DE69529396D1 - Transfer-Giessverfahren in Kombination mit wabenförmigen Kern - Google Patents

Transfer-Giessverfahren in Kombination mit wabenförmigen Kern

Info

Publication number
DE69529396D1
DE69529396D1 DE69529396T DE69529396T DE69529396D1 DE 69529396 D1 DE69529396 D1 DE 69529396D1 DE 69529396 T DE69529396 T DE 69529396T DE 69529396 T DE69529396 T DE 69529396T DE 69529396 D1 DE69529396 D1 DE 69529396D1
Authority
DE
Germany
Prior art keywords
combination
casting process
honeycomb core
transfer casting
transfer
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
Application number
DE69529396T
Other languages
English (en)
Other versions
DE69529396T2 (de
Inventor
Thomas R Cundiff
Bradley A Frye
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
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
Application granted granted Critical
Publication of DE69529396D1 publication Critical patent/DE69529396D1/de
Publication of DE69529396T2 publication Critical patent/DE69529396T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products 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 form; Layered products 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 form; Layered products 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
    • 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
    • B29C70/086—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 and with one or more layers of pure plastics material, e.g. foam layers
    • 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
    • B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • 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
    • B29C70/542—Placing or positioning the reinforcement in a covering or packaging element before or during moulding, e.g. drawing in a sleeve
    • 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
    • B29D24/00—Producing articles with hollow walls
    • B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
    • B29D24/005—Producing 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
    • 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
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • 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
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • 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
    • B29L2007/00—Flat articles, e.g. films or sheets
    • B29L2007/002—Panels; Plates; Sheets
    • 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
    • B32B38/00—Ancillary operations in connection with laminating processes
    • B32B2038/0052—Other operations not otherwise provided for
    • B32B2038/0076—Curing, vulcanising, cross-linking
    • 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
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02—Composition of the impregnated, bonded or embedded layer
    • B32B2260/021—Fibrous or filamentary layer
    • 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
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04—Impregnation, embedding, or binder material
    • B32B2260/046—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
    • 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
    • B32B2605/00—Vehicles
    • B32B2605/18—Aircraft
    • 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
    • Y10T428/23—Sheet including cover or casing
    • Y10T428/233—Foamed or expanded material encased
    • 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
    • Y10T428/23—Sheet including cover or casing
    • Y10T428/234—Sheet including cover or casing including elements cooperating to form cells
    • Y10T428/236—Honeycomb type cells extend perpendicularly to nonthickness layer
    • 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
    • Y10T428/23—Sheet including cover or casing
    • Y10T428/239—Complete cover or casing
    • 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.]
    • Y10T428/24628—Nonplanar uniform thickness material
    • Y10T428/24661—Forming, or cooperating to form cells
DE69529396T 1995-01-03 1995-10-30 Transfer-Giessverfahren in Kombination mit wabenförmigen Kern Expired - Lifetime DE69529396T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/368,062 US5567499A (en) 1995-01-03 1995-01-03 Resin transfer molding in combination with honeycomb core

Publications (2)

Publication Number Publication Date
DE69529396D1 true DE69529396D1 (de) 2003-02-20
DE69529396T2 DE69529396T2 (de) 2003-05-15

Family

ID=23449724

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69529396T Expired - Lifetime DE69529396T2 (de) 1995-01-03 1995-10-30 Transfer-Giessverfahren in Kombination mit wabenförmigen Kern

Country Status (3)

Country Link
US (2) US5567499A (de)
EP (1) EP0722825B1 (de)
DE (1) DE69529396T2 (de)

Families Citing this family (82)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5698266A (en) * 1993-04-05 1997-12-16 Commissariat A L'energie Atomique Process for the production of thin coatings having optical and abrasion resistance properties
FR2740383B1 (fr) * 1995-10-27 1998-01-16 Aerospatiale Procede de fabrication d'un panneau en materiau composite avec moulage par transfert de resine
CA2195050A1 (en) * 1996-01-29 1997-07-30 Mark David Thiede-Smet Low-weight and water-resistant honeycomb sandwich panels made by resin transfer molding process
US5848767A (en) * 1996-08-05 1998-12-15 The Boeing Company One piece spacecraft frame
EP0929607B1 (de) * 1996-09-20 2003-12-10 Vantico GmbH Verfahren zum transfer-spritzgiessen von stabilen epoxidharzzusammensetzungen
FR2764525B1 (fr) 1997-06-13 1999-07-23 Commissariat Energie Atomique Fixation ou separation d'ions, notamment de pb, par des derives de per (3,6 anhydro) cyclodextrines
JP4342620B2 (ja) * 1998-12-02 2009-10-14 富士重工業株式会社 ハニカムサンドイッチ構造複合材パネルの成形方法
DE19915083C1 (de) * 1999-04-01 2000-04-13 Daimler Chrysler Ag Verfahren zur Herstellung faserverstärkter Kunststoffbauteile mit nicht-vollständig abwickelbarer Geometrie
US6227606B1 (en) 1999-09-09 2001-05-08 Daimlerchrysler Corporation Engine hood assembly
US6834159B1 (en) 1999-09-10 2004-12-21 Goodrich Corporation Aircraft heated floor panel
FR2798618B1 (fr) * 1999-09-21 2002-05-03 Aerospatiale Matra Airbus Procede de fabrication d'un panneau sandwich en materiau composite, et panneau ainsi obtenu
US6367406B1 (en) * 1999-09-24 2002-04-09 Larson/Glastron Boats, Inc. Boat and method for manufacturing using resin transfer molding
DE10007373C1 (de) * 2000-02-18 2000-11-23 Daimler Chrysler Aerospace Verfahren zur Herstellung von Sandwichbauteilen
US6893733B2 (en) 2000-07-07 2005-05-17 Delphi Technologies, Inc. Modified contoured crushable structural members and methods for making the same
US6586110B1 (en) 2000-07-07 2003-07-01 Delphi Technologies, Inc. Contoured metal structural members and methods for making the same
US7226559B2 (en) * 2000-12-08 2007-06-05 Toyota Motor Sales, U.S.A., Inc. Method for molding structures
US6557702B1 (en) * 2001-10-31 2003-05-06 Skb Corporation Golf club travel bag
US6638466B1 (en) 2000-12-28 2003-10-28 Raytheon Aircraft Company Methods of manufacturing separable structures
US7138028B2 (en) * 2001-07-26 2006-11-21 The Boeing Company Vacuum assisted resin transfer method for co-bonding composite laminate structures
US20030019567A1 (en) * 2001-07-26 2003-01-30 Burpo Steven J. Vacuum assisted resin transfer method for co-bonding composite laminate structures
JP4663174B2 (ja) * 2001-08-03 2011-03-30 富士重工業株式会社 ハニカムサンドイッチ構造複合材の成形方法
US6890401B2 (en) 2001-10-30 2005-05-10 The Boeing Company Liquid molded hollow cell core composite articles
US6780488B2 (en) 2001-10-30 2004-08-24 The Boeing Company Liquid molded hollow cell core composite articles
DE60220620T2 (de) * 2001-10-30 2008-02-14 The Boeing Co., Chicago Holzzellenkern-Verbundwerkstoffgegenstände und Verfahren zu deren Herstellung
DK176335B1 (da) * 2001-11-13 2007-08-20 Siemens Wind Power As Fremgangsmåde til fremstilling af vindmöllevinger
US6884055B2 (en) * 2002-05-29 2005-04-26 The Boeing Company Potting compound injection apparatus and method of injecting potting compound into panel cells
US20050042961A1 (en) * 2003-08-18 2005-02-24 Henkel Loctite Corporation Curable compositions for advanced processes, and products made therefrom
US7294220B2 (en) * 2003-10-16 2007-11-13 Toyota Motor Sales, U.S.A., Inc. Methods of stabilizing and/or sealing core material and stabilized and/or sealed core material
DE10358295B4 (de) * 2003-10-17 2009-11-26 Euro-Composites S.A. Leichtbau-Verbundmaterial sowie Verfahren zu dessen Herstellung
DE10354106B4 (de) * 2003-11-19 2013-09-26 Bayerische Motoren Werke Aktiengesellschaft Verfahren zum Herstellen einer Faserverbundstruktur
US20050123717A1 (en) * 2003-12-08 2005-06-09 Shen Shyan B. Sealing of honeycomb core and the honeycomb core assembly made with the same
FR2863933B1 (fr) * 2003-12-17 2007-05-11 Saint Gobain Vetrotex Procede de fabrication d'une piece composite par moulage
US20050133956A1 (en) * 2003-12-23 2005-06-23 Beauchamp Walter A. Resin formulation
US7284726B2 (en) * 2004-02-17 2007-10-23 Sikorsky Aircraft Corporation Self extinguishing composite primary structure
US7649060B2 (en) * 2005-12-02 2010-01-19 Henkel Corporation Curable compositions
US8029889B1 (en) 2004-12-03 2011-10-04 Henkel Corporation Prepregs, towpregs and preforms
US20060134408A1 (en) * 2004-12-20 2006-06-22 Mitsubishi Rayon Co., Ltd. Process for producing sandwich structure and adhesive film therefor
US20060138279A1 (en) * 2004-12-23 2006-06-29 Nathan Pisarski Aircraft floor panel
JP2008529849A (ja) 2005-02-21 2008-08-07 エアバス・ドイチュラント・ゲーエムベーハー 繊維複合材料構造要素および繊維複合材料構造要素を製造する方法
DE102005008252B4 (de) * 2005-02-21 2014-03-20 Airbus Operations Gmbh Verfahren zur Herstellung eines Faserverbund-Bauelements
US7837147B2 (en) 2005-03-18 2010-11-23 The Boeing Company Systems and methods for reducing noise in aircraft fuselages and other structures
DE102005048156B9 (de) * 2005-10-06 2010-08-12 Dorma Gmbh + Co. Kg Mobile Trennwand
US8371526B2 (en) * 2006-01-12 2013-02-12 Goodrich Corporation Aircraft heater floor panel
DE102006044842A1 (de) * 2006-02-07 2007-08-16 Grob, Margret Flugzeugbauteil sowie Verfahren zur Herstellung eines Flugzeugbauteiles
ES2298034B1 (es) * 2006-05-12 2009-02-01 Jesus Fco. Barberan Latorre Sistema de fabricacion de paneles con nido de abeja.
JP2010510110A (ja) * 2006-11-21 2010-04-02 ヘンケル コーポレイション 最新方法で使用するための強化バインダー組成物
US7537827B1 (en) 2006-12-13 2009-05-26 Henkel Corporation Prepreg laminates
WO2008089334A2 (en) 2007-01-19 2008-07-24 Vec Industries, L.L.C. Method and apparatus for molding composite articles
US9511571B2 (en) * 2007-01-23 2016-12-06 The Boeing Company Composite laminate having a damping interlayer and method of making the same
US20100065686A1 (en) * 2008-04-28 2010-03-18 Tauscher Kurt M Aircraft heated floor panel
JP5546551B2 (ja) 2008-11-21 2014-07-09 ヘンケル コーポレイション 熱分解性ポリマー被覆金属粉末
US8425710B2 (en) * 2009-03-13 2013-04-23 The Boeing Company Automated placement of vibration damping materials
US8167245B1 (en) * 2009-11-03 2012-05-01 The Boeing Company Fuel barrier
JP6253979B2 (ja) 2010-04-13 2017-12-27 ヘンケル アイピー アンド ホールディング ゲゼルシャフト ミット ベシュレンクテル ハフツング 硬化性組成物、複合材製造のための前記組成物の使用プロセス、ならびに優れた表面仕上げおよび高い繊維固着を有する複合材の製造プロセス
US8628717B2 (en) 2010-06-25 2014-01-14 The Boeing Company Composite structures having integrated stiffeners and method of making the same
US9682514B2 (en) 2010-06-25 2017-06-20 The Boeing Company Method of manufacturing resin infused composite parts using a perforated caul sheet
US8940213B2 (en) 2010-06-25 2015-01-27 The Boeing Company Resin infusion of composite parts using a perforated caul sheet
US8636252B2 (en) 2010-06-25 2014-01-28 The Boeing Company Composite structures having integrated stiffeners with smooth runouts and method of making the same
JP5927183B2 (ja) * 2010-07-02 2016-06-01 ヘクセル ホールディング ゲーエムベーハー 繊維強化複合成形品
US9682447B2 (en) 2010-08-20 2017-06-20 Henkel IP & Holding GmbH Organic acid- or latent organic acid-functionalized polymer-coated metal powders for solder pastes
CN102173113B (zh) * 2010-12-13 2014-05-14 中国航空工业集团公司北京航空材料研究院 一种适用于液态成型工艺改善泡沫与织物粘接质量的方法
US20130221555A1 (en) * 2011-08-26 2013-08-29 Basf Se Process for producing moldings
EP2753442B1 (de) 2011-09-06 2019-10-30 Henkel IP & Holding GmbH Mit di- oder poly-funktionalen olefinen mit elektronenmangel überzogenes metallpulver für lötpasten
CN103857731B (zh) * 2011-09-30 2017-06-13 株式会社斯巴鲁 纤维强化树脂复合材料及其制造方法
WO2013050074A1 (de) 2011-10-05 2013-04-11 Basf Se Verfahren zur herstellung von faserverstärkten verbundwerkstoffen
EP3282067A3 (de) 2012-08-21 2018-07-18 Milwaukee Composites, Inc. Fussbodenanordnung mit wärmeabstrahlungsschicht
EP3024642B1 (de) 2013-07-26 2020-04-22 Learjet Inc. Verbundwerkstoff mit einer wassereintrittsbarriere
CN103862764B (zh) * 2013-12-23 2017-01-25 中航复合材料有限责任公司 一种用液态成型工艺制备蜂窝夹层结构复合材料的方法
DE102014221037A1 (de) * 2014-10-16 2016-04-21 Robert Bosch Gmbh MEMS-Mikrofonbauelement
CN105128360B (zh) * 2015-07-30 2017-12-12 苏州格拉菲英新能源科技有限公司 一种柔性无机纤维纸及其制备方法
US9845596B2 (en) * 2015-09-29 2017-12-19 Awi Licensing Llc Ceiling system
CN105235233B (zh) * 2015-10-12 2018-01-23 湖北三江航天红阳机电有限公司 一种蜂窝夹层结构透气通道设计制作方法
DE102016102451A1 (de) * 2016-02-12 2017-08-17 Aguti Produktentwicklung & Design Gmbh Dreheinheit für eine Drehvorrichtung für einen Fahrzeugsitz
DE102016117103A1 (de) 2016-09-12 2018-03-15 Airbus Operations Gmbh Verfahren zur Herstellung eines Faserverbundbauteils
US10800129B2 (en) 2017-01-24 2020-10-13 Bell Textron Inc. Honeycomb core sandwich panels
US10392097B2 (en) * 2017-02-16 2019-08-27 The Boeing Company Efficient sub-structures
CN108045002A (zh) * 2018-01-02 2018-05-18 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种蜂窝夹层结构及其制备方法
CN110281603B (zh) * 2018-03-15 2021-10-08 杜邦安全与建筑公司 具有蜂窝芯的复合层合板及其制造方法
WO2019177662A1 (en) 2018-03-15 2019-09-19 E. I. Du Pont De Nemours And Company A composite laminate having a honeycomb core, and method for the manufacture thereof
FR3083735B1 (fr) * 2018-07-10 2020-09-11 Safran Nacelles Procede de fabrication d’un panneau composite
JP6840277B1 (ja) * 2020-02-25 2021-03-10 株式会社すぎはら 積層板の製造方法
CN113635612B (zh) * 2021-07-30 2023-05-23 中国航空工业集团公司济南特种结构研究所 一种大尺寸耐高温蜂窝的制备方法

Family Cites Families (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2227212A (en) * 1938-07-23 1940-12-31 Catalin Corp Laminated material and method of manufacture
GB785595A (en) * 1952-10-11 1957-10-30 Eugen Johann Ritter Process for the manufacture of composite sheets or shaped members having covering layers impregnated with synthetic resin
US2839442A (en) * 1955-02-23 1958-06-17 Smith Corp A O Process of making a lightweight structural panel
US3655818A (en) * 1968-10-18 1972-04-11 Minnesota Mining & Mfg Particulate adhesive containing polyepoxides carboxylated butadiene-acrylonitrile copolymer and a urea derivative as a curing agent
GB1273771A (en) * 1969-02-28 1972-05-10 Ciba Geigy Uk Ltd Improvements in or relating to cellular core structures
US3622430A (en) * 1969-11-24 1971-11-23 Peter L Jurisich Dimpled sheet structural laminate
US3857217A (en) * 1972-11-15 1974-12-31 W Reps Lightweight, rigid structural panel for walls, ceilings and the like
US4162341A (en) * 1974-08-26 1979-07-24 Suntech, Inc. Honeycomb insulation structure
US4089328A (en) * 1976-11-02 1978-05-16 Futurumverken Ab Kitchen ventilator
JPS55173691U (de) * 1979-05-31 1980-12-12
US4353947A (en) * 1981-10-05 1982-10-12 International Harvester Co. Laminated composite structure and method of manufacture
US4622091A (en) * 1984-11-29 1986-11-11 The Boeing Company Resin film infusion process and apparatus
US4765942A (en) * 1986-09-30 1988-08-23 The Boeing Company Method of consolidating thermoplastic poly(amide-imide) components
DE3720371A1 (de) * 1987-06-19 1989-01-05 Messerschmitt Boelkow Blohm Leichtbauverbundplatte und verfahren zu deren herstellung
JPS6471935A (en) * 1987-09-08 1989-03-16 Inax Corp Self-purifying toilet stool
JPH01171935A (ja) * 1987-12-28 1989-07-06 Toyota Motor Corp ハニカムサンドイッチ構造体の製造方法
US5061418A (en) * 1988-01-22 1991-10-29 Tertm, Inc. Thermal expansion resin transfer molding
US5089328A (en) * 1988-02-26 1992-02-18 Van Dresser Corporation Panel and method of making the same
JP2573670B2 (ja) * 1988-08-24 1997-01-22 日東電工株式会社 スパイラル型膜分離装置
US4879152A (en) * 1989-02-15 1989-11-07 Green Patrick H Composite panel structure
NL8900398A (nl) * 1989-02-17 1990-09-17 Schreiner Luchtvaart Werkwijze voor het aanbrengen van een plaatselijke versterking in een sandwichconstructie.
DE4004599A1 (de) * 1990-02-15 1991-08-22 Basf Ag Laminate mit stabilen befestigungsstellen
JPH0832817B2 (ja) * 1990-08-17 1996-03-29 東邦レーヨン株式会社 低発煙性フェノール樹脂系プリプレグ及びその製造法
JPH07121567B2 (ja) * 1990-12-26 1995-12-25 日本特殊塗料株式会社 深絞り可能な軽量防音材
US5234757A (en) * 1991-04-30 1993-08-10 The Dexter Corporation Expandable films and molded products therefrom
DE4200572C2 (de) * 1992-01-11 1994-05-26 Dornier Luftfahrt Verfahren zur Herstellung von regenerosionsgeschützten Radomen
US5338594A (en) * 1992-02-07 1994-08-16 Hexcel Corporation Foam filled honeycomb and methods for their production
US5445861A (en) * 1992-09-04 1995-08-29 The Boeing Company Lightweight honeycomb panel structure

Also Published As

Publication number Publication date
US5567499A (en) 1996-10-22
EP0722825A2 (de) 1996-07-24
DE69529396T2 (de) 2003-05-15
EP0722825B1 (de) 2003-01-15
EP0722825A3 (de) 1997-01-15
US5851336A (en) 1998-12-22

Similar Documents

Publication Publication Date Title
DE69529396T2 (de) Transfer-Giessverfahren in Kombination mit wabenförmigen Kern
DE69531443D1 (de) Transfer-Giessverfahren mit gefülltem wabenförmigem Kern
DE69510417D1 (de) Verbundwerkstoff mit schaumfähigem kern
DE69524295D1 (de) Intelligentes Drucksystem
PT968820E (pt) Impressao flexografica selectiva
BR9509031A (pt) Microestruturas em disposiçao cruzada
ITMI950223A0 (it) Gruppo stampi
DE69504242D1 (de) Giessverfahren mit verbessertem Kernauszug, Kern und System dafür
NO20000057D0 (no) Kjerneroer
DE69512791D1 (de) Filter mit konzentrischen kern
KR950026224U (ko) 조립식 부력체 구조물
KR950033885U (ko) 조립식 온돌
KR950032098U (ko) 조립식 베개
DE69517508T2 (de) Wabenkernstruktur
KR970008447U (ko) 프린터에서의 양면인쇄장치
FI1691U1 (fi) Hopsaettningsmaskin foer lastpallsben
KR950032489U (ko) 금형 구조체
BR7200639U (pt) Disposicao construtiva em cambio
KR970024940U (ko) 라디에이터 코어
BR7402231U (pt) Aperfeiçoamento em broqueiro
DE9401615U1 (de) Astroleuchte mit Maßgravuren
SE9203545D0 (sv) Transmission, i synnerhet fordonsvaexellaada
BR9404535A (pt) Aperfeiçoameto em emolduramento
BR9301851A (pt) Aperfeiçoamentos em lajes pré-moldadas.
SE9502774D0 (sv) Device in printers

Legal Events

Date Code Title Description
8364 No opposition during term of opposition