DE69329078D1 - Verfahren zur Herstellung eines wabenförmigen Kernes mit einer niedrigen Dichte und mit schrägen Oberflächen für einen Verbundkörper - Google Patents

Verfahren zur Herstellung eines wabenförmigen Kernes mit einer niedrigen Dichte und mit schrägen Oberflächen für einen Verbundkörper

Info

Publication number
DE69329078D1
DE69329078D1 DE69329078T DE69329078T DE69329078D1 DE 69329078 D1 DE69329078 D1 DE 69329078D1 DE 69329078 T DE69329078 T DE 69329078T DE 69329078 T DE69329078 T DE 69329078T DE 69329078 D1 DE69329078 D1 DE 69329078D1
Authority
DE
Germany
Prior art keywords
producing
low density
inclined surfaces
honeycomb core
composite body
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
DE69329078T
Other languages
English (en)
Other versions
DE69329078T2 (de
Inventor
Alexander C Dublinski
Thomas A Carstensen
Philip J Ramey
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of DE69329078D1 publication Critical patent/DE69329078D1/de
Publication of DE69329078T2 publication Critical patent/DE69329078T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0089Producing honeycomb structures
    • 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
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/38Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
    • 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
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/76Cores
    • 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
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32Component parts, details or accessories; Auxiliary operations
    • B29C43/36Moulds for making articles of definite length, i.e. discrete articles
    • B29C43/3642Bags, bleeder sheets or cauls for isostatic pressing
    • 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
    • B29C70/06Fibrous reinforcements only
    • B29C70/08Fibrous 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
    • B29C70/086Fibrous 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
    • 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
    • B29C70/549Details of caul plates, e.g. materials or shape
    • 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
    • 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
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32Component parts, details or accessories; Auxiliary operations
    • B29C43/36Moulds for making articles of definite length, i.e. discrete articles
    • B29C43/3642Bags, bleeder sheets or cauls for isostatic pressing
    • B29C2043/3644Vacuum bags; Details thereof, e.g. fixing or clamping
    • 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
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/38Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
    • B29C33/40Plastics, e.g. foam or rubber
    • B29C33/405Elastomers, e.g. rubber
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2705/00Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
    • B29K2705/02Aluminium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2827/00Use of polyvinylhalogenides or derivatives thereof as mould material
    • B29K2827/12Use of polyvinylhalogenides or derivatives thereof as mould material containing fluorine
    • B29K2827/16PVDF, i.e. polyvinylidene fluoride
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2877/00Use of PA, i.e. polyamides, e.g. polyesteramides or derivatives thereof, as mould material
    • B29K2877/10Aromatic polyamides [polyaramides] or derivatives thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037Other properties
    • B29K2995/0046Elastic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2007/00Flat articles, e.g. films or sheets
    • B29L2007/002Panels; Plates; Sheets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2024/00Articles with hollow walls
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/60Multitubular or multicompartmented articles, e.g. honeycomb
    • B29L2031/608Honeycomb structures
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1052Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1052Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • Y10T156/1062Prior to assembly
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/23Sheet including cover or casing
    • Y10T428/234Sheet including cover or casing including elements cooperating to form cells
    • Y10T428/236Honeycomb type cells extend perpendicularly to nonthickness layer
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24149Honeycomb-like
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T83/00Cutting
    • Y10T83/04Processes
    • Y10T83/0405With preparatory or simultaneous ancillary treatment of work
DE1993629078 1992-12-23 1993-12-07 Verfahren zur Herstellung eines wabenförmigen Kernes mit einer niedrigen Dichte und mit schrägen Oberflächen für einen Verbundkörper Expired - Lifetime DE69329078T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/995,437 US5354195A (en) 1992-12-23 1992-12-23 Composite molding apparatus for high pressure co-cure molding of lightweight honeycomb core composite articles having ramped surfaces utilizing low density, stabilized ramped honeycomb cores

Publications (2)

Publication Number Publication Date
DE69329078D1 true DE69329078D1 (de) 2000-08-24
DE69329078T2 DE69329078T2 (de) 2001-03-22

Family

ID=25541798

Family Applications (2)

Application Number Title Priority Date Filing Date
DE1993629078 Expired - Lifetime DE69329078T2 (de) 1992-12-23 1993-12-07 Verfahren zur Herstellung eines wabenförmigen Kernes mit einer niedrigen Dichte und mit schrägen Oberflächen für einen Verbundkörper
DE1993622171 Expired - Lifetime DE69322171T2 (de) 1992-12-23 1993-12-07 Vorrichtung zur formung eines verbandwerkstoffes und verfahren zur hochdruckverretzung eines leichten verbundgegenstands mit einem wabenförmigen kern,mit schrägen oberflächen unter verwendung von leichten,stabilizierten, schrägen,wabenförmigen kernen und das so hergestellte produkt

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE1993622171 Expired - Lifetime DE69322171T2 (de) 1992-12-23 1993-12-07 Vorrichtung zur formung eines verbandwerkstoffes und verfahren zur hochdruckverretzung eines leichten verbundgegenstands mit einem wabenförmigen kern,mit schrägen oberflächen unter verwendung von leichten,stabilizierten, schrägen,wabenförmigen kernen und das so hergestellte produkt

Country Status (13)

Country Link
US (3) US5354195A (de)
EP (2) EP0675796B1 (de)
JP (1) JP3335355B2 (de)
KR (1) KR100286153B1 (de)
AU (1) AU674051B2 (de)
BR (1) BR9307729A (de)
CA (1) CA2148470A1 (de)
DE (2) DE69329078T2 (de)
ES (1) ES2124390T3 (de)
IL (1) IL108100A (de)
TR (1) TR28891A (de)
TW (1) TW264428B (de)
WO (1) WO1994014600A1 (de)

Families Citing this family (87)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5520532A (en) * 1994-08-01 1996-05-28 United Technologies Corporation Molding assembly for forming airfoil structures
FR2726500B1 (fr) * 1994-11-09 1997-01-10 Eurocopter France Procede pour la realisation de panneaux composites de type sandwich et panneaux ainsi obtenus
AU2584095A (en) * 1995-01-27 1996-08-14 Sikorsky Aircraft Corporation Method for making honeycomb core composite articles
US5580502A (en) * 1995-03-23 1996-12-03 Sikorsky Aircraft Corporation Method of fabricating a composite article having an integral, co-cured composite stiffening member
FR2744054B1 (fr) * 1996-01-29 1998-04-30 Aerospatiale Procede de realisation de pieces en materiau composite a haute precision dimensionnelle mettant en oeuvre une polymerisation par ionisation et pieces ainsi obtenues
US6146578A (en) * 1997-10-09 2000-11-14 Lear Corporation Method for molding headliners
US6197146B1 (en) * 1998-12-21 2001-03-06 Sikorsky Aircraft Corporation Method and apparatus for forming airfoil structures
US6090335A (en) * 1999-01-08 2000-07-18 Northrop Grumman Corporation Process of forming fiber reinforced composite articles using an insitu cured resin infusion port
US6261675B1 (en) 1999-03-23 2001-07-17 Hexcel Corporation Core-crush resistant fabric and prepreg for fiber reinforced composite sandwich structures
US6245275B1 (en) * 1999-05-13 2001-06-12 Vought Aircraft Industries, Inc. Method for fabricating composite structures
AU3789801A (en) * 1999-12-07 2001-06-18 Boeing Company, The Double bag vacuum infusion process and system for low cost, advanced composite fabrication
US6620369B1 (en) 2000-02-09 2003-09-16 Northrop Grumman Corporation Net molding of resin composite parts
JP4078017B2 (ja) * 2000-06-27 2008-04-23 三菱重工業株式会社 宇宙環境で使用されるハニカムサンドイッチパネル
DE10033232C5 (de) * 2000-07-10 2006-10-05 Webasto Ag Fahrzeugdachteil mit einer Kunststoff-Außenhaut, Verfahren und Vorrichtung zur Herstellung desselben
CA2423665A1 (en) * 2000-10-02 2002-04-11 Bell Helicopter Textron Inc. Composite skin panel opening edge and method for manufacture
US7226559B2 (en) * 2000-12-08 2007-06-05 Toyota Motor Sales, U.S.A., Inc. Method for molding structures
US6719870B2 (en) * 2000-12-15 2004-04-13 The Boeing Company Fastenerless internal support for hollow structures
US6739861B2 (en) * 2001-11-26 2004-05-25 Sikorsky Aircraft Corporation High pressure co-cure of lightweight core composite article utilizing a core having a plurality of protruding pins
WO2005016643A1 (en) * 2002-04-30 2005-02-24 Aerospace Composite Structures, Llc Method of thermoforming frtp sandwich panels, thermoformed articles, modular container
US8114335B2 (en) * 2002-12-30 2012-02-14 The Goodyear Tire & Rubber Company Partial depth-wise cure of a tire inner liner
US6974606B2 (en) * 2003-05-23 2005-12-13 Northrop Grumman Corporation Thermoplastic coating for composite structures
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
US7160498B2 (en) * 2004-03-08 2007-01-09 Tracker Marine, L.L.C. Closed molding tool
US7837147B2 (en) 2005-03-18 2010-11-23 The Boeing Company Systems and methods for reducing noise in aircraft fuselages and other structures
US7416401B2 (en) * 2005-06-13 2008-08-26 The Boeing Company Lightweight composite fairing bar and method for manufacturing the same
GB0611875D0 (en) * 2006-06-15 2006-07-26 Airbus Uk Ltd A stringer for an aircraft wing and a method of forming thereof
DE102006031336B4 (de) * 2006-07-06 2010-08-05 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils in der Luft- und Raumfahrt
DE102006031325B4 (de) * 2006-07-06 2010-07-01 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031323B4 (de) * 2006-07-06 2010-07-15 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031326B4 (de) * 2006-07-06 2010-09-23 Airbus Deutschland Gmbh Formkern und Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031335B4 (de) * 2006-07-06 2011-01-27 Airbus Operations Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031334A1 (de) * 2006-07-06 2008-01-10 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
US8305773B2 (en) * 2006-08-18 2012-11-06 Delphi Technologies, Inc. Lightweight audio system for automotive applications and method
US7854874B2 (en) * 2006-11-20 2010-12-21 The Boeing Company Apparatus and methods for forming hat stiffened composite parts using thermally expansive tooling cauls
ES2698436T3 (es) * 2006-12-01 2019-02-04 Tanazawa Hakkosha Kk Molde para moldeo de resina, método de fabricación de molde para moldeo de resina y producto moldeado de resina
US9511571B2 (en) * 2007-01-23 2016-12-06 The Boeing Company Composite laminate having a damping interlayer and method of making the same
US7861969B2 (en) * 2007-05-24 2011-01-04 The Boeing Company Shaped composite stringers and methods of making
ITTO20070507A1 (it) * 2007-07-11 2009-01-12 Alenia Aeronautica Spa Procedimento di fabbricazione di una struttura d'ala monolitica a profilo integrale
US7879276B2 (en) * 2007-11-08 2011-02-01 The Boeing Company Foam stiffened hollow composite stringer
US20090155524A1 (en) 2007-12-13 2009-06-18 Rapp Robert A Composite panel and method of manufacturing the same
GB2456566B (en) * 2008-01-18 2012-03-07 Gkn Aerospace Services Ltd A method of manufacturing a polymer matrix composite forming tool
US8071008B1 (en) * 2008-03-27 2011-12-06 Ceradyne, Inc. Composite forming technology
EP2116358B1 (de) * 2008-05-09 2016-06-29 Saab Ab Verfahren und Vorrichtung zur Anpassung eines Flansches
DE102008002117B4 (de) * 2008-05-30 2013-10-31 Airbus Operations Gmbh Verbund und Struktur
US9238335B2 (en) * 2008-07-10 2016-01-19 The Boeing Company Mandrel for autoclave curing applications
US9327467B2 (en) 2008-07-10 2016-05-03 The Boeing Company Composite mandrel for autoclave curing applications
US8540921B2 (en) * 2008-11-25 2013-09-24 The Boeing Company Method of forming a reinforced foam-filled composite stringer
KR101033476B1 (ko) * 2009-01-08 2011-05-09 주식회사 대한항공 프리프레그 절곡 성형장치 및 그 성형방법
US8425710B2 (en) * 2009-03-13 2013-04-23 The Boeing Company Automated placement of vibration damping materials
US8500066B2 (en) * 2009-06-12 2013-08-06 The Boeing Company Method and apparatus for wireless aircraft communications and power system using fuselage stringers
US8570152B2 (en) * 2009-07-23 2013-10-29 The Boeing Company Method and apparatus for wireless sensing with power harvesting of a wireless signal
US8617687B2 (en) * 2009-08-03 2013-12-31 The Boeing Company Multi-functional aircraft structures
US8251174B2 (en) * 2010-03-26 2012-08-28 Spirit Aerosystems, Inc. Method for bonding honeycomb cores
DE102010018726B4 (de) * 2010-04-29 2013-08-14 Premium Aerotec Gmbh Verfahren zur Herstellung eines mit zumindest einem Hohlprofil versehenen Bauteils
FR2963272B1 (fr) 2010-07-29 2012-08-17 Airbus Operations Sas Procede de fabrication d'un panneau raidi en materiau composite
US9676124B2 (en) * 2010-12-01 2017-06-13 Plasan Carbon Composites, Inc. Method and system for forming composite articles
US9776385B2 (en) 2011-04-05 2017-10-03 Sikorsky Aircraft Corporation External to bagging mechanical clamp
US20130154154A1 (en) * 2011-06-27 2013-06-20 William L. Rodman Composite structures having cored members
JP6050351B2 (ja) 2011-07-28 2016-12-21 プレイザン カーボン コンポジティーズ,インコーポレイテッド 複合材製品の成形用システム及び方法
US8985174B2 (en) * 2011-08-26 2015-03-24 The Boeing Company Integrally stiffened, reusable vacuum bag and method of making the same
US9333713B2 (en) 2012-10-04 2016-05-10 The Boeing Company Method for co-curing composite skins and stiffeners in an autoclave
US9409358B2 (en) * 2012-10-15 2016-08-09 Sikorsky Aircraft Corporation Composite structure core crush prevention
US9149999B2 (en) 2012-10-30 2015-10-06 Bell Helicopter Textron Inc. Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same
US9333684B2 (en) 2012-10-30 2016-05-10 Bell Helicopter Textron Inc. Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same
US9015941B2 (en) 2012-10-30 2015-04-28 Bell Helicopter Textron Inc. Method of repairing honeycomb core using pourable structural foam
US9597826B2 (en) * 2012-10-30 2017-03-21 Bell Helicopter Textron Inc. Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same
EP2842865B1 (de) 2013-08-28 2019-12-18 Airbus Operations GmbH Fensterscheibe für ein flugwerk und verfahren zur herstellung davon
US9896183B2 (en) 2014-08-25 2018-02-20 Sikorsky Aircraft Corporation Airframe component with electrically bonded connections
US9845059B2 (en) * 2015-05-11 2017-12-19 Bose Corporation Acoustic enclosure for motor vehicle
US10632708B2 (en) * 2016-02-29 2020-04-28 Alienus Film Llc Insulating film
CN106541434B (zh) * 2016-11-30 2018-06-22 上海荣南科技有限公司 一种天窗密封条精切机机械装置
AT519620B1 (de) * 2017-02-14 2018-11-15 Hilitech Gmbh Schaumstoffplatte
CN106863874B (zh) * 2017-03-06 2019-04-09 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种复杂曲面蜂窝夹层结构的蜂窝定型方法
DE102017214340A1 (de) 2017-08-17 2019-02-21 Airbus Operations Gmbh Verfahren zur Herstellung eines Sandwichbauteils, Kern für ein Sandwichbauteil sowie Sandwichbauteil
FR3074088B1 (fr) * 2017-11-30 2021-02-12 Safran Aircraft Engines Carter en materiau composite renforce et son procede de fabrication
US20200398520A1 (en) * 2018-03-05 2020-12-24 Nippi Corporation Method for forming honeycomb sandwich composite material and jig used therefor
GB2575102A (en) * 2018-06-29 2020-01-01 Airbus Operations Ltd Duct stringer with bulkhead
DE102018119751A1 (de) * 2018-08-14 2020-02-20 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Anlage zum Herstellen eines Hybrid-Bauteils
US11034064B2 (en) * 2018-08-29 2021-06-15 The Boeing Company Overlapping caul plates and method for composite manufacturing
CN109291466B (zh) * 2018-08-30 2020-10-20 哈尔滨飞机工业集团有限责任公司 一种大倒角蜂窝夹层结构件的成型方法
WO2020178950A1 (ja) * 2019-03-04 2020-09-10 日本飛行機株式会社 圧力パッド、圧力パッドの製造方法およびハニカムコアサンドイッチ構造体の製造方法
US10987831B2 (en) * 2019-05-24 2021-04-27 The Boeing Company Dies for forming a part and associated systems and methods
DE102019005908A1 (de) * 2019-08-22 2021-02-25 Siempelkamp Maschinen- Und Anlagenbau Gmbh Verfahren zum Erzeugen eines Bauelements
JP7264267B2 (ja) * 2019-10-03 2023-04-25 株式会社Ihi プリプレグから繊維強化プラスチック結合体を製造する方法
CN111775517A (zh) * 2020-06-03 2020-10-16 航天材料及工艺研究所 一种结构与生物安全一体化轻质蜂窝夹层结构及其制备方法
WO2021255880A1 (ja) * 2020-06-17 2021-12-23 三菱重工業株式会社 治具及び複合材の加工方法
CN115195152A (zh) * 2021-04-14 2022-10-18 波音公司 用于处理复合结构的设备和方法

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL89352C (de) * 1957-02-20 1900-01-01
US3345233A (en) * 1963-11-06 1967-10-03 Midland Ross Corp Process for making circumambient wall unit
CH440639A (de) * 1966-04-21 1967-07-31 Contraves Ag Verfahren zum Herstellen von Zellstrukturbaukörpern und nach diesem Verfahren hergestellter Baukörper
US3575756A (en) * 1968-10-15 1971-04-20 North American Rockwell Laminated structural members
US3666600A (en) * 1969-03-10 1972-05-30 North American Rockwell Apparatus for forming layup laminate
DE2836418A1 (de) * 1978-08-19 1980-02-28 Helmut Dipl Phys Nussbaum Halbzeug fuer sandwich-leichtbauweisen, hergestellt aus roehrchen von vlies-werkstoff, z.b. aus papier
US4350551A (en) * 1980-12-29 1982-09-21 The Boeing Company Fluid slip sheet and method
GB2124130B (en) * 1982-07-24 1985-11-27 Rolls Royce Vacuum moulding fibre reinforced resin
GB2173144B (en) * 1985-04-02 1989-08-09 Rolls Royce Plc Moulding of composite materials
AT385710B (de) * 1985-06-26 1988-05-10 Ver Edelstahlwerke Ag Verfahren und vorrichtung zum trennen bzw. schneiden von flaechigen werkstuecken aus, z.b. faserverstaerkten kunststoffen
US4915896A (en) * 1987-09-01 1990-04-10 Phillips Petroleum Company Vacuum bagging process for fiber reinforced thermoplastics
US5071338A (en) * 1987-09-08 1991-12-10 United Technologies Corporation Tool for forming complex composite articles
US4910065A (en) * 1987-10-15 1990-03-20 The Boeing Company Reinforced honeycomb core sandwich panels and method for making same
JPH01267010A (ja) * 1987-12-07 1989-10-24 Boeing Co:The 熱可塑性積層体を製造する方法
GB2219245A (en) * 1988-06-03 1989-12-06 Rawson Francis F H Ultrasonic cutting
FR2643015B1 (fr) * 1989-02-14 1991-04-19 Air Liquide Procede d'elaboration d'une atmosphere pour la fabrication d'elements composites a haute performance par moulage au sac
US4879152A (en) * 1989-02-15 1989-11-07 Green Patrick H Composite panel structure
US4942013A (en) * 1989-03-27 1990-07-17 Mcdonnell Douglas Corporation Vacuum resin impregnation process
US5034256A (en) * 1989-08-28 1991-07-23 United Technologies Corporation Closeout configuration for honeycomb core composite sandwich panels
JP2716564B2 (ja) * 1990-03-22 1998-02-18 富士重工業株式会社 ハニカム構造部材の切断方法および切断装置
JP2517445B2 (ja) * 1990-06-05 1996-07-24 スカイアルミニウム株式会社 ダイアフラム成形用a1合金板およびその製造方法
US5242651A (en) * 1990-07-25 1993-09-07 Vought Aircraft Company Pressure balanced processing of composite structures
US5248242A (en) * 1990-09-28 1993-09-28 The Boeing Company Aerodynamic rotor blade of composite material fabricated in one cure cycle
US5152949A (en) * 1990-12-19 1992-10-06 United Technologies Corporation Tooling method for resin transfer molding
US5236646A (en) * 1991-02-28 1993-08-17 The United States Of America As Represented By The Secretary Of The Navy Process for preparing thermoplastic composites
US5106568A (en) * 1991-11-15 1992-04-21 Mcdonnell Douglas Corporation Method and apparatus for vacuum bag molding of composite materials

Also Published As

Publication number Publication date
CA2148470A1 (en) 1994-07-07
AU5870194A (en) 1994-07-19
ES2124390T3 (es) 1999-02-01
WO1994014600A1 (en) 1994-07-07
EP0822057B1 (de) 2000-07-19
IL108100A0 (en) 1994-04-12
JP3335355B2 (ja) 2002-10-15
BR9307729A (pt) 1999-08-31
US5688353A (en) 1997-11-18
TW264428B (de) 1995-12-01
AU674051B2 (en) 1996-12-05
IL108100A (en) 1998-04-05
EP0675796A1 (de) 1995-10-11
US5354195A (en) 1994-10-11
KR100286153B1 (ko) 2001-04-16
DE69322171T2 (de) 1999-06-24
EP0675796B1 (de) 1998-11-18
KR950704107A (ko) 1995-11-17
US5527414A (en) 1996-06-18
DE69329078T2 (de) 2001-03-22
TR28891A (tr) 1997-07-17
EP0822057A1 (de) 1998-02-04
DE69322171D1 (de) 1998-12-24
JPH08506534A (ja) 1996-07-16

Similar Documents

Publication Publication Date Title
DE69329078D1 (de) Verfahren zur Herstellung eines wabenförmigen Kernes mit einer niedrigen Dichte und mit schrägen Oberflächen für einen Verbundkörper
DE69316027D1 (de) Verfahren zur herstellung einer faserigen struktur mit immobilisiertem teilchenförmigem material
DE69529775T2 (de) Verfahren zur Herstellung einer Damaszenstruktur mit einer WGe Polierstoppschicht
DE69117845T2 (de) Verfahren zur Herstellung eines Kompositkörpers und Verwendung in Festoxidbrennstoffzelle
DE69325424D1 (de) Verbundwerkstoff Vorform und Verfahren zur Herstellung eines faserverstärkten Verbundwerkstoffes
DE69002271T2 (de) Verfahren zur herstellung einer dichtung mit metallischem koerper und einem weichen abschichtungselement.
DE69306137T2 (de) Verfahren zur Herstellung einer Faserverstärkung für ein Teil aus Verbundmaterial mit nicht-koplanaren Seiten und Verbundteile mit einer solchen Verstärkung
DE69712685D1 (de) Formanordnung zur Herstellung eines mehrschichtigen geformten Gegenstandes und deren Verwendung bei einem Verfahren zur Herstellung eines mehrschichtigen geformten Gegenstandes
DE69511351T2 (de) Verfahren zur Herstellung eines Verbundoxides mit sauerstoffabsorbierender und -desorbierender Fähigkeit
DE59510891D1 (de) Verfahren zur Herstellung eines Schichtverbundkörpers
DE69726997D1 (de) Verfahren zur Herstellung einer Platte mit Honigwabenstruktur aus einem Kohlenstoff/Kohlenstoff- oder Kohlenstoff/Keramik-Verbundkörper sowie Strukturen die eine derartige Platte enthalten
ATA75189A (de) Verfahren zur herstellung eines ni-fe-legierungsbleches mit ausgezeichneten gleichstrommagnetischen und wechselstrommagnetischen eigenschaften
DE69130111T2 (de) Verfahren zur herstellung eines verbundwerkstoffes sowie verbundwerkstoff
DE69001703D1 (de) Verfahren und geraet zur herstellung einer nute in einem werkstueck.
DE69109110D1 (de) Verfahren zur herstellung eines mehrschichtigen gegenstandes für honigwabenstrukturen.
DE69304040T2 (de) Leichtgewicht-Behälter mit zusammengesetztem Aufbau und Verfahren zur Herstellung desselben
DE69502277D1 (de) Verfahren zur herstellung einer düse für kraftstoffventil und düse
DE69324850T2 (de) Verfahren und Vorrichtung zur Herstellung eines Verbundwerkstoffs für eine Wabenstruktur
DE3881508T2 (de) Multischicht-Acryl-Verbundfäden und Verfahren zur Herstellung derselben.
DE69025029T3 (de) Kunstharzformkörper mit einer dünnen Metallschicht und Verfahren zu seiner Herstellung
ATA99392A (de) Verfahren zur herstellung eines regenerats und dessen verwendung
DE69210954T2 (de) Verfahren zur Herstellung eines weichmagnetischen Komposit-Materials und weichmagnetisches Komposit-Material
DE69510562D1 (de) Verfahren und form zur herstellung eines befestigungselements mit einem ineinandergreifenden verbindungselement und so hergestellter artikel
DE69316357D1 (de) Verfahren zur herstellung einer hindurchdringenden öffnung in einem faserverstärkten compositmaterial
DE59405973D1 (de) Verfahren zur Herstellung eines in Längsrichtung hochelastisch dehnbaren Trägerbandes und ein danach gefertigtes Trägerband

Legal Events

Date Code Title Description
8364 No opposition during term of opposition