DE69331245D1 - Verfahren zur Consolidierung/gleichzeitigen Herstellung von mehreren Verbundstoffen - Google Patents
Verfahren zur Consolidierung/gleichzeitigen Herstellung von mehreren VerbundstoffenInfo
- Publication number
- DE69331245D1 DE69331245D1 DE69331245T DE69331245T DE69331245D1 DE 69331245 D1 DE69331245 D1 DE 69331245D1 DE 69331245 T DE69331245 T DE 69331245T DE 69331245 T DE69331245 T DE 69331245T DE 69331245 D1 DE69331245 D1 DE 69331245D1
- Authority
- DE
- Germany
- Prior art keywords
- consolidation
- composite materials
- simultaneous production
- several composite
- several
- 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 - Fee Related
Links
- 239000002131 composite material Substances 0.000 title 1
- 238000007596 consolidation process Methods 0.000 title 1
- 238000000034 method Methods 0.000 title 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/02—Pretreatment of the fibres or filaments
- C22C47/06—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element
- C22C47/062—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element from wires or filaments only
- C22C47/068—Aligning wires
-
- 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
-
- 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
- B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
- B32B3/08—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions characterised by added members at particular parts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/30—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer formed with recesses or projections, e.g. hollows, grooves, protuberances, ribs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B38/06—Embossing
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/02—Pretreatment of the fibres or filaments
- C22C47/06—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element
- C22C47/062—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element from wires or filaments only
- C22C47/064—Winding wires
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/20—Making alloys containing metallic or non-metallic fibres or filaments by subjecting to pressure and heat an assembly comprising at least one metal layer or sheet and one layer of fibres or filaments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/10—Sintering only
- B22F2003/1042—Sintering only with support for articles to be sintered
- B22F2003/1046—Sintering only with support for articles to be sintered with separating means for articles to be sintered
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2309/00—Parameters for the laminating or treatment process; Apparatus details
- B32B2309/08—Dimensions, e.g. volume
- B32B2309/10—Dimensions, e.g. volume linear, e.g. length, distance, width
- B32B2309/105—Thickness
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49789—Obtaining plural product pieces from unitary workpiece
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4981—Utilizing transitory attached element or associated separate material
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Composite Materials (AREA)
- Textile Engineering (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Laminated Bodies (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/943,736 US5337940A (en) | 1990-12-11 | 1992-09-11 | Composite preform and method of manufacturing fiber reinforced composite |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69331245D1 true DE69331245D1 (de) | 2002-01-10 |
DE69331245T2 DE69331245T2 (de) | 2002-07-11 |
Family
ID=25480178
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69331245T Expired - Fee Related DE69331245T2 (de) | 1992-09-11 | 1993-09-10 | Verfahren zur Consolidierung/gleichzeitigen Herstellung von mehreren Verbundstoffen |
DE69325424T Expired - Fee Related DE69325424T2 (de) | 1992-09-11 | 1993-09-10 | Verbundwerkstoff Vorform und Verfahren zur Herstellung eines faserverstärkten Verbundwerkstoffes |
DE69331350T Expired - Fee Related DE69331350T2 (de) | 1992-09-11 | 1993-09-10 | Verfahren zur Herstellung eines Prefabrikats für einen kreisförmigen Metallverbundwerkstoffs |
Family Applications After (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69325424T Expired - Fee Related DE69325424T2 (de) | 1992-09-11 | 1993-09-10 | Verbundwerkstoff Vorform und Verfahren zur Herstellung eines faserverstärkten Verbundwerkstoffes |
DE69331350T Expired - Fee Related DE69331350T2 (de) | 1992-09-11 | 1993-09-10 | Verfahren zur Herstellung eines Prefabrikats für einen kreisförmigen Metallverbundwerkstoffs |
Country Status (4)
Country | Link |
---|---|
US (2) | US5337940A (de) |
EP (3) | EP0587438B1 (de) |
JP (1) | JP3492731B2 (de) |
DE (3) | DE69331245T2 (de) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2713662B1 (fr) * | 1993-12-08 | 1996-01-12 | Snecma | Procédé d'obtention d'une pièce circulaire métallique renforcée par des fibres. |
US5624516A (en) * | 1994-12-20 | 1997-04-29 | Atlantic Research Corporation | Methods of making preforms for composite material manufacture |
GB9619890D0 (en) * | 1996-09-24 | 1996-11-06 | Rolls Royce Plc | A method of making a fibre reinforced metal component |
US6077066A (en) | 1996-11-22 | 2000-06-20 | Atlantic Research Corporation | Tooling apparatus for composite fabrication |
SE511439C2 (sv) | 1997-06-16 | 1999-09-27 | Amal Ab | Förfarande för åstadkommande av en böjstyv, långsträckt kropp samt en anordning vid en böjstyv, långsträckt kropp |
ATE322560T1 (de) * | 1999-11-04 | 2006-04-15 | Avio Spa | Verfahren zur herstellung eines bauteiles aus verbundwerkstoff |
WO2002022296A2 (en) | 2000-09-11 | 2002-03-21 | Allison Advanced Development Company | Mechanically grooved sheet and method of manufacture |
US6465110B1 (en) | 2000-10-10 | 2002-10-15 | Material Sciences Corporation | Metal felt laminate structures |
GB0119636D0 (en) | 2001-08-11 | 2001-10-03 | Rolls Royce Plc | a method of manufacturing a fibre reinforced metal component |
DE10326818B4 (de) * | 2003-06-15 | 2007-07-05 | Mtu Aero Engines Gmbh | Verbundwerkstoff, Verfahren zur Herstellung eines Verbundwerkstoffs und Verwendung desselben |
DE10348506A1 (de) * | 2003-10-18 | 2005-05-12 | Mtu Aero Engines Gmbh | Verbundwerkstoff, Verfahren zur Herstellung eines Verbundwerkstoffs und Verwendung desselben |
GB0324810D0 (en) * | 2003-10-24 | 2003-11-26 | Rolls Royce Plc | A method of manufacturing a fibre reinforced metal matrix composite article |
GB0327044D0 (en) * | 2003-11-18 | 2004-04-07 | Rolls Royce Plc | A method of manufacturing a fibre reinforced metal matrix composite article and a cassette for use therein |
DE10357658B4 (de) * | 2003-12-10 | 2010-09-09 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung eines Halbzeugs aus Verbundwerkstoff |
US20060107516A1 (en) * | 2004-11-24 | 2006-05-25 | Touchstone Research Laboratory, Ltd. | Intermittently connected metal matrix composite bars |
US7842375B2 (en) * | 2005-05-17 | 2010-11-30 | Rolls-Royce Corporation | Fiber retention system for metal matrix composite preform |
US7735714B2 (en) * | 2005-05-18 | 2010-06-15 | Midgett Steven G | Composite metal tube and ring and a process for producing a composite metal tube and ring |
FR2919284B1 (fr) * | 2007-07-26 | 2010-09-24 | Snecma | Piece mecanique comportant un insert en materiau composite. |
US8281907B2 (en) | 2007-12-03 | 2012-10-09 | Honeywell International Inc. | Brake assembly having multi-piece core and replaceable friction surfaces |
CN101314839B (zh) * | 2008-06-13 | 2010-04-21 | 哈尔滨工业大学 | 一种连续纤维增强金属基复合材料的补强方法 |
FR2933422B1 (fr) * | 2008-07-04 | 2011-05-13 | Messier Dowty Sa | Procede de fabrication d'une piece metallique comportant des renforts internes formes de fibres ceramiques |
JP5458804B2 (ja) * | 2009-10-26 | 2014-04-02 | トヨタ紡織株式会社 | プレス方法及びプレス装置 |
FR2953859B1 (fr) * | 2009-12-16 | 2013-12-20 | Snecma | Procede de fabrication d'un insert de forme droite en materiau composite a matrice metallique |
US9090043B2 (en) | 2011-08-03 | 2015-07-28 | The Boeing Company | Molybdenum composite hybrid laminates and methods |
US8878072B2 (en) * | 2012-06-19 | 2014-11-04 | Lockheed Martin Corporation | High reliability fluid-tight low-profile electrically conductive interconnects for large scale frame attachment |
US9258907B2 (en) | 2012-08-09 | 2016-02-09 | Lockheed Martin Corporation | Conformal 3D non-planar multi-layer circuitry |
WO2014092710A1 (en) * | 2012-12-13 | 2014-06-19 | Empire Technology Development Llc | Lightweight structural materials |
US8772745B1 (en) | 2013-03-14 | 2014-07-08 | Lockheed Martin Corporation | X-ray obscuration film and related techniques |
US10123410B2 (en) | 2014-10-10 | 2018-11-06 | Lockheed Martin Corporation | Fine line 3D non-planar conforming circuit |
JP6551059B2 (ja) * | 2015-08-27 | 2019-07-31 | 国立研究開発法人物質・材料研究機構 | SiC繊維を含むハイブリッド複合材料およびその製造方法 |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE315253C (de) * | ||||
DE280518C (de) * | 1913-05-23 | 1900-01-01 | ||
US2269523A (en) * | 1937-05-31 | 1942-01-13 | Ellis Miller | Process for cladding metals and the product thereof |
US3201862A (en) * | 1960-12-28 | 1965-08-24 | Gotoh Kazuo | Process for making steel-reinforced aluminum members |
US3419952A (en) * | 1966-09-12 | 1969-01-07 | Gen Electric | Method for making composite material |
NL6813191A (de) * | 1968-09-14 | 1970-03-17 | ||
US3551996A (en) * | 1969-08-14 | 1971-01-05 | Harvey Aluminum Inc | Process for the production of aluminum-steel composite |
US3936550A (en) * | 1971-04-12 | 1976-02-03 | General Electric Company | Composite metallic preform tape |
US3915781A (en) * | 1974-02-28 | 1975-10-28 | United Technologies Corp | Resin bonded composite articles and process for fabrication thereof |
CA1079011A (en) * | 1976-12-17 | 1980-06-10 | Karl M. Prewo | Quick bond composite and process |
US4217157A (en) * | 1978-11-20 | 1980-08-12 | United Technologies Corporation | Method of fabricating fiber-reinforced articles |
DE2916299A1 (de) * | 1979-04-21 | 1980-10-23 | Messerschmitt Boelkow Blohm | Verfahren zum herstellen eines verbundwerkstoffes |
US4697324A (en) * | 1984-12-06 | 1987-10-06 | Avco Corporation | Filamentary structural module for composites |
US4746054A (en) * | 1985-08-29 | 1988-05-24 | Northrop Corporation | Method of joining concentric cylinders |
GB8602003D0 (en) * | 1986-01-28 | 1986-03-05 | Lawton P G | Carbonisable fibre assembly |
US4782992A (en) * | 1986-11-21 | 1988-11-08 | Textron Inc. | Method of forming articles |
US4896815A (en) * | 1987-05-29 | 1990-01-30 | Avco Lycoming | Method for forming titanium aluminide-ductile titanium aluminum alloy matrix composites |
JPH01165948A (ja) * | 1987-12-22 | 1989-06-29 | Hideyuki Nishizawa | 電気泳動用繊維強化ゲルの作成装置 |
US5184769A (en) * | 1989-07-26 | 1993-02-09 | Avco Corporation | Tooling and method for consolidating a filamentary reinforced metal matrix composite |
US5431984A (en) * | 1990-12-11 | 1995-07-11 | Avco Corporation | Composite preforms with groves for fibers and groves for off-gassing |
-
1992
- 1992-09-11 US US07/943,736 patent/US5337940A/en not_active Expired - Lifetime
-
1993
- 1993-09-09 JP JP24733493A patent/JP3492731B2/ja not_active Expired - Fee Related
- 1993-09-10 DE DE69331245T patent/DE69331245T2/de not_active Expired - Fee Related
- 1993-09-10 EP EP93307151A patent/EP0587438B1/de not_active Expired - Lifetime
- 1993-09-10 EP EP98203916A patent/EP0909826B1/de not_active Expired - Lifetime
- 1993-09-10 EP EP98203915A patent/EP0909825B1/de not_active Expired - Lifetime
- 1993-09-10 DE DE69325424T patent/DE69325424T2/de not_active Expired - Fee Related
- 1993-09-10 DE DE69331350T patent/DE69331350T2/de not_active Expired - Fee Related
-
1994
- 1994-05-31 US US08/251,534 patent/US5427304A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE69325424T2 (de) | 1999-12-09 |
EP0587438B1 (de) | 1999-06-23 |
US5337940A (en) | 1994-08-16 |
EP0909825B1 (de) | 2001-11-28 |
EP0909826A1 (de) | 1999-04-21 |
JPH06212315A (ja) | 1994-08-02 |
DE69331350D1 (de) | 2002-01-24 |
JP3492731B2 (ja) | 2004-02-03 |
DE69331350T2 (de) | 2002-08-08 |
DE69331245T2 (de) | 2002-07-11 |
EP0587438A1 (de) | 1994-03-16 |
EP0909826B1 (de) | 2001-12-12 |
EP0909825A1 (de) | 1999-04-21 |
DE69325424D1 (de) | 1999-07-29 |
US5427304A (en) | 1995-06-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |