FR2391974A1 - Lamifie composite ceramique-metal, joints poreux ceramiques et leur procede de fabrication - Google Patents
Lamifie composite ceramique-metal, joints poreux ceramiques et leur procede de fabricationInfo
- Publication number
- FR2391974A1 FR2391974A1 FR7710105A FR7710105A FR2391974A1 FR 2391974 A1 FR2391974 A1 FR 2391974A1 FR 7710105 A FR7710105 A FR 7710105A FR 7710105 A FR7710105 A FR 7710105A FR 2391974 A1 FR2391974 A1 FR 2391974A1
- Authority
- FR
- France
- Prior art keywords
- low density
- metallic
- thermal deformations
- composite ceramic
- metal laminate
- 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
-
- 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
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/08—Interconnection of layers by mechanical means
-
- 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
- B32B15/02—Layer formed of wires, e.g. mesh
-
- 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
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
-
- 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
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B9/041—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material of metal
-
- 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
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B9/047—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material made of fibres or filaments
-
- 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
- C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
- C04B37/02—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles
- C04B37/023—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles characterised by the interlayer used
- C04B37/026—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles characterised by the interlayer used consisting of metals or metal salts
-
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/005—Selecting particular materials
-
- 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
- F01D5/284—Selection of ceramic materials
-
- 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
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/103—Metal fibres
-
- 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
-
- 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
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/02—Aspects relating to interlayers, e.g. used to join ceramic articles with other articles by heating
- C04B2237/12—Metallic interlayers
- C04B2237/123—Metallic interlayers based on iron group metals, e.g. steel
-
- 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
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/34—Oxidic
- C04B2237/341—Silica or silicates
-
- 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
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/38—Fiber or whisker reinforced
-
- 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
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/40—Metallic
- C04B2237/405—Iron metal group, e.g. Co or Ni
-
- 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
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/59—Aspects relating to the structure of the interlayer
- C04B2237/592—Aspects relating to the structure of the interlayer whereby the interlayer is not continuous, e.g. not the whole surface of the smallest substrate is covered by the interlayer
-
- 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
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/60—Forming at the joining interface or in the joining layer specific reaction phases or zones, e.g. diffusion of reactive species from the interlayer to the substrate or from a substrate to the joining interface, carbide forming at the joining interface
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B1/00—Engines characterised by fuel-air mixture compression
- F02B1/02—Engines characterised by fuel-air mixture compression with positive ignition
- F02B1/04—Engines characterised by fuel-air mixture compression with positive ignition with fuel-air mixture admission into cylinder
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Ceramic Products (AREA)
- Laminated Bodies (AREA)
- Compositions Of Oxide Ceramics (AREA)
Abstract
L'invention concerne un lamifié composite céramique-métal ainsi que son procédé de fabrication. Le lamifié composite selon l'invention comprend une couche en céramique, une interface à structure métallique, tridimensionnelle, flexible, élastique et présentant un faible module et une faible densité, cette interface étant fixée à la couche en céramique, ainsi qu'un organe en métal fixé à la structure métallique à faible module. Les lamifiés de l'invention sont destinés à être utilisés dans des applications à hautes températures, par exemple en tant que joints pour pale de turbo-moteurs.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/674,047 US4142022A (en) | 1976-04-05 | 1976-04-05 | Ceramic-metal laminate |
US05/677,258 US4075364A (en) | 1976-04-15 | 1976-04-15 | Porous ceramic seals and method of making same |
AU74791/81A AU533531B2 (en) | 1976-04-05 | 1981-08-31 | Multiple fibre reinforced ceramic-metal laminate |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2391974A1 true FR2391974A1 (fr) | 1978-12-22 |
FR2391974B1 FR2391974B1 (fr) | 1984-06-29 |
Family
ID=27156100
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7710105A Granted FR2391974A1 (fr) | 1976-04-05 | 1977-04-04 | Lamifie composite ceramique-metal, joints poreux ceramiques et leur procede de fabrication |
Country Status (7)
Country | Link |
---|---|
DE (1) | DE2715290C2 (fr) |
DK (1) | DK132677A (fr) |
FR (1) | FR2391974A1 (fr) |
IT (1) | IT1086845B (fr) |
LU (1) | LU77068A1 (fr) |
NL (1) | NL7703622A (fr) |
SE (1) | SE426581B (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2849652A1 (fr) * | 2003-01-03 | 2004-07-09 | Commissariat Energie Atomique | Procede d'assemblage d'une piece en ceramique avec une piece metallique |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4273824A (en) * | 1979-05-11 | 1981-06-16 | United Technologies Corporation | Ceramic faced structures and methods for manufacture thereof |
US4280975A (en) * | 1979-10-12 | 1981-07-28 | General Electric Company | Method for constructing a turbine shroud |
DE3014645C2 (de) * | 1980-04-16 | 1982-12-02 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Metall-Keramik-Bauteil und Verfahren zu seiner Herstellung |
DE3327216A1 (de) * | 1983-07-28 | 1985-02-07 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Verfahren zur anordnung einer waermedaemmschicht auf einem metallsubstrat |
US4639388A (en) * | 1985-02-12 | 1987-01-27 | Chromalloy American Corporation | Ceramic-metal composites |
DE3514379A1 (de) * | 1985-04-20 | 1986-10-23 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Waermetauscher |
DE3617456A1 (de) * | 1986-05-23 | 1987-12-03 | Vaw Ver Aluminium Werke Ag | Verfahren und vorrichtung zur festen verbindung von keramischen formteilen mit metallen |
DE3638088A1 (de) * | 1986-11-07 | 1988-05-19 | Bernd Retter | Verfahren und vorrichtung zum beschichten von verschleissflaechen sowie nach dem verfahren erstellte verschleissflaechen |
DE3724995A1 (de) * | 1987-02-26 | 1988-09-08 | Radex Heraklith | Verfahren zur herstellung eines verbundkoerpers und verbundkoerper selbst |
DE4021259C2 (de) * | 1989-12-22 | 1994-02-24 | Didier Werke Ag | Verfahren zur Herstellung eines Verbundteiles |
DE4434825A1 (de) * | 1994-09-29 | 1996-05-23 | Tissu Rothrist Ag | Verbundwerkstoff in Flachform |
DE102009058853A1 (de) * | 2009-12-18 | 2011-06-22 | Rolls-Royce Deutschland Ltd & Co KG, 15827 | Turbinenschaufel |
DE102013110154A1 (de) * | 2013-09-16 | 2015-03-19 | Elringklinger Ag | Dichtungssystem und Verbindung einer thermisch hochbelasteten Komponente mit einer thermisch wenig belastbaren Einheit |
EP3517054A1 (fr) * | 2015-09-03 | 2019-07-31 | Biomedical Enterprises, Inc. | Implant orthopédique élastique et son procédé de fabrication |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3114612A (en) * | 1959-05-15 | 1963-12-17 | Eugene W Friedrich | Composite structure |
FR1426197A (fr) * | 1963-10-28 | 1966-01-28 | Atomic Energy Commission | Ensemble d'une pièce métallique et d'une pièce en matière céramique métallisée, et procédé pour sa fabrication |
US3386159A (en) * | 1964-05-04 | 1968-06-04 | Philips Corp | Method of forming a refractory metal-to-ceramic seal |
DE2165696A1 (de) * | 1971-01-20 | 1972-07-27 | British Leyland Truck & Bus | Verfahren zum Löten bzw. Hartlöten von Keramik an Metall |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4844164B1 (fr) * | 1969-04-08 | 1973-12-22 |
-
1977
- 1977-03-23 SE SE7703321A patent/SE426581B/xx unknown
- 1977-03-25 DK DK132677A patent/DK132677A/da unknown
- 1977-04-01 NL NL7703622A patent/NL7703622A/xx not_active Application Discontinuation
- 1977-04-04 LU LU77068A patent/LU77068A1/xx unknown
- 1977-04-04 FR FR7710105A patent/FR2391974A1/fr active Granted
- 1977-04-04 IT IT48799/77A patent/IT1086845B/it active
- 1977-04-05 DE DE2715290A patent/DE2715290C2/de not_active Expired
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3114612A (en) * | 1959-05-15 | 1963-12-17 | Eugene W Friedrich | Composite structure |
FR1426197A (fr) * | 1963-10-28 | 1966-01-28 | Atomic Energy Commission | Ensemble d'une pièce métallique et d'une pièce en matière céramique métallisée, et procédé pour sa fabrication |
US3386159A (en) * | 1964-05-04 | 1968-06-04 | Philips Corp | Method of forming a refractory metal-to-ceramic seal |
DE2165696A1 (de) * | 1971-01-20 | 1972-07-27 | British Leyland Truck & Bus | Verfahren zum Löten bzw. Hartlöten von Keramik an Metall |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2849652A1 (fr) * | 2003-01-03 | 2004-07-09 | Commissariat Energie Atomique | Procede d'assemblage d'une piece en ceramique avec une piece metallique |
Also Published As
Publication number | Publication date |
---|---|
DE2715290C2 (de) | 1986-02-06 |
DE2715290A1 (de) | 1977-10-13 |
FR2391974B1 (fr) | 1984-06-29 |
NL7703622A (nl) | 1977-10-07 |
DK132677A (da) | 1977-10-06 |
SE426581B (sv) | 1983-01-31 |
SE7703321L (sv) | 1977-10-06 |
LU77068A1 (fr) | 1977-08-12 |
IT1086845B (it) | 1985-05-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |