FR2336205A1 - Procede de fabrication d'articles composites resistant aux hautes temperatures - Google Patents
Procede de fabrication d'articles composites resistant aux hautes temperaturesInfo
- Publication number
- FR2336205A1 FR2336205A1 FR7626225A FR7626225A FR2336205A1 FR 2336205 A1 FR2336205 A1 FR 2336205A1 FR 7626225 A FR7626225 A FR 7626225A FR 7626225 A FR7626225 A FR 7626225A FR 2336205 A1 FR2336205 A1 FR 2336205A1
- Authority
- FR
- France
- Prior art keywords
- high temperatures
- composite articles
- manufacturing composite
- articles resistant
- resistant
- 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.)
- Granted
Links
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
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/282—Selecting composite materials, e.g. blades with reinforcing 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
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- 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
- B22F2999/00—Aspects linked to processes or compositions used in powder metallurgy
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49337—Composite blade
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Crystallography & Structural Chemistry (AREA)
- Composite Materials (AREA)
- General Engineering & Computer Science (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Powder Metallurgy (AREA)
- Laminated Bodies (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA242,605A CA1042641A (fr) | 1975-12-24 | 1975-12-24 | Fabrication d'elements composites pour aubes de turbines |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2336205A1 true FR2336205A1 (fr) | 1977-07-22 |
FR2336205B1 FR2336205B1 (fr) | 1982-03-26 |
Family
ID=4104849
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7626225A Granted FR2336205A1 (fr) | 1975-12-24 | 1976-08-31 | Procede de fabrication d'articles composites resistant aux hautes temperatures |
Country Status (6)
Country | Link |
---|---|
US (1) | US4060413A (fr) |
JP (1) | JPS5281061A (fr) |
CA (1) | CA1042641A (fr) |
DE (1) | DE2619235A1 (fr) |
FR (1) | FR2336205A1 (fr) |
GB (1) | GB1536748A (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2711330A1 (fr) * | 1993-10-19 | 1995-04-28 | Deutsche Forsch Luft Raumfahrt | Procédé de fabrication de composants armés de fibres longues. |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5547335A (en) * | 1978-09-27 | 1980-04-03 | Sumitomo Chem Co Ltd | Manufacturing method of fiber reinforced metal based composite material |
US4778110A (en) * | 1982-09-30 | 1988-10-18 | Rohr Industries, Inc. | Modular composite cascade assembly |
DE3873447T2 (de) * | 1987-08-21 | 1993-03-18 | Mitsubishi Materials Corp | Verfahren zur darstellung von supraleitenden materialien. |
US4861546A (en) * | 1987-12-23 | 1989-08-29 | Precision Castparts Corp. | Method of forming a metal article from powdered metal |
US5118257A (en) * | 1990-05-25 | 1992-06-02 | Sundstrand Corporation | Boot attachment for composite turbine blade, turbine blade and method of making turbine blade |
US5314309A (en) * | 1990-05-25 | 1994-05-24 | Anthony Blakeley | Turbine blade with metallic attachment and method of making the same |
DE4021547A1 (de) * | 1990-07-06 | 1992-01-16 | Deutsche Forsch Luft Raumfahrt | Verfahren zum herstellen von faserverstaerkten bauteilen |
DE4041104C1 (fr) * | 1990-12-21 | 1992-06-04 | Mtu Muenchen Gmbh | |
US5933703A (en) * | 1991-10-29 | 1999-08-03 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland | Process for the preparation of fibre reinforced metal matrix composites and novel preforms therefor |
US5579532A (en) * | 1992-06-16 | 1996-11-26 | Aluminum Company Of America | Rotating ring structure for gas turbine engines and method for its production |
US5405571A (en) * | 1992-06-16 | 1995-04-11 | Aluminum Company Of America | Tape casting fiber reinforced composite structures |
DE4335558A1 (de) * | 1993-10-19 | 1995-04-20 | Deutsche Forsch Luft Raumfahrt | Verfahren zum Herstellen von langfaserverstärkten Bauteilen |
US5592686A (en) * | 1995-07-25 | 1997-01-07 | Third; Christine E. | Porous metal structures and processes for their production |
US5960249A (en) * | 1998-03-06 | 1999-09-28 | General Electric Company | Method of forming high-temperature components and components formed thereby |
DE10157478A1 (de) * | 2001-11-23 | 2003-06-05 | Fne Gmbh | Metall-Verbundwerkstoff und Verfahren zur Herstellung eines Metall-Verbundwerkstoffs |
SG120941A1 (en) * | 2003-07-03 | 2006-04-26 | Agency Science Tech & Res | Double-layer metal sheet and method of fabricatingthe same |
WO2006019942A2 (fr) * | 2004-07-22 | 2006-02-23 | Integral Technologies, Inc. | Pompes exemptes de decharges electrostatiques economiques faites de resines chargees de materiaux conducteurs |
US20060073311A1 (en) * | 2004-10-05 | 2006-04-06 | The Boeing Company | Apparatus and method for composite tape profile cutting |
US7842145B2 (en) * | 2004-10-05 | 2010-11-30 | The Boeing Company | Method for laying composite tape |
US8318291B2 (en) * | 2005-09-07 | 2012-11-27 | The Boeing Company | Composite member defining a contour surface |
GB0718026D0 (en) * | 2007-09-15 | 2007-10-24 | Rolls Royce Plc | Joining method and a resultant article |
EP2570674A1 (fr) * | 2011-09-15 | 2013-03-20 | Sandvik Intellectual Property AB | Aube de rotor résistant à l'érosion consistant en un stratifié métallique |
CN102335747B (zh) * | 2011-11-02 | 2013-08-14 | 湖南航天诚远精密机械有限公司 | 铝碳化硅复合材料igbt基板的制备及镶嵌铝合金的方法 |
CN104372254B (zh) * | 2014-10-29 | 2017-01-25 | 重庆华孚粉末冶金有限公司 | 碳化硅颗粒增强铁基复合材料及其制备方法 |
CN107755668B (zh) * | 2017-09-20 | 2020-03-17 | 上海交通大学 | 制备增强镍基高温合金复合材料单晶叶片的方法 |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2262597A1 (fr) * | 1974-02-28 | 1975-09-26 | United Aircraft Corp |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3095642A (en) * | 1957-11-26 | 1963-07-02 | Owens Corning Fiberglass Corp | Metal and fiber composite materials and methods of producing |
US3293073A (en) * | 1964-02-12 | 1966-12-20 | Union Carbide Corp | Process for imparting wash and wear properties to cellulose-containing textile fabric and resulting product |
US3419952A (en) * | 1966-09-12 | 1969-01-07 | Gen Electric | Method for making composite material |
US3600103A (en) * | 1969-10-06 | 1971-08-17 | United Aircraft Corp | Composite blade |
JPS5539601B1 (fr) * | 1970-05-12 | 1980-10-13 | ||
US3887365A (en) * | 1971-03-24 | 1975-06-03 | Nasa | Process for making sheets with parallel pores of uniform size |
US3731360A (en) * | 1971-04-07 | 1973-05-08 | United Aircraft Corp | Method of making a composite blade with an integrally attached root thereon |
US3762835A (en) * | 1971-07-02 | 1973-10-02 | Gen Electric | Foreign object damage protection for compressor blades and other structures and related methods |
US3781191A (en) * | 1972-02-22 | 1973-12-25 | Transfer Systems | Nuclear control rod having embedded filaments |
US3994722A (en) * | 1975-12-24 | 1976-11-30 | General Dynamics Corporation | Method and material for fabricating filament reinforced composite structures and tools |
-
1975
- 1975-12-24 CA CA242,605A patent/CA1042641A/fr not_active Expired
-
1976
- 1976-04-30 DE DE19762619235 patent/DE2619235A1/de not_active Withdrawn
- 1976-06-08 GB GB23589/76A patent/GB1536748A/en not_active Expired
- 1976-06-11 US US05/694,927 patent/US4060413A/en not_active Expired - Lifetime
- 1976-08-31 FR FR7626225A patent/FR2336205A1/fr active Granted
- 1976-12-23 JP JP51154386A patent/JPS5281061A/ja active Pending
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2262597A1 (fr) * | 1974-02-28 | 1975-09-26 | United Aircraft Corp |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2711330A1 (fr) * | 1993-10-19 | 1995-04-28 | Deutsche Forsch Luft Raumfahrt | Procédé de fabrication de composants armés de fibres longues. |
Also Published As
Publication number | Publication date |
---|---|
CA1042641A (fr) | 1978-11-21 |
US4060413A (en) | 1977-11-29 |
FR2336205B1 (fr) | 1982-03-26 |
DE2619235A1 (de) | 1977-07-07 |
GB1536748A (en) | 1978-12-20 |
JPS5281061A (en) | 1977-07-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |