * 2013-06-10 2016-11-09 三菱電機株式会社 ハニカムサンドイッチ構造体およびハニカムサンドイッチ構造体の製造方法
US9662742B2 (en) 2013-07-09 2017-05-30 The Boeing Company Metallic bladders
US9469087B2 (en) 2013-07-09 2016-10-18 The Boeing Company Thermoplastic and titanium sandwich structures
US10029398B2 (en) 2013-07-09 2018-07-24 The Boeing Company Consolidation of complex contoured thermoplastic structures
US9358703B2 (en) 2013-07-09 2016-06-07 The Boeing Company Thermoplastic sandwich structures
US10618230B2 (en) 2013-07-09 2020-04-14 The Boeing Company Thermoplastic structures
JP6326739B2 (ja) * 2013-08-27 2018-05-23 王子ホールディングス株式会社 ハニカムサンドイッチ構造体及びハニカムサンドイッチ構造体の製造方法
JP6326738B2 (ja) * 2013-08-27 2018-05-23 王子ホールディングス株式会社 ハニカムサンドイッチ構造体及びハニカムサンドイッチ構造体の製造方法
EP3077195B1 (en) * 2013-12-06 2018-08-29 Continental Structural Plastics, Inc. Open area core with chopped fiber reinforced skin
FR3056936B1 (fr) 2016-10-03 2018-10-05 Airbus Operations Procede de fabrication d'un panneau acoustique renforce par au moins une couche en materiau composite thermoplastique
US11059259B2 (en) 2016-11-21 2021-07-13 Wabash National, L.P. Composite core with reinforced plastic strips and method thereof
WO2018140955A1 (en) 2017-01-30 2018-08-02 Wabash National, L.P. Composite core with reinforced areas and method
CA3053554A1 (en) 2017-02-14 2018-08-23 Wabash National, L.P. Hybrid composite panel and method
US11008051B2 (en) 2018-02-06 2021-05-18 Wabash National, L.P. Interlocking composite core and method
US11772715B2 (en) 2019-03-27 2023-10-03 Wabash National, L.P. Composite panel with connecting strip and method
CN110481053B (zh) * 2019-07-29 2021-07-09 安徽润象新材料科技有限公司 一种宽幅复合车厢板的制造设备及制造工艺
CN112647606B (zh) * 2021-01-08 2022-01-04 陈国新 一种高强度蜂巢状保温板及其制备方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1524796A (fr) * 1966-05-23 1968-05-10 Du Pont Structures nervurées en résine thermoplastique, leur procédé de fabrication et articles produits à partir de ces structures
US4157273A (en) * 1975-03-20 1979-06-05 Phillips Petroleum Company Bonding with a poly(arylene sulfide)-polytetrafluoroethylene adhesive
US4212923A (en) * 1975-03-20 1980-07-15 Phillips Petroleum Company Laminate using a poly(arylene sulfide)-polytetrafluoroethylene adhesive
US4032683A (en) * 1976-09-27 1977-06-28 Phillips Petroleum Company Structural member and method of making same
US4357013A (en) * 1981-07-31 1982-11-02 David Fernandez Reinforced foam core composite structure and method
US4557961A (en) * 1983-05-27 1985-12-10 The Boeing Company Light-weight, fire-retardant structural panel
US4496024A (en) * 1983-08-06 1985-01-29 Midwest-Acoust-A-Fiber, Inc. Sound absorption panel and method of making
CH663378A5 (en) * 1983-09-09 1987-12-15 Symalit Lizenz Ag Multilayer planar construction element and process and device for the production thereof
GB2188866B (en) * 1985-04-14 1990-03-14 H R Smith Lightweight high temperature thermoplastics material structures
US4716067A (en) * 1986-09-12 1987-12-29 The Boeing Company Honeycomb core structure with embedded fastener
DE3672220D1 (de) * 1986-10-22 1990-08-02 Schreiner Luchtvaart Sandwichaufbau und verfahren zu seiner herstellung.
NL8603228A (nl) * 1986-12-18 1988-07-18 Nijverdal Ten Cate Textiel Werkwijze voor het vervaardigen van een gelaagde constructie, en daarmee verkregen constructie.
DE3644676A1 (de) * 1986-12-30 1988-07-14 Schladitz Klaus Verfahren zur herstellung von leichtbauteilen

Also Published As

Publication number Publication date
WO1990014943A1 (en) 1990-12-13
EP0400599A2 (en) 1990-12-05
EP0400599A3 (en) 1991-07-03
JPH04500339A (ja) 1992-01-23
CA2017661A1 (en) 1990-11-30

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WITN Application deemed withdrawn, e.g. because no request for examination was filed or no examination fee was paid