DE69322171T2 - 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 - Google Patents
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 produktInfo
- Publication number
- DE69322171T2 DE69322171T2 DE1993622171 DE69322171T DE69322171T2 DE 69322171 T2 DE69322171 T2 DE 69322171T2 DE 1993622171 DE1993622171 DE 1993622171 DE 69322171 T DE69322171 T DE 69322171T DE 69322171 T2 DE69322171 T2 DE 69322171T2
- Authority
- DE
- Germany
- Prior art keywords
- light
- troubled
- stabilized
- shaping
- fabric
- 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
- 239000002131 composite material Substances 0.000 title 1
- 239000000463 material Substances 0.000 title 1
- 238000000034 method Methods 0.000 title 1
- 238000007493 shaping process Methods 0.000 title 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0089—Producing honeycomb structures
-
- 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
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/38—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
-
- 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
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/76—Cores
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C43/36—Moulds for making articles of definite length, i.e. discrete articles
- B29C43/3642—Bags, bleeder sheets or cauls for isostatic pressing
-
- 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
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/549—Details of caul plates, e.g. materials or shape
-
- 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
- B29D24/007—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 and a chamfered edge
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C43/36—Moulds for making articles of definite length, i.e. discrete articles
- B29C43/3642—Bags, bleeder sheets or cauls for isostatic pressing
- B29C2043/3644—Vacuum bags; Details thereof, e.g. fixing or clamping
-
- 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
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/38—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
- B29C33/40—Plastics, e.g. foam or rubber
- B29C33/405—Elastomers, e.g. rubber
-
- 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
- B29K2705/00—Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
- B29K2705/02—Aluminium
-
- 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
- B29K2827/00—Use of polyvinylhalogenides or derivatives thereof as mould material
- B29K2827/12—Use of polyvinylhalogenides or derivatives thereof as mould material containing fluorine
- B29K2827/16—PVDF, i.e. polyvinylidene fluoride
-
- 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
- B29K2877/00—Use of PA, i.e. polyamides, e.g. polyesteramides or derivatives thereof, as mould material
- B29K2877/10—Aromatic polyamides [polyaramides] or derivatives thereof
-
- 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
- B29K2995/0037—Other properties
- B29K2995/0046—Elastic
-
- 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
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2024/00—Articles with hollow walls
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
- Y10T156/1062—Prior to assembly
-
- 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
- Y10T428/24—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
- Y10T83/00—Cutting
- Y10T83/04—Processes
- Y10T83/0405—With preparatory or simultaneous ancillary treatment of work
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Manufacturing & Machinery (AREA)
- Laminated Bodies (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
Applications Claiming Priority (2)
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 |
PCT/US1993/011826 WO1994014600A1 (en) | 1992-12-23 | 1993-12-07 | A composite molding apparatus and method for high pressure co-cure molding of lightweight honeycomb core composite articles having ramped surfaces utilizing low density, stabilized ramped honeycomb cores and product formed thereby |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69322171D1 DE69322171D1 (de) | 1998-12-24 |
DE69322171T2 true DE69322171T2 (de) | 1999-06-24 |
Family
ID=25541798
Family Applications (2)
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 |
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 |
Family Applications After (1)
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 |
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) | DE69322171T2 (de) |
ES (1) | ES2124390T3 (de) |
IL (1) | IL108100A (de) |
TR (1) | TR28891A (de) |
TW (1) | TW264428B (de) |
WO (1) | WO1994014600A1 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AT519620A1 (de) * | 2017-02-14 | 2018-08-15 | Hilitech Gmbh | Schaumstoffplatte |
Families Citing this family (86)
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 |
JP3403201B2 (ja) * | 1995-01-27 | 2003-05-06 | シコルスキー エアクラフト コーポレイション | ハニカムコア複合製品の製造方法 |
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 |
WO2001041993A2 (en) * | 1999-12-07 | 2001-06-14 | The Boeing Company | 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 |
DE10066339B4 (de) * | 2000-07-10 | 2010-09-16 | 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 |
DE102006031334A1 (de) * | 2006-07-06 | 2008-01-10 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
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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 |
US9327467B2 (en) * | 2008-07-10 | 2016-05-03 | The Boeing Company | Composite mandrel for autoclave curing applications |
US9238335B2 (en) * | 2008-07-10 | 2016-01-19 | The Boeing Company | 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 |
KR20140018852A (ko) * | 2010-12-01 | 2014-02-13 | 플라산 카본 컴포짓, 인코포레이티드 | 복합 물품을 형성하는 방법과 시스템 |
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 |
KR20140053143A (ko) | 2011-07-28 | 2014-05-07 | 플라산 카본 컴포짓, 인코포레이티드 | 복합재 물품들을 급속히 형성하기 위한 열 시스템 및 방법 |
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 |
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 |
US9015941B2 (en) | 2012-10-30 | 2015-04-28 | Bell Helicopter Textron Inc. | Method of repairing honeycomb core using pourable structural foam |
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 |
WO2017151688A1 (en) * | 2016-02-29 | 2017-09-08 | Alienus Film Llc | Vacuum 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 |
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 |
JP6722369B2 (ja) * | 2018-03-05 | 2020-07-15 | 日本飛行機株式会社 | ハニカムサンドイッチ複合材の成形方法 |
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 |
EP4039437A4 (de) * | 2019-10-03 | 2023-10-25 | IHI Corporation | Verfahren zur herstellung eines faserverstärkten kunststoffverbundkörpers aus prepreg |
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)
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 |
EP0319895A3 (de) * | 1987-12-07 | 1990-10-31 | The Boeing Company | Verfahren zum Verdichten von teilweise vorgehärteten thermoplastischen Verbund-Plättchen |
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 |
-
1992
- 1992-12-23 US US07/995,437 patent/US5354195A/en not_active Expired - Lifetime
-
1993
- 1993-12-07 AU AU58701/94A patent/AU674051B2/en not_active Ceased
- 1993-12-07 ES ES94904821T patent/ES2124390T3/es not_active Expired - Lifetime
- 1993-12-07 KR KR1019950702575A patent/KR100286153B1/ko not_active IP Right Cessation
- 1993-12-07 DE DE1993622171 patent/DE69322171T2/de not_active Expired - Lifetime
- 1993-12-07 DE DE1993629078 patent/DE69329078T2/de not_active Expired - Lifetime
- 1993-12-07 WO PCT/US1993/011826 patent/WO1994014600A1/en active IP Right Grant
- 1993-12-07 JP JP51519294A patent/JP3335355B2/ja not_active Expired - Fee Related
- 1993-12-07 EP EP19940904821 patent/EP0675796B1/de not_active Expired - Lifetime
- 1993-12-07 EP EP19970115208 patent/EP0822057B1/de not_active Expired - Lifetime
- 1993-12-07 CA CA 2148470 patent/CA2148470A1/en not_active Abandoned
- 1993-12-07 BR BR9307729A patent/BR9307729A/pt not_active Application Discontinuation
- 1993-12-20 IL IL108100A patent/IL108100A/en not_active IP Right Cessation
- 1993-12-22 TW TW82110892A patent/TW264428B/zh not_active IP Right Cessation
- 1993-12-23 TR TR121493A patent/TR28891A/xx unknown
-
1994
- 1994-05-18 US US08/245,984 patent/US5527414A/en not_active Expired - Lifetime
-
1995
- 1995-12-26 US US08/581,865 patent/US5688353A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AT519620A1 (de) * | 2017-02-14 | 2018-08-15 | Hilitech Gmbh | Schaumstoffplatte |
AT519620B1 (de) * | 2017-02-14 | 2018-11-15 | Hilitech Gmbh | Schaumstoffplatte |
Also Published As
Publication number | Publication date |
---|---|
TR28891A (tr) | 1997-07-17 |
EP0822057B1 (de) | 2000-07-19 |
AU5870194A (en) | 1994-07-19 |
DE69329078D1 (de) | 2000-08-24 |
EP0675796B1 (de) | 1998-11-18 |
JP3335355B2 (ja) | 2002-10-15 |
AU674051B2 (en) | 1996-12-05 |
KR100286153B1 (ko) | 2001-04-16 |
BR9307729A (pt) | 1999-08-31 |
JPH08506534A (ja) | 1996-07-16 |
EP0675796A1 (de) | 1995-10-11 |
DE69322171D1 (de) | 1998-12-24 |
IL108100A (en) | 1998-04-05 |
DE69329078T2 (de) | 2001-03-22 |
US5354195A (en) | 1994-10-11 |
TW264428B (de) | 1995-12-01 |
IL108100A0 (en) | 1994-04-12 |
US5527414A (en) | 1996-06-18 |
EP0822057A1 (de) | 1998-02-04 |
US5688353A (en) | 1997-11-18 |
WO1994014600A1 (en) | 1994-07-07 |
CA2148470A1 (en) | 1994-07-07 |
KR950704107A (ko) | 1995-11-17 |
ES2124390T3 (es) | 1999-02-01 |
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