DE69532193D1 - Wärmeleitfähige nichtmetallische wabenstrukturen und verfahren - Google Patents
Wärmeleitfähige nichtmetallische wabenstrukturen und verfahrenInfo
- Publication number
- DE69532193D1 DE69532193D1 DE69532193T DE69532193T DE69532193D1 DE 69532193 D1 DE69532193 D1 DE 69532193D1 DE 69532193 T DE69532193 T DE 69532193T DE 69532193 T DE69532193 T DE 69532193T DE 69532193 D1 DE69532193 D1 DE 69532193D1
- Authority
- DE
- Germany
- Prior art keywords
- thermally conductive
- heat
- resistant non
- wave structures
- metal wave
- Prior art date
- Legal status (The legal status 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 status listed.)
- Expired - Lifetime
Links
- 229910052755 nonmetal Inorganic materials 0.000 title 1
- 150000002843 nonmetals Chemical class 0.000 title 1
- 239000000835 fiber Substances 0.000 abstract 4
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
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
-
- 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
- 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
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0012—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular thermal properties
- B29K2995/0013—Conductive
-
- 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
- B29L2031/60—Multitubular or multicompartmented articles, e.g. honeycomb
- B29L2031/608—Honeycomb structures
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/902—High modulus filament or fiber
-
- 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
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24149—Honeycomb-like
-
- 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
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24149—Honeycomb-like
- Y10T428/24165—Hexagonally shaped cavities
-
- 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
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2918—Rod, strand, filament or fiber including free carbon or carbide or therewith [not as steel]
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Laminated Bodies (AREA)
- Ceramic Products (AREA)
- Conductive Materials (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US221833 | 1994-04-01 | ||
US08/221,833 US5498462A (en) | 1994-04-01 | 1994-04-01 | High thermal conductivity non-metallic honeycomb |
PCT/US1995/003951 WO1995026877A1 (en) | 1994-04-01 | 1995-03-31 | Thermally conductive non-metallic honeycomb and process |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69532193D1 true DE69532193D1 (de) | 2004-01-08 |
DE69532193T2 DE69532193T2 (de) | 2004-11-25 |
Family
ID=22829594
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69532193T Expired - Lifetime DE69532193T2 (de) | 1994-04-01 | 1995-03-31 | Wärmeleitfähige nichtmetallische wabenstrukturen und verfahren |
Country Status (8)
Country | Link |
---|---|
US (1) | US5498462A (de) |
EP (1) | EP0754121B1 (de) |
JP (1) | JP2863636B2 (de) |
AT (1) | ATE255001T1 (de) |
AU (1) | AU2233695A (de) |
DE (1) | DE69532193T2 (de) |
ES (1) | ES2207647T3 (de) |
WO (1) | WO1995026877A1 (de) |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH06173772A (ja) * | 1992-08-10 | 1994-06-21 | Boeing Co:The | 逆推進装置内壁およびそのサンドイッチ構造 |
US5769153A (en) * | 1996-11-07 | 1998-06-23 | The United States Of America As Represented By The Secretary Of The Navy | Method and apparatus for casting thin-walled honeycomb structures |
US5975237A (en) * | 1997-07-30 | 1999-11-02 | The Boeing Company | Reinforcing structure for engine nacelle acoustic panel |
US6129311A (en) * | 1997-07-30 | 2000-10-10 | The Boeing Company | Engine nacelle outer cowl panel with integral track fairings |
US6173807B1 (en) | 1998-04-13 | 2001-01-16 | The Boeing Company | Engine nacelle acoustic panel with integral wedge fairings and an integral forward ring |
US6179943B1 (en) | 1997-07-30 | 2001-01-30 | The Boeing Company | Method for forming a composite acoustic panel |
US6153687A (en) * | 1999-04-27 | 2000-11-28 | Hexcel Corporation | Honeycomb dip resin |
US6245407B1 (en) | 1999-04-27 | 2001-06-12 | Hexcel Corporation | Thermoformable honeycomb structures |
US6592963B1 (en) * | 2000-06-16 | 2003-07-15 | E. I. Du Pont De Nemours And Company | Honeycomb structure |
US7033663B1 (en) * | 2000-06-27 | 2006-04-25 | Eaton Corporation | Functionally graded friction material |
US6910996B1 (en) * | 2002-09-27 | 2005-06-28 | Nicholas John Patz | Method for producing a honeycomb structure and apparatus therefor |
US7185468B2 (en) | 2002-10-31 | 2007-03-06 | Jeld-Wen, Inc. | Multi-layered fire door and method for making the same |
US20040141815A1 (en) * | 2002-11-01 | 2004-07-22 | Jeff Moreau | Fiber re-enforcement of joints and corners of composite sheet piling segments |
US20070110979A1 (en) * | 2004-04-21 | 2007-05-17 | Jeld-Wen, Inc. | Fiber-reinforced composite fire door |
JP2007534865A (ja) * | 2004-04-21 | 2007-11-29 | ジェルドウィン インコーポレイテッド | 繊維強化複合体、及び繊維強化複合体を含む建築用構造物 |
DE102005012146B4 (de) * | 2005-03-16 | 2007-04-05 | Aco Severin Ahlmann Gmbh & Co. Kg | Rinnenkörper und Rinnensystem mit einem derartigen Rinnenkörper |
US7328508B2 (en) * | 2005-07-05 | 2008-02-12 | International Business Machines Corporation | Anisotropic heat spreading apparatus and method for semiconductor devices |
US20080034693A1 (en) * | 2006-08-10 | 2008-02-14 | Moore Michael T | Wallboard panel |
DE102007035851A1 (de) * | 2007-01-13 | 2008-08-14 | Vacuum Walls Ag | Vakuum-Isolationspaneel und Herstellungsverfahren dafür |
US20090175006A1 (en) * | 2008-01-09 | 2009-07-09 | Rong-Yuan Jou | Honeycomb heat dissipating apparatus |
US8671693B2 (en) * | 2008-01-11 | 2014-03-18 | George C. P. Straza | Thermally conductive structure |
US8043690B2 (en) | 2008-04-21 | 2011-10-25 | The Boeing Company | Exhaust washed structure and associated composite structure and method of fabrication |
DE102008062678B4 (de) * | 2008-12-17 | 2011-05-12 | Daimler Ag | Verbundbauteil mit einer Wabenstruktur |
US20100192590A1 (en) * | 2009-01-30 | 2010-08-05 | Michael Robert Johnson | Thermally balanced materials |
US20100193605A1 (en) * | 2009-01-30 | 2010-08-05 | Michael Robert Johnson | Thermally balanced aero structures |
EP2475519B8 (de) * | 2009-09-09 | 2015-04-22 | Megtec Turbosonic Inc. | Anordnung aus elektronischen nassfiltern |
JP5574835B2 (ja) * | 2010-06-14 | 2014-08-20 | 三菱電機株式会社 | ハニカムコアサンドイッチ構造体 |
JP6089026B2 (ja) | 2011-03-28 | 2017-03-01 | メグテック ターボソニック インコーポレイテッドMegtec Turbosonic Inc. | 湿式電気集塵機用の耐浸食性導電性複合材料集塵電極 |
US11027289B2 (en) | 2011-12-09 | 2021-06-08 | Durr Systems Inc. | Wet electrostatic precipitator system components |
JP2017001901A (ja) * | 2015-06-05 | 2017-01-05 | 株式会社デンソー | 炭化物接合体及びその製造方法 |
US10697470B2 (en) | 2016-02-15 | 2020-06-30 | General Electric Company | Containment case trench filler layer and method of containing releasable components from rotatable machines |
US11274184B2 (en) * | 2016-04-12 | 2022-03-15 | Trillium Marketing Inc. | Bi-polymer thermoplastic |
NL2016945B1 (en) * | 2016-06-10 | 2018-01-24 | Lantor Bv | Flexible core for machine processing or production of composite parts or materials |
KR20190089880A (ko) | 2016-10-27 | 2019-07-31 | 루아그 슈바이쯔 아게 | 섬유 보강 중합체 제조방법 |
US10695986B2 (en) | 2017-08-22 | 2020-06-30 | Rohr, Inc. | Method for forming a structural panel |
US10906659B2 (en) | 2018-04-03 | 2021-02-02 | Rohr, Inc. | Structured panel with structural reinforcement(s) |
US11040765B2 (en) * | 2018-06-27 | 2021-06-22 | Goodrich Corporation | Advanced composite heated floor panel |
US11242822B2 (en) | 2018-12-14 | 2022-02-08 | Rohr, Inc. | Structured panel with multi-panel structure(s) |
US11398214B2 (en) * | 2018-12-14 | 2022-07-26 | Rohr, Inc. | Forming a structured panel with one or more structural reinforcements |
GB2593957B (en) * | 2020-11-06 | 2022-05-11 | Corridoor Ltd | Structure formation apparatus, method and structure |
FR3126920A1 (fr) * | 2022-03-10 | 2023-03-17 | Airbus Operations | Structure en nid d’abeilles présentant une conductivité thermique améliorée |
FR3133338B1 (fr) * | 2022-03-10 | 2024-06-21 | Airbus Operations Sas | Structure en nid d’abeilles présentant une conductivité thermique améliorée |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3404748A (en) * | 1967-12-06 | 1968-10-08 | Griffolyn Company Inc | Insulation laminate with reinforcing fibers and corrugated layer |
US4204016A (en) * | 1975-07-25 | 1980-05-20 | Chavannes Marc A | Reinforced paper products |
US4409274A (en) * | 1982-02-24 | 1983-10-11 | Westvaco Corporation | Composite material |
US4440819A (en) * | 1982-12-27 | 1984-04-03 | Hughes Aircraft Company | Interconnection of unidirectional fiber arrays with random fiber networks |
US4504343A (en) * | 1983-05-16 | 1985-03-12 | Composite Technology, Inc. | Method of making composite member with transverse fibers |
US4568593A (en) * | 1983-05-16 | 1986-02-04 | Composite Technology, Inc. | Composite corrugated panel with transverse fibers |
JPS60252718A (ja) * | 1984-05-23 | 1985-12-13 | Mitsubishi Rayon Co Ltd | 高性能複合材料の中間体 |
US4628001A (en) * | 1984-06-20 | 1986-12-09 | Teijin Limited | Pitch-based carbon or graphite fiber and process for preparation thereof |
JPS6397635A (ja) * | 1986-10-14 | 1988-04-28 | Ube Ind Ltd | インタ−リ−フを有する繊維強化エポキシ樹脂プリプレグ |
DE3872911T2 (de) * | 1987-03-31 | 1992-12-03 | Asahi Chemical Ind | Gewebe mit mehrschichtenaufbau und ein derartiges gewebe enthaltender verbundwerkstoff. |
DE3838153A1 (de) * | 1988-11-10 | 1990-05-31 | Schuetz Werke Gmbh Co Kg | Leichtbauwerkstoff sowie verfahren und anlage zur herstellung von wabenstrukturen aus dem leichtbauwerkstoff |
DE3913602A1 (de) * | 1989-04-25 | 1990-10-31 | Dornier Gmbh Lindauer | Greiferstange aus faserverstaerkten kunststoffbaendern |
US5131970A (en) * | 1990-03-02 | 1992-07-21 | Northrop Corporation | Block-bonded process for producing thermoplastic resin impregnated fiber honeycomb core |
US5139596A (en) * | 1990-05-31 | 1992-08-18 | Basf Structural Materials, Inc. | Continuous process for the preparation of thermoplastic honeycomb |
JPH04113832A (ja) * | 1990-09-04 | 1992-04-15 | Mitsubishi Rayon Co Ltd | ハニカムコアーの構造 |
US5567500A (en) * | 1991-08-07 | 1996-10-22 | Speciality Cellular Products Company | Composite honeycomb core structure comprising cell walls constructed of at least three unidirectional fiber layers or at least two unidirectional fiber layers and a random fiber layer |
US5288537A (en) * | 1992-03-19 | 1994-02-22 | Hexcel Corporation | High thermal conductivity non-metallic honeycomb |
JPH06173772A (ja) * | 1992-08-10 | 1994-06-21 | Boeing Co:The | 逆推進装置内壁およびそのサンドイッチ構造 |
-
1994
- 1994-04-01 US US08/221,833 patent/US5498462A/en not_active Expired - Lifetime
-
1995
- 1995-03-31 EP EP95915463A patent/EP0754121B1/de not_active Expired - Lifetime
- 1995-03-31 WO PCT/US1995/003951 patent/WO1995026877A1/en active IP Right Grant
- 1995-03-31 AT AT95915463T patent/ATE255001T1/de not_active IP Right Cessation
- 1995-03-31 ES ES95915463T patent/ES2207647T3/es not_active Expired - Lifetime
- 1995-03-31 AU AU22336/95A patent/AU2233695A/en not_active Abandoned
- 1995-03-31 JP JP7525835A patent/JP2863636B2/ja not_active Expired - Lifetime
- 1995-03-31 DE DE69532193T patent/DE69532193T2/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP0754121A4 (de) | 1997-07-09 |
ATE255001T1 (de) | 2003-12-15 |
AU2233695A (en) | 1995-10-23 |
DE69532193T2 (de) | 2004-11-25 |
JPH09507443A (ja) | 1997-07-29 |
JP2863636B2 (ja) | 1999-03-03 |
US5498462A (en) | 1996-03-12 |
ES2207647T3 (es) | 2004-06-01 |
WO1995026877A1 (en) | 1995-10-12 |
EP0754121A1 (de) | 1997-01-22 |
EP0754121B1 (de) | 2003-11-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8327 | Change in the person/name/address of the patent owner |
Owner name: HEXCEL CORPORATION, DUBLIN, CALIF., US |
|
8364 | No opposition during term of opposition |