DE69807545D1 - Verfahren zur Herstellung von Hohlkörpern aus Verbundmaterial - Google Patents
Verfahren zur Herstellung von Hohlkörpern aus VerbundmaterialInfo
- Publication number
- DE69807545D1 DE69807545D1 DE69807545T DE69807545T DE69807545D1 DE 69807545 D1 DE69807545 D1 DE 69807545D1 DE 69807545 T DE69807545 T DE 69807545T DE 69807545 T DE69807545 T DE 69807545T DE 69807545 D1 DE69807545 D1 DE 69807545D1
- Authority
- DE
- Germany
- Prior art keywords
- production
- composite material
- hollow bodies
- bodies
- hollow
- 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
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
- B29C70/44—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
- 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
- B29C33/52—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 soluble or fusible
-
- 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
- B29C70/342—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 isostatic pressure
-
- 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
- B29C2791/00—Shaping characteristics in general
- B29C2791/001—Shaping in several steps
-
- 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
- B29C33/3828—Moulds made of at least two different materials having different thermal conductivities
-
- 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
- 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
- B29C33/448—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 destructible
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0012—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular thermal properties
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S264/00—Plastic and nonmetallic article shaping or treating: processes
- Y10S264/44—Plastic and nonmetallic article shaping or treating: processes using destructible molds or cores in molding processes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9702664A FR2760399B1 (fr) | 1997-03-06 | 1997-03-06 | Procede de fabrication de pieces creuses en materiau composite |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69807545D1 true DE69807545D1 (de) | 2002-10-10 |
DE69807545T2 DE69807545T2 (de) | 2003-04-24 |
Family
ID=9504472
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69807545T Expired - Lifetime DE69807545T2 (de) | 1997-03-06 | 1998-03-05 | Verfahren zur Herstellung von Hohlkörpern aus Verbundmaterial |
Country Status (8)
Country | Link |
---|---|
US (1) | US6264868B1 (de) |
EP (1) | EP0862978B1 (de) |
JP (1) | JP2000514742A (de) |
CA (1) | CA2254091C (de) |
DE (1) | DE69807545T2 (de) |
ES (1) | ES2183296T3 (de) |
FR (1) | FR2760399B1 (de) |
WO (1) | WO1998039151A1 (de) |
Families Citing this family (34)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6174484B1 (en) | 1998-11-16 | 2001-01-16 | General Electric Company | Apparatus and method for producing a compression molded product |
DE19956170A1 (de) * | 1999-11-23 | 2001-05-31 | Mann & Hummel Filter | Kernausschmelzverfahren zur Herstellung einer Hohlraumstruktur |
FR2818578B1 (fr) * | 2000-12-26 | 2003-03-21 | Snecma Moteurs | Procede de fabrication de structures en nid d'abeilles et outillage pour une telle fabrication |
US6921503B1 (en) * | 2002-12-02 | 2005-07-26 | Foam Matrix, Inc. | Lost foam molding |
ATE409565T1 (de) * | 2004-02-13 | 2008-10-15 | Saab Ab | Verfahren zur herstellung eines gegenstands aus verbundwerkstoff |
DE102004009744B4 (de) * | 2004-02-25 | 2009-06-18 | Eurocopter Deutschland Gmbh | Verfahren zur Herstellung eines Formkerns |
US7638084B2 (en) * | 2004-03-19 | 2009-12-29 | Frankel Kenneth A | Methods for forming fiber reinforced composite parts having one or more selectively positioned core, structural insert, or veneer pieces integrally associated therewith |
US7588655B2 (en) * | 2004-11-24 | 2009-09-15 | The Boeing Company | Mandrel with differential in thermal expansion to eliminate wrinkles in ply |
US7357166B2 (en) * | 2004-11-24 | 2008-04-15 | The Boeing Company | Flexible mandrel for highly contoured composite stringer |
ES2313230T3 (es) * | 2005-12-20 | 2009-03-01 | Saab Ab | Procedimiento de fabricacion de un articulo integral que consta de un material compuesto reforzado con fibras, yh un conjunto de herramientas para la fabricacion del mismo. |
US9314941B2 (en) * | 2007-07-13 | 2016-04-19 | Advanced Ceramics Manufacturing, Llc | Aggregate-based mandrels for composite part production and composite part production methods |
JP5178221B2 (ja) * | 2008-01-31 | 2013-04-10 | 倉敷化工株式会社 | 成形用中空部材の製造方法 |
DE102008013759B4 (de) * | 2008-03-12 | 2012-12-13 | Airbus Operations Gmbh | Verfahren zur Herstellung eines integralen Faserverbundbauteils sowie Kernform zur Durchführung des Verfahrens |
RU2456157C1 (ru) * | 2011-03-16 | 2012-07-20 | Закрытое акционерное общество "Комплексный технический сервис" | Способ изготовления полимерной оснастки по моделям |
US8631671B2 (en) * | 2011-04-14 | 2014-01-21 | GM Global Technology Operations LLC | Internal mandrel and method |
DE102011116656B3 (de) * | 2011-10-21 | 2013-01-17 | Daimler Ag | Druckgastank und Fertigungsverfahren für selbigen |
US9126355B2 (en) * | 2012-05-02 | 2015-09-08 | Spirit Aerosystems, Inc. | Composite material part manufacturing process using removable and retainable material |
US9481136B2 (en) * | 2012-10-31 | 2016-11-01 | The Boeing Company | Over-molded vacuum barrier and inner mold line bag carrier with soluble details in trapped closed mold tooling |
ITTO20130871A1 (it) * | 2013-10-29 | 2015-04-30 | Alenia Aermacchi Spa | Metodo per la realizzazione di strutture cave di rinforzo intersecanti fra loro. |
US9827710B2 (en) * | 2014-02-04 | 2017-11-28 | The Boeing Company | Radius filler and method of manufacturing same |
CN103909661B (zh) * | 2014-04-15 | 2017-02-15 | 江苏恒神股份有限公司 | 方舱副车架用梁模具制造方法及所得模具 |
CN104175568B (zh) * | 2014-07-18 | 2017-10-31 | 威海光威复合材料股份有限公司 | 制造混凝土泵车用碳纤维臂架的生产方法 |
DE102014217042A1 (de) * | 2014-08-27 | 2016-04-21 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zur Herstellung eines Hohlbauteils aus faserverstärktem Kunststoff |
US10449734B2 (en) * | 2014-09-18 | 2019-10-22 | Alenia Aermacchi S.P.A. | Methods for manufacturing elongated structural elements of composite material |
EP3034263A1 (de) | 2014-12-19 | 2016-06-22 | Sadair Spear AB | Verfahren zur Herstellung faserverstärkter Strukturen, Dorn, Formsystem und faserverstärkte Struktur |
DE102016103979A1 (de) | 2016-03-04 | 2017-09-07 | KTM Technologies GmbH | Verfahren zur Herstellung eines faserverstärkten Strukturhohlbauteils sowie Strukturhohlbauteil |
DE102016103977A1 (de) * | 2016-03-04 | 2017-09-07 | KTM Technologies GmbH | Formkern mit Expansionsmaterial |
JP6504269B2 (ja) * | 2016-10-31 | 2019-04-24 | 三菱ケミカル株式会社 | 繊維強化プラスチック成形体の製造方法 |
DE102016124061A1 (de) | 2016-12-12 | 2018-06-14 | KTM Technologies GmbH | Verlorener Formkern sowie ein Verfahren zur Herstellung eines Bauteils und das Bauteil selbst |
CN107096882B (zh) * | 2017-06-13 | 2023-03-21 | 柳州智云科技有限公司 | 基于3d打印的铸造用模具及该模具的制备方法 |
JP7128700B2 (ja) * | 2018-09-20 | 2022-08-31 | 株式会社Subaru | 繊維強化樹脂構造体 |
CN111873478B (zh) * | 2020-07-30 | 2022-03-25 | 航天特种材料及工艺技术研究所 | 一种成型工装及利用该成型工装制备矩形中空复合材料管状构件的方法 |
CN112571836B (zh) * | 2020-11-27 | 2022-10-11 | 长春长光宇航复合材料有限公司 | 预埋金属件闭腔网格框架结构复合材料的制备方法 |
DE102020134901A1 (de) * | 2020-12-23 | 2022-06-23 | Airbus Operations Gmbh | Formkern zur Herstellung eines Bauteils aus Faserverbundmaterial |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1050562A (de) * | 1900-01-01 | |||
US3094422A (en) * | 1959-12-21 | 1963-06-18 | Fonderie De Prec | Core elements |
US3795559A (en) * | 1971-10-01 | 1974-03-05 | Boeing Co | Aircraft fluted core radome and method for making the same |
US4202856A (en) * | 1977-09-30 | 1980-05-13 | Rockwell International Corporation | Graphite-epoxy molding method |
US4155970A (en) * | 1977-11-04 | 1979-05-22 | Mcdonnell Douglas Corporation | Method for making a hollow composite using a destructible core |
US4167430A (en) * | 1978-04-28 | 1979-09-11 | General Dynamics Corporation | Method for fabricating a composite bonded structure |
FR2440831A1 (fr) * | 1978-11-07 | 1980-06-06 | Dassault Avions | Panneaux a base de fibres a haute resistance, particulierement applicables a la construction des avions |
GB2067455A (en) * | 1979-02-20 | 1981-07-30 | Rolls Royce | Composite structure |
US4424183A (en) * | 1982-07-06 | 1984-01-03 | Baker International Corporation | Destructible core structure and method for using same |
US4614627A (en) * | 1982-10-05 | 1986-09-30 | Dunlop Limited | Method of injection molding a thermoplastic hollow or hollow foam filled one piece head of a golf club |
US4615855A (en) * | 1984-03-15 | 1986-10-07 | Programmed Composites, Inc. | Process for forming composite article |
FR2562834B1 (fr) * | 1984-04-12 | 1987-01-02 | Ranjon Marc | Procede de fabrication de pieces resistantes creuses, notamment de portions d'aeronefs ou d'engins, et pieces ainsi obtenues |
GB2173144B (en) * | 1985-04-02 | 1989-08-09 | Rolls Royce Plc | Moulding of composite materials |
US4681724A (en) * | 1986-04-28 | 1987-07-21 | United Technologies Corporation | Removable irreversibly shrinking male mandrel |
JPS63147605A (ja) * | 1986-07-28 | 1988-06-20 | 株式会社日立製作所 | スリツプキヤステイング用鋳型の製作法及びスリツプキヤステイング成形方法 |
US4812115A (en) * | 1987-10-05 | 1989-03-14 | Dow Corning Corporation | Fixed-volume trapped rubber molding apparatus |
DE3820574A1 (de) * | 1988-06-16 | 1989-12-21 | Agia Ag Fuer Ind Anwendungstec | Verlorener formkern |
CA2025826C (en) * | 1990-03-05 | 1997-08-05 | Borden, Inc. | Method for easy removal of sand cores from castings |
US5262100A (en) * | 1990-07-11 | 1993-11-16 | Advanced Plastics Partnership | Method of core removal from molded products |
US5248552A (en) * | 1990-07-11 | 1993-09-28 | Advanced Plastics Partnership | Molding core |
CA2056330C (en) * | 1990-12-19 | 2003-06-10 | Alexander C. Dublinski | Method of fabricating a complex part made of composite material |
US5131834A (en) * | 1990-12-21 | 1992-07-21 | Northrop Corporation | Silicone gel isostatic pressurizing bag and method of use and manufacture |
US5125993A (en) * | 1991-07-25 | 1992-06-30 | E. I. Du Pont De Nemours And Company | Method for forming and consolidating a fiber reinforced resin structure |
US5292475A (en) * | 1992-03-06 | 1994-03-08 | Northrop Corporation | Tooling and process for variability reduction of composite structures |
US5817269A (en) * | 1996-10-25 | 1998-10-06 | The Boeing Company | Composite fabrication method and tooling to improve part consolidation |
-
1997
- 1997-03-06 FR FR9702664A patent/FR2760399B1/fr not_active Expired - Fee Related
-
1998
- 1998-03-05 DE DE69807545T patent/DE69807545T2/de not_active Expired - Lifetime
- 1998-03-05 JP JP10538239A patent/JP2000514742A/ja active Pending
- 1998-03-05 US US09/180,276 patent/US6264868B1/en not_active Expired - Lifetime
- 1998-03-05 EP EP98400520A patent/EP0862978B1/de not_active Expired - Lifetime
- 1998-03-05 CA CA002254091A patent/CA2254091C/fr not_active Expired - Fee Related
- 1998-03-05 ES ES98400520T patent/ES2183296T3/es not_active Expired - Lifetime
- 1998-03-05 WO PCT/FR1998/000433 patent/WO1998039151A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
EP0862978B1 (de) | 2002-09-04 |
EP0862978A1 (de) | 1998-09-09 |
US6264868B1 (en) | 2001-07-24 |
ES2183296T3 (es) | 2003-03-16 |
CA2254091A1 (fr) | 1998-09-11 |
FR2760399B1 (fr) | 1999-05-07 |
CA2254091C (fr) | 2003-12-02 |
FR2760399A1 (fr) | 1998-09-11 |
DE69807545T2 (de) | 2003-04-24 |
WO1998039151A1 (fr) | 1998-09-11 |
JP2000514742A (ja) | 2000-11-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |