RU94004999A - METHOD OF MANUFACTURING A DETAIL FROM A COMPOSITION MATERIAL - Google Patents
METHOD OF MANUFACTURING A DETAIL FROM A COMPOSITION MATERIALInfo
- Publication number
- RU94004999A RU94004999A RU94004999/33A RU94004999A RU94004999A RU 94004999 A RU94004999 A RU 94004999A RU 94004999/33 A RU94004999/33 A RU 94004999/33A RU 94004999 A RU94004999 A RU 94004999A RU 94004999 A RU94004999 A RU 94004999A
- Authority
- RU
- Russia
- Prior art keywords
- workpiece
- fibers
- core
- needles
- plating layers
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title claims 3
- 238000004519 manufacturing process Methods 0.000 title claims 2
- 239000000835 fiber Substances 0.000 claims 4
- 238000007747 plating Methods 0.000 claims 2
- 238000005056 compaction Methods 0.000 claims 1
- 230000000875 corresponding Effects 0.000 claims 1
- 238000004080 punching Methods 0.000 claims 1
Claims (1)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9301767 | 1993-02-17 | ||
FR9301767A FR2701665B1 (en) | 1993-02-17 | 1993-02-17 | Method for manufacturing a part made of composite material, in particular a sandwich panel, from several assembled preforms. |
Publications (2)
Publication Number | Publication Date |
---|---|
RU94004999A true RU94004999A (en) | 1995-10-20 |
RU2119872C1 RU2119872C1 (en) | 1998-10-10 |
Family
ID=9444130
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU94004999A RU2119872C1 (en) | 1993-02-17 | 1994-02-16 | Method for manufacture of part from composite material and method for manufacture of sandwich-type panel from composite material |
Country Status (12)
Country | Link |
---|---|
US (1) | US5490892A (en) |
EP (1) | EP0611741B1 (en) |
JP (1) | JP3719721B2 (en) |
AT (1) | ATE160334T1 (en) |
CA (1) | CA2115473C (en) |
DE (1) | DE69406815T2 (en) |
ES (1) | ES2110190T3 (en) |
FR (1) | FR2701665B1 (en) |
MX (1) | MX9401201A (en) |
NO (1) | NO180287C (en) |
RU (1) | RU2119872C1 (en) |
UA (1) | UA26925C2 (en) |
Families Citing this family (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2746388B1 (en) * | 1996-03-19 | 1998-06-05 | Aerospatiale | METHOD FOR MANUFACTURING A HONEYCOMB-TYPE PANEL IN CARBON/CARBON OR CARBON/CERAMIC COMPOSITE AND STRUCTURES MADE FROM SUCH A PANEL |
US5749195A (en) * | 1996-12-10 | 1998-05-12 | Laventure; David | Sealing membrane and method of sealing |
JP3722188B2 (en) * | 1999-01-28 | 2005-11-30 | 石川島播磨重工業株式会社 | Ceramic matrix composite member and manufacturing method thereof |
US6261675B1 (en) | 1999-03-23 | 2001-07-17 | Hexcel Corporation | Core-crush resistant fabric and prepreg for fiber reinforced composite sandwich structures |
DE10246851C1 (en) * | 2002-10-08 | 2003-12-18 | Sgl Carbon Ag | Production of components made from a high temperature resistant fiber-reinforced composite ceramic comprises separating strips from neighboring strips in the region outside contact zones using a spacer made from graphite |
US20050158171A1 (en) * | 2004-01-15 | 2005-07-21 | General Electric Company | Hybrid ceramic matrix composite turbine blades for improved processibility and performance |
US20050236832A1 (en) * | 2004-04-22 | 2005-10-27 | Saxon, Inc. | Vehicle inventory sticker form |
US20070036958A1 (en) * | 2005-08-10 | 2007-02-15 | Agvantage, Inc. | Composite material with grain filler and method of making same |
JP4795062B2 (en) * | 2006-03-15 | 2011-10-19 | 有限会社泰成電機工業 | Plate-shaped object and method for manufacturing the same |
FR2921076B1 (en) * | 2007-09-18 | 2010-04-02 | Roy Guy Le | HIGH STRUCTURAL RESISTANCE PANEL, DEVICE AND METHOD FOR MANUFACTURING SUCH PANEL |
US8372498B2 (en) * | 2007-12-17 | 2013-02-12 | Sikorsky Aircraft Corporation | Composite core densification |
US20100196652A1 (en) * | 2009-02-03 | 2010-08-05 | Demien Jacquinet | Quasi-isotropic sandwich structures |
IT1393462B1 (en) * | 2009-03-23 | 2012-04-20 | Angelo Peruzza Di Paolo Peruzza & C S A S Ora A Peruzza S R L | FILM FOR THE PRODUCTION OF COMPOSITE MATERIALS, A PRODUCTION METHOD OF THAT FILM, AND A METHOD FOR THE PRODUCTION OF COMPOSITE MATERIALS USING THIS FILM |
FR2948693B1 (en) | 2009-07-28 | 2014-01-17 | Saertex France | METHOD FOR MAKING A SOUL WITH INTEGRATED PADING FIBERS FOR PANELS OF COMPOSITE MATERIALS, PANEL OBTAINED AND DEVICE |
WO2011012587A1 (en) * | 2009-07-28 | 2011-02-03 | Saertex Gmbh & Co. Kg | Process for the production of a core with integrated bridging fibers for panels made of composite materials, panel that is obtained and device |
FR2972448B1 (en) * | 2011-03-07 | 2013-04-19 | Commissariat Energie Atomique | PROCESS FOR PRODUCING A CERAMIC MATRIX COMPOSITE |
FR2989921B1 (en) * | 2012-04-27 | 2015-05-15 | Hexcel Reinforcements | USE IN THE MANUFACTURE OF A COMPOSITE PIECE OF A PENETRATION OPERATION FOR IMPROVING THE TRANSVERSE ELECTRICAL CONDUCTIVITY OF THE COMPOSITE PIECE |
US9527262B2 (en) * | 2012-09-28 | 2016-12-27 | General Electric Company | Layered arrangement, hot-gas path component, and process of producing a layered arrangement |
US9833930B2 (en) * | 2012-10-23 | 2017-12-05 | Albany Engineered Composites, Inc. | Circumferential stiffeners for composite fancases |
RU2544043C2 (en) * | 2012-10-25 | 2015-03-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" | Method of honeycomb structure manufacturing |
DK2922690T3 (en) * | 2012-11-20 | 2017-05-22 | Vestas Wind Sys As | Wind turbine blades and methods for making them |
FR3001452B1 (en) * | 2013-01-29 | 2015-02-13 | Herakles | METHOD OF MANUFACTURING A CURVED SHAPE ACOUSTICAL ATTENUATION PANEL |
RU2537307C1 (en) * | 2013-07-22 | 2014-12-27 | Анатолий Михайлович Мельников | Sandwich panel manufacturing method (versions) |
CN105531243B (en) | 2013-09-20 | 2018-01-16 | 通用电气公司 | The ceramic matrix composite and its manufacture method made by chemical vapor infiltration |
GB201402732D0 (en) * | 2014-02-17 | 2014-04-02 | Rolls Royce Plc | A honeycomb structure |
DE102014215964A1 (en) * | 2014-08-12 | 2016-02-18 | Bayerische Motoren Werke Aktiengesellschaft | Method for producing an SMC component provided with a unidirectional fiber layer |
FR3026675B1 (en) * | 2014-10-02 | 2016-11-11 | Mbda France | PROCESS FOR THE PRODUCTION OF A DOUBLE-WALL THERMOSTRUCTURAL COMPOSITE MONOLITHIC PIECE AND PART OBTAINED |
US10414142B2 (en) | 2014-12-29 | 2019-09-17 | Rolls-Royce Corporation | Needle punching of composites for preform assembly and thermomechanical enhancement |
FR3039147B1 (en) * | 2015-07-24 | 2017-08-25 | Aircelle Sa | ACOUSTICAL ATTENUATION PANEL IN CERAMIC OXIDE COMPOSITE MATERIAL WITH ELECTROCHIMICALLY CONVERTED METALLIC MATERIAL |
FR3056438B1 (en) | 2016-09-27 | 2019-11-01 | Coriolis Group | METHOD FOR PRODUCING COMPOSITE MATERIAL PARTS BY IMPREGNATING A PARTICULAR PREFORM |
RU175034U1 (en) * | 2016-12-21 | 2017-11-16 | федеральное государственное бюджетное образовательное учреждение высшего образования "Московский государственный технический университет имени Н.Э. Баумана (национальный исследовательский университет)" (МГТУ им. Н.Э. Баумана) | Scheme of a heat-shielding coating of a reusable heat shield of a descent vehicle for returning after a flight to the moon |
RU173721U1 (en) * | 2016-12-21 | 2017-09-07 | федеральное государственное бюджетное образовательное учреждение высшего образования "Московский государственный технический университет имени Н.Э. Баумана (национальный исследовательский университет)" (МГТУ им. Н.Э. Баумана) | Scheme of a heat-shielding coating of a reusable heat shield of a descent vehicle for returning from a low Earth orbit |
FR3070623B1 (en) * | 2017-09-04 | 2020-10-09 | Coriolis Composites | PROCESS FOR MAKING A PART IN COMPOSITE MATERIAL BY NEEDLING ORIENTED OF A PREFORM |
FR3084011B1 (en) * | 2018-07-17 | 2021-02-26 | Safran Ceram | METHOD OF MANUFACTURING AN ACCOUSTIC PANEL |
FR3089854B1 (en) * | 2018-12-18 | 2022-02-04 | Saint Gobain Performance Plastics France | METHOD FOR PREPARING A COMPOSITE MATERIAL IN THE FORM OF A SANDWICH |
EP3674081B1 (en) * | 2018-12-31 | 2022-02-23 | Ansaldo Energia Switzerland AG | High-temperature resistant tiles and manufacturing method thereof |
IT202100009203A1 (en) | 2021-04-13 | 2022-10-13 | Humanfactorx S R L Start Up Costituita A Norma Dellart 4C Legge 24 Gennaio 15 | PADDED |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3895084A (en) * | 1972-03-28 | 1975-07-15 | Ducommun Inc | Fiber reinforced composite product |
GB1387868A (en) * | 1972-06-30 | 1975-03-19 | Secr Defence | Reinforcement member |
US3994762A (en) * | 1972-07-21 | 1976-11-30 | Hyfil Limited | Carbon fiber composites |
US3900650A (en) * | 1973-02-08 | 1975-08-19 | James W Sedore | Fibrillar locking system |
GB1590827A (en) * | 1977-09-28 | 1981-06-10 | British United Shoe Machinery | Sheet materials and themanufacture thereof |
FR2446175A1 (en) * | 1979-01-09 | 1980-08-08 | Europ Propulsion | REINFORCED LAMINATED TEXTURE |
FR2493304A1 (en) * | 1980-10-30 | 1982-05-07 | Europ Propulsion | PROCESS FOR ASSEMBLING REFRACTORY PARTS |
US4335176A (en) * | 1980-11-24 | 1982-06-15 | Ppg Industries, Inc. | Bonded needled fiber glass thermoplastic reinforced mats |
US4790052A (en) * | 1983-12-28 | 1988-12-13 | Societe Europeenne De Propulsion | Process for manufacturing homogeneously needled three-dimensional structures of fibrous material |
FR2584106B1 (en) * | 1985-06-27 | 1988-05-13 | Europ Propulsion | METHOD FOR MANUFACTURING THREE-DIMENSIONAL STRUCTURES BY NEEDLEING PLANE LAYERS OF SUPERIMPOSED FIBROUS MATERIAL AND FIBROUS MATERIAL USED FOR THE IMPLEMENTATION OF THE PROCESS |
US5041321A (en) * | 1984-11-02 | 1991-08-20 | The Boeing Company | Fiberformed ceramic insulation and method |
US4983451A (en) * | 1987-08-05 | 1991-01-08 | Kabushiki Kaisha Kobe Seiko Sho | Carbon fiber-reinforced carbon composite material and process for producing the same |
FR2660591B1 (en) * | 1990-04-09 | 1992-08-14 | Europ Propulsion | PROCESS FOR CONFORMING PREFORMS FOR THE MANUFACTURE OF PARTS OF THERMOSTRUCTURAL COMPOSITE MATERIAL, PARTICULARLY OF PARTS IN THE FORM OF SAILS OR PANELS. |
FR2691923B1 (en) * | 1992-06-04 | 1994-09-09 | Europ Propulsion | Honeycomb structure in thermostructural composite material and its manufacturing process. |
-
1993
- 1993-02-17 FR FR9301767A patent/FR2701665B1/en not_active Expired - Fee Related
-
1994
- 1994-02-09 ES ES94400273T patent/ES2110190T3/en not_active Expired - Lifetime
- 1994-02-09 AT AT94400273T patent/ATE160334T1/en not_active IP Right Cessation
- 1994-02-09 DE DE69406815T patent/DE69406815T2/en not_active Expired - Fee Related
- 1994-02-09 EP EP94400273A patent/EP0611741B1/en not_active Expired - Lifetime
- 1994-02-11 CA CA002115473A patent/CA2115473C/en not_active Expired - Fee Related
- 1994-02-15 US US08/197,638 patent/US5490892A/en not_active Expired - Fee Related
- 1994-02-16 RU RU94004999A patent/RU2119872C1/en not_active IP Right Cessation
- 1994-02-16 MX MX9401201A patent/MX9401201A/en not_active IP Right Cessation
- 1994-02-16 NO NO940541A patent/NO180287C/en not_active IP Right Cessation
- 1994-02-16 UA UA94005094A patent/UA26925C2/en unknown
- 1994-02-17 JP JP02037594A patent/JP3719721B2/en not_active Expired - Fee Related
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