RU2488488C2 - Способ и устройство для производства цилиндрических конструктивных компонентов - Google Patents
Способ и устройство для производства цилиндрических конструктивных компонентов Download PDFInfo
- Publication number
- RU2488488C2 RU2488488C2 RU2010122662/05A RU2010122662A RU2488488C2 RU 2488488 C2 RU2488488 C2 RU 2488488C2 RU 2010122662/05 A RU2010122662/05 A RU 2010122662/05A RU 2010122662 A RU2010122662 A RU 2010122662A RU 2488488 C2 RU2488488 C2 RU 2488488C2
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- RU
- Russia
- Prior art keywords
- support
- pressure
- molding tool
- fibrous
- cylindrical
- Prior art date
Links
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 26
- 238000000034 method Methods 0.000 title claims abstract description 22
- 239000004744 fabric Substances 0.000 claims abstract description 66
- 239000000835 fiber Substances 0.000 claims abstract description 17
- 239000011159 matrix material Substances 0.000 claims abstract description 15
- 238000000465 moulding Methods 0.000 claims description 77
- 239000012528 membrane Substances 0.000 claims description 40
- 230000003014 reinforcing effect Effects 0.000 claims description 38
- 239000000945 filler Substances 0.000 claims description 10
- 239000011248 coating agent Substances 0.000 claims description 3
- 238000000576 coating method Methods 0.000 claims description 3
- 238000003825 pressing Methods 0.000 claims description 2
- 238000005470 impregnation Methods 0.000 claims 1
- 238000009434 installation Methods 0.000 claims 1
- 238000010327 methods by industry Methods 0.000 abstract 1
- 239000000126 substance Substances 0.000 abstract 1
- 239000011347 resin Substances 0.000 description 7
- 229920005989 resin Polymers 0.000 description 7
- 238000004804 winding Methods 0.000 description 7
- 239000000463 material Substances 0.000 description 6
- 238000010438 heat treatment Methods 0.000 description 5
- 239000002657 fibrous material Substances 0.000 description 4
- 230000002093 peripheral effect Effects 0.000 description 3
- 239000004918 carbon fiber reinforced polymer Substances 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- -1 for example Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 230000012447 hatching Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000002985 plastic film Substances 0.000 description 1
- 229920006255 plastic film Polymers 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—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
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
- B29C33/48—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling
- B29C33/50—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible
- B29C33/505—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible cores or mandrels, e.g. inflatable
-
- 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
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/345—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using matched moulds
-
- 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
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/36—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and impregnating by casting, e.g. vacuum casting
-
- 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
- B29C70/443—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 and impregnating by vacuum or injection
-
- 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
- B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
-
- 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
- B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement
-
- 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
- B29D23/00—Producing tubular articles
- B29D23/001—Pipes; Pipe joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B30—PRESSES
- B30B—PRESSES IN GENERAL
- B30B5/00—Presses characterised by the use of pressing means other than those mentioned in the preceding groups
- B30B5/02—Presses characterised by the use of pressing means other than those mentioned in the preceding groups wherein the pressing means is in the form of a flexible element, e.g. diaphragm, urged by fluid pressure
-
- 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
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
- B29K2105/0872—Prepregs
- B29K2105/089—Prepregs fabric
-
- 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
- B29K2307/00—Use of elements other than metals as reinforcement
- B29K2307/04—Carbon
-
- 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
- B29L2023/00—Tubular articles
- B29L2023/22—Tubes or pipes, i.e. rigid
-
- 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
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
- B29L2031/3082—Fuselages
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Applications Claiming Priority (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US749207P | 2007-12-13 | 2007-12-13 | |
| DE102007060029A DE102007060029A1 (de) | 2007-12-13 | 2007-12-13 | Verfahren und Vorrichtung zur Herstellung röhrenförmiger Strukturbauteile |
| DE102007060029.3 | 2007-12-13 | ||
| US61/007,492 | 2007-12-13 | ||
| PCT/EP2008/065355 WO2009074419A1 (de) | 2007-12-13 | 2008-11-12 | Verfahren und vorrichtung zur herstellung röhrenförmiger strukturbauteile |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2010122662A RU2010122662A (ru) | 2012-01-20 |
| RU2488488C2 true RU2488488C2 (ru) | 2013-07-27 |
Family
ID=40679895
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2010122662/05A RU2488488C2 (ru) | 2007-12-13 | 2008-11-12 | Способ и устройство для производства цилиндрических конструктивных компонентов |
Country Status (9)
| Country | Link |
|---|---|
| US (3) | US20100276069A1 (https=) |
| EP (1) | EP2229273B1 (https=) |
| JP (1) | JP2011506136A (https=) |
| CN (1) | CN101896329B (https=) |
| BR (1) | BRPI0821246A2 (https=) |
| CA (1) | CA2707802A1 (https=) |
| DE (1) | DE102007060029A1 (https=) |
| RU (1) | RU2488488C2 (https=) |
| WO (1) | WO2009074419A1 (https=) |
Families Citing this family (28)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8529818B2 (en) * | 2009-09-30 | 2013-09-10 | General Electric Company | Automated fiber placement in female mold |
| DE102009057009B4 (de) * | 2009-12-04 | 2015-01-08 | Airbus Defence and Space GmbH | Vorrichtung und Verfahren zur Herstellung eines schalenförmigen Verbundbauteils |
| DE102009056978A1 (de) * | 2009-12-07 | 2011-06-09 | Airbus Operations Gmbh | Vorrichtung und Verfahren zur Herstellung einer aus einem Faserverbundwerkstoff bestehenden Rumpfschale für ein Luftfahrzeug |
| DE102010043415B4 (de) | 2010-11-04 | 2015-04-09 | Airbus Operations Gmbh | Verfahren zum Herstellen eines hohlen Bauteils sowie Vorrichtung |
| DE102010051739B3 (de) | 2010-11-19 | 2011-12-29 | Siempelkamp Maschinen- Und Anlagenbau Gmbh & Co. Kg | Verfahren und Vorrichtung zum Herstellen von zylindrischen Großstrukturen |
| DE102011119226A1 (de) * | 2011-11-22 | 2013-05-23 | Daimler Ag | Verfahren zum Herstellen eines Hohlprofilssowie Hohlprofilbauteil |
| EP2626194A1 (en) * | 2012-02-07 | 2013-08-14 | Siemens Aktiengesellschaft | Method of manufacturing a turbine blade, system for manufacturing a turbine blade and intermediate member for manufacturing a turbine blade |
| ITTO20120317A1 (it) * | 2012-04-12 | 2013-10-13 | Alenia Aermacchi Spa | Procedimento per la fabbricazione di barili integrali di fusoliera in materiale composito |
| DE102012010271B4 (de) * | 2012-05-25 | 2017-10-12 | Premium Aerotec Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils mittels eines Vakuumaufbaues |
| DE102012210043A1 (de) * | 2012-06-14 | 2013-12-19 | Airbus Operations Gmbh | Verfahren und Vorrichtung zur Herstellung einer Leichtbaustruktur sowie Leichtbaustruktur |
| JP6214300B2 (ja) | 2012-10-29 | 2017-10-18 | キヤノン株式会社 | 定着用部材の製造方法及び製造装置 |
| DE102012112939A1 (de) * | 2012-12-21 | 2014-06-26 | Leichtbau-Zentrum Sachsen Gmbh | Vorrichtung und Verfahren zur Infiltration einer Faserpreform |
| DE102013205089A1 (de) * | 2013-03-22 | 2014-09-25 | Supertex Composites Gmbh | Verfahren und Herstellungssystem zur Herstellung eines faserverstärkten Strukturbauteils |
| DE102013209143A1 (de) * | 2013-05-16 | 2014-11-20 | Zf Friedrichshafen Ag | Verfahren zum Herstellen eines rotationssymmetrischen Faser-Kunststoff-Verbund-Bauteils, Vorrichtung zur Durchführung eines derartigen Verfahrens und rotationssym-metrisches Faser-Kunststoff-Verbund-Bauteil |
| DE102014112311B4 (de) | 2014-08-27 | 2025-06-05 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verfahren und Formwerkzeug zur Infusion eines Matrixmaterials |
| DE102014217039A1 (de) * | 2014-08-27 | 2016-03-03 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren für die Herstellung eines mit wenigstens einem Verstärkungsschott verstärkten geschlossenen Hohlprofils aus Faserverbundmaterial |
| DE102014217486A1 (de) * | 2014-09-02 | 2016-03-03 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zum Herstellen von FKV-Bauteilen mit lokaler Verstärkung |
| CN104494160B (zh) * | 2014-11-25 | 2017-01-25 | 中联重科股份有限公司 | 折叠臂架、纤维增强树脂基复合材料臂节及其制造方法 |
| GB2554218A (en) * | 2015-03-17 | 2018-03-28 | Harvard College | Automated membrane fabrication system |
| EP3312083B1 (en) * | 2015-11-05 | 2021-10-20 | Airbus Operations, S.L.U. | Forming tool for manufacturing an aperture surrounding frame for an aircraft fuselage |
| US10689087B2 (en) | 2016-08-02 | 2020-06-23 | The Boeing Company | Tubular structure and a method of manufacturing thereof |
| GB2555089A (en) * | 2016-10-11 | 2018-04-25 | Jaguar Land Rover Ltd | A Method of moulding a composite structure |
| ES2954328T3 (es) * | 2017-07-25 | 2023-11-21 | Subaru Corp | Plantilla de moldeo de materiales compuestos y método de moldeo de materiales compuestos |
| US10520933B2 (en) | 2018-04-13 | 2019-12-31 | The Boeing Company | System and method for removing a workpiece from a manufacturing fixture |
| US11523750B2 (en) | 2018-08-06 | 2022-12-13 | Biosense Webster (Israel) Ltd. | Assessing tissue contact with catheter using pairs of electrodes and common reference ground established using designed circuit-board capacitance |
| DE102019007784B4 (de) * | 2019-11-09 | 2021-07-01 | Diehl Aviation Laupheim Gmbh | Hohlkanal-Herstellung im Sandwich-Panel mit Platzhalter und Sandwich-Panel |
| CN116442565B (zh) * | 2023-04-25 | 2026-03-10 | 哈尔滨工程大学 | 复合材料波纹夹芯圆柱耐压壳一体成型模具及其制备方法 |
| CN117287623A (zh) * | 2023-09-08 | 2023-12-26 | 浙江大学 | 用于低温绝热容器外壳的筒体、低温绝热容器及制造设备 |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2739350A (en) * | 1952-01-28 | 1956-03-27 | Northrop Aircraft Inc | Method and means of molding |
| US2815534A (en) * | 1954-07-12 | 1957-12-10 | Ising George Earl | Process for making a closed one-piece reinforced plastic tank |
| EP0408161A2 (de) * | 1989-07-12 | 1991-01-16 | Mecron Medizinische Produkte Gmbh | Verfahren zur Herstellung eines Hohlkörpers |
| RU2123571C1 (ru) * | 1993-05-03 | 1998-12-20 | Дриллфлекс | Трубчатая конструкция предварительно отформованной заготовки или матрицы для обсадки скважины |
| EP0911143A1 (fr) * | 1997-10-20 | 1999-04-28 | Sarma | Procédé de moulage d'une pièce globalement cylindrique à profil creux en matière composite, moule pour sa fabrication et pièce ainsi obtenue |
| RU2156397C1 (ru) * | 1999-06-30 | 2000-09-20 | Государственное предприятие "Производственное объединение "Авангард" | Способ ремонта трубопровода (варианты) |
| WO2000061464A1 (en) * | 1999-04-14 | 2000-10-19 | A & P Technology, Inc. | Integrally-reinforced braided tubular structure and method of producing the same |
| EP1134069A1 (en) * | 1998-09-30 | 2001-09-19 | Toray Industries, Inc. | Hollow structure of fiber-reinforced resin and method of manufacturing the same |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2995781A (en) * | 1957-11-19 | 1961-08-15 | Clarence L Sipler | Method of making tubular conduits |
| US3049901A (en) * | 1960-04-01 | 1962-08-21 | Singer Fidelity Inc | Flexible hose |
| JP2935722B2 (ja) * | 1990-02-28 | 1999-08-16 | 富士重工業株式会社 | 航空機の胴体構造およびその成形方法 |
| CA2056224A1 (en) | 1990-12-19 | 1992-06-20 | Terry Martin Boustead | Conformal composite molding |
| DE19803909A1 (de) | 1998-02-02 | 1999-08-05 | Ver Foerderung Inst Kunststoff | Verfahren zur Herstellung von endlosfaserverstärkten Hohlkörpern im Harzinjektionsverfahren |
| JP4346143B2 (ja) * | 1999-02-24 | 2009-10-21 | 社団法人日本航空宇宙工業会 | 複合樹脂製品の成形方法及びその装置 |
| DE19913079A1 (de) * | 1999-03-23 | 2000-09-28 | Bayerische Motoren Werke Ag | Bauteil aus einem thermoplastischen Faserverbundwerkstoff und Verfahren zu dessen Herstellung |
| US7204951B2 (en) * | 2002-07-30 | 2007-04-17 | Rocky Mountain Composites, Inc. | Method of assembling a single piece co-cured structure |
| US20040219855A1 (en) * | 2003-05-02 | 2004-11-04 | Tsotsis Thomas K. | Highly porous interlayers to toughen liquid-molded fabric-based composites |
| US20080289743A1 (en) * | 2003-05-02 | 2008-11-27 | Tsotsis Thomas K | Highly porous interlayers to toughen liquid-molded fabric-based composites |
| DE102004006615B4 (de) | 2004-02-10 | 2016-03-31 | Airbus Helicopters Deutschland GmbH | Verfahren zur Herstellung eines Faserverbundwerkstoff-Hohlbauteils sowie Zwischenprodukt dafür |
| US7527222B2 (en) * | 2004-04-06 | 2009-05-05 | The Boeing Company | Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
| JP4826176B2 (ja) * | 2005-08-31 | 2011-11-30 | 東レ株式会社 | 強化繊維プリフォームおよびrtm成形方法 |
| US7824171B2 (en) * | 2005-10-31 | 2010-11-02 | The Boeing Company | Corner-consolidating inflatable apparatus and method for manufacturing composite structures |
| WO2008092971A1 (es) * | 2007-01-30 | 2008-08-07 | Airbus España, S.L. | Estructura de material compuesto para fuselaje de aeronave y su procedimiento de fabricación |
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2007
- 2007-12-13 DE DE102007060029A patent/DE102007060029A1/de not_active Ceased
-
2008
- 2008-11-12 EP EP08860048.1A patent/EP2229273B1/de not_active Not-in-force
- 2008-11-12 CN CN200880120453.0A patent/CN101896329B/zh not_active Expired - Fee Related
- 2008-11-12 RU RU2010122662/05A patent/RU2488488C2/ru not_active IP Right Cessation
- 2008-11-12 CA CA2707802A patent/CA2707802A1/en not_active Abandoned
- 2008-11-12 BR BRPI0821246-5A patent/BRPI0821246A2/pt not_active IP Right Cessation
- 2008-11-12 JP JP2010537352A patent/JP2011506136A/ja active Pending
- 2008-11-12 WO PCT/EP2008/065355 patent/WO2009074419A1/de not_active Ceased
-
2010
- 2010-06-04 US US12/794,487 patent/US20100276069A1/en not_active Abandoned
-
2014
- 2014-05-23 US US14/285,704 patent/US9180628B2/en not_active Expired - Fee Related
-
2015
- 2015-10-30 US US14/928,389 patent/US20160129647A1/en not_active Abandoned
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| US2739350A (en) * | 1952-01-28 | 1956-03-27 | Northrop Aircraft Inc | Method and means of molding |
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Also Published As
| Publication number | Publication date |
|---|---|
| CA2707802A1 (en) | 2009-06-18 |
| BRPI0821246A2 (pt) | 2015-06-16 |
| CN101896329A (zh) | 2010-11-24 |
| US20100276069A1 (en) | 2010-11-04 |
| US20160129647A1 (en) | 2016-05-12 |
| US20140346715A1 (en) | 2014-11-27 |
| CN101896329B (zh) | 2014-04-09 |
| WO2009074419A1 (de) | 2009-06-18 |
| EP2229273A1 (de) | 2010-09-22 |
| RU2010122662A (ru) | 2012-01-20 |
| EP2229273B1 (de) | 2016-01-27 |
| US9180628B2 (en) | 2015-11-10 |
| DE102007060029A1 (de) | 2009-06-18 |
| JP2011506136A (ja) | 2011-03-03 |
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| MM4A | The patent is invalid due to non-payment of fees |
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