NO894096L - Fremgangsmaate for fremstilling av sammensatte komponentersom bestaar av et nett og en forsterkningsstruktur. - Google Patents
Fremgangsmaate for fremstilling av sammensatte komponentersom bestaar av et nett og en forsterkningsstruktur.Info
- Publication number
- NO894096L NO894096L NO89894096A NO894096A NO894096L NO 894096 L NO894096 L NO 894096L NO 89894096 A NO89894096 A NO 89894096A NO 894096 A NO894096 A NO 894096A NO 894096 L NO894096 L NO 894096L
- Authority
- NO
- Norway
- Prior art keywords
- blank
- consist
- net
- procedure
- profile
- Prior art date
Links
- 238000000034 method Methods 0.000 title abstract 2
- 238000004519 manufacturing process Methods 0.000 title 1
- 239000011230 binding agent Substances 0.000 abstract 2
- 230000002787 reinforcement Effects 0.000 abstract 2
- 239000002131 composite material Substances 0.000 abstract 1
- 238000005470 impregnation Methods 0.000 abstract 1
- 230000008595 infiltration Effects 0.000 abstract 1
- 238000001764 infiltration Methods 0.000 abstract 1
- 238000003754 machining Methods 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
- 239000011159 matrix material Substances 0.000 abstract 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/71—Ceramic products containing macroscopic reinforcing agents
- C04B35/78—Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
- C04B35/80—Fibres, filaments, whiskers, platelets, or the like
- C04B35/83—Carbon fibres in a carbon matrix
-
- 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
- B29C69/00—Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore
- B29C69/001—Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore a shaping technique combined with cutting, e.g. in parts or slices combined with rearranging and joining the cut parts
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
-
- 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
- B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
- B29C48/001—Combinations of extrusion moulding with other shaping operations
- B29C48/0011—Combinations of extrusion moulding with other shaping operations combined with compression 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
- B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
- B29C48/001—Combinations of extrusion moulding with other shaping operations
- B29C48/0017—Combinations of extrusion moulding with other shaping operations combined with blow-moulding or thermoforming
-
- 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
- B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
- B29C48/03—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
- B29C48/07—Flat, e.g. panels
-
- 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
- B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
- B29C48/03—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
- B29C48/07—Flat, e.g. panels
- B29C48/08—Flat, e.g. panels flexible, e.g. films
-
- 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
- B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
- B29C48/03—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
- B29C48/12—Articles with an irregular circumference when viewed in cross-section, e.g. window profiles
-
- 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
- B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
- B29C48/15—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor incorporating preformed parts or layers, e.g. extrusion moulding around inserts
-
- 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
-
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- 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
- Y10S427/00—Coating processes
- Y10S427/10—Chemical vapor infiltration, i.e. CVI
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Ceramic Engineering (AREA)
- Composite Materials (AREA)
- Combustion & Propulsion (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Engineering & Computer Science (AREA)
- Moulding By Coating Moulds (AREA)
- Nonwoven Fabrics (AREA)
- Reinforced Plastic Materials (AREA)
- Laminated Bodies (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Filtering Materials (AREA)
- Prostheses (AREA)
- Materials For Medical Uses (AREA)
- Woven Fabrics (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR8813590A FR2637838B1 (fr) | 1988-10-14 | 1988-10-14 | Procede de fabrication de pieces composites constituees d'un voile et d'un renfort |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| NO894096D0 NO894096D0 (no) | 1989-10-13 |
| NO894096L true NO894096L (no) | 1990-04-17 |
Family
ID=9371058
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NO89894096A NO894096L (no) | 1988-10-14 | 1989-10-13 | Fremgangsmaate for fremstilling av sammensatte komponentersom bestaar av et nett og en forsterkningsstruktur. |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US5034172A (no) |
| EP (1) | EP0364360B1 (no) |
| JP (1) | JPH02164781A (no) |
| AT (1) | ATE87260T1 (no) |
| DE (1) | DE68905564D1 (no) |
| FR (1) | FR2637838B1 (no) |
| NO (1) | NO894096L (no) |
| PT (1) | PT91977B (no) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2655364B1 (fr) * | 1989-12-01 | 1992-04-10 | Europ Propulsion | Procede de fabrication d'une piece en materiau composite, notamment a texture fibres de carbone ou refractaires et matrice carbone ou ceramique. |
| FR2659949B1 (fr) * | 1990-03-26 | 1992-12-04 | Europ Propulsion | Procede de conformation d'une texture fibreuse de renfort pour la fabrication d'une piece en materiau composite. |
| FR2660591B1 (fr) * | 1990-04-09 | 1992-08-14 | Europ Propulsion | Procede de conformation de preformes pour la fabrication de pieces en materiau composite thermostructural, notamment de pieces en forme de voiles ou panneaux. |
| FR2855557B1 (fr) * | 2003-05-26 | 2007-03-02 | Snecma Moteurs | Volet de tuyere a duree de vie augmentee pour turbomoteurs d'avion. |
| FR2873757B1 (fr) * | 2004-07-28 | 2006-09-29 | Snecma Moteurs Sa | Tuyere convergente de turboreacteur |
| US8642151B2 (en) | 2011-01-21 | 2014-02-04 | Albany Engineered Composites, Inc. | Preform and method for reinforcing woven fiber nodes |
| US9021813B2 (en) | 2011-07-18 | 2015-05-05 | The Boeing Company | Cable-actuated variable area fan nozzle with elastomeric seals |
| US10767863B2 (en) | 2015-07-22 | 2020-09-08 | Rolls-Royce North American Technologies, Inc. | Combustor tile with monolithic inserts |
| US11131206B2 (en) | 2018-11-08 | 2021-09-28 | Raytheon Technologies Corporation | Substrate edge configurations for ceramic coatings |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1947695A (en) * | 1930-09-10 | 1934-02-20 | Westinghouse Air Brake Co | Process of making flexible shaft couplings |
| US2781552A (en) * | 1955-10-21 | 1957-02-19 | Us Ceramic Tile Company | Process for making thin articles of polytetrafluoroethylene |
| FR2401888A1 (fr) * | 1977-09-06 | 1979-03-30 | Europ Propulsion | Piece poreuse carbonee densifiee in situ par depot chimique en phase vapeur de materiaux refractaires autres que le carbone et procede de fabrication |
| US4201611A (en) * | 1978-04-17 | 1980-05-06 | The United States Of America As Represented By The Secretary Of The Air Force | Carbon/carbon composite for re-entry vehicle applications |
| US4318955A (en) * | 1978-08-25 | 1982-03-09 | Kulakov Valery V | Method for making a carbonic friction product |
| US4353857A (en) * | 1980-02-01 | 1982-10-12 | Ford Motor Company | Method for making plastic panel and panel |
| US4490201A (en) * | 1981-08-10 | 1984-12-25 | The B. F. Goodrich Company | Method of fabricating carbon composites |
| US4489019A (en) * | 1981-12-22 | 1984-12-18 | Aisin Seiki Kabushiki Kaisha | Method for producing a longitudinal molding with nonuniform sections |
| FR2529257A1 (fr) * | 1982-06-28 | 1983-12-30 | Snecma | Volet de tuyere a structure composite carbone et acier |
| FR2565262B1 (fr) * | 1984-05-29 | 1986-09-26 | Europ Propulsion | Procede de fabrication d'une texture fibreuse multidirectionnelle et dispositif destine a la mise en oeuvre du procede |
| DE3527993C1 (de) * | 1985-08-03 | 1990-04-19 | Böhler AG, 4000 Düsseldorf | Verfahren zur Herstellung von Blattfedern sowie Formkoerper zur Durchfuehrung des Verfahrens |
| US4637550A (en) * | 1985-10-01 | 1987-01-20 | The United States Of America As Represented By The Secretary Of The Air Force | Dual material exhaust nozzle flap |
-
1988
- 1988-10-14 FR FR8813590A patent/FR2637838B1/fr not_active Expired - Fee Related
-
1989
- 1989-10-11 AT AT89402807T patent/ATE87260T1/de not_active IP Right Cessation
- 1989-10-11 DE DE8989402807T patent/DE68905564D1/de not_active Expired - Lifetime
- 1989-10-11 EP EP89402807A patent/EP0364360B1/fr not_active Expired - Lifetime
- 1989-10-11 US US07/420,051 patent/US5034172A/en not_active Expired - Fee Related
- 1989-10-13 PT PT91977A patent/PT91977B/pt not_active IP Right Cessation
- 1989-10-13 JP JP1265291A patent/JPH02164781A/ja active Pending
- 1989-10-13 NO NO89894096A patent/NO894096L/no unknown
Also Published As
| Publication number | Publication date |
|---|---|
| JPH02164781A (ja) | 1990-06-25 |
| EP0364360A1 (fr) | 1990-04-18 |
| US5034172A (en) | 1991-07-23 |
| ATE87260T1 (de) | 1993-04-15 |
| FR2637838B1 (fr) | 1991-01-25 |
| EP0364360B1 (fr) | 1993-03-24 |
| PT91977A (pt) | 1990-04-30 |
| NO894096D0 (no) | 1989-10-13 |
| DE68905564D1 (de) | 1993-04-29 |
| FR2637838A1 (fr) | 1990-04-20 |
| PT91977B (pt) | 1995-08-09 |
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