WO1993022258A1 - A ceramic composite, particularly for use at temperatures above 1400 °c - Google Patents
A ceramic composite, particularly for use at temperatures above 1400 °c Download PDFInfo
- Publication number
- WO1993022258A1 WO1993022258A1 PCT/SE1992/000297 SE9200297W WO9322258A1 WO 1993022258 A1 WO1993022258 A1 WO 1993022258A1 SE 9200297 W SE9200297 W SE 9200297W WO 9322258 A1 WO9322258 A1 WO 9322258A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- matrix
- interface material
- reinforcing materials
- composite material
- interface
- Prior art date
Links
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
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
-
- 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
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/64—Burning or sintering processes
- C04B35/645—Pressure sintering
Definitions
- a ceramic composite particularly for use at temperatures above 1400°C
- the present invention refers to a ceramic composite material comprising matrix and possibly reinforcing mate ⁇ rials and an intermediate weak interface material and parti ⁇ cularly adapted for use at temperatures above 1400°C and in oxidizing environment, said matrix and possibly reinforcing materials consisting of the same or different ceramic oxides having a melting point above 1600°c.
- Ceramic composite materials might be divided into materials reinforced by particles, whiskers or elongated fibres. Said materials are prepared by powder processes and sintering or by gas-phase infiltration. The materials hitherto mentioned in the literature often are based on the provision of desired composite characteristics by means of a weak interface material between the matrix and the reinfor ⁇ cing material, preferably fibres, said interface material consisting of carbon or boron nitride, see e.g. Frety, N. , Boussuge, M. , "Relationship between high-temperature development of fibre-matrix interfaces and the mechanical behaviour of SiC-SiC composites", Composites Sci. Techn. 37 177-189 (1990) and Singh, R.N.
- the object of the present invention now is to suggest such a ceramic composite material and the feature essen ⁇ tially distinguishing the invention is that the interface material consists of one or more ceramic oxides not exhi ⁇ biting solid solubility, eutecticum below the temperature of manufacture or use or reaction with any of the matrix or p ⁇ ssibly reinforcing materials and in combination with said materials providing a stress field liable to micro- cracking, said matrix and reinforcing materials being sub ⁇ stantially pure.
- the present invention refers to an interface material for a ceramic composite material in which the matrix and/or the reinforcing material consist of a ceramic oxide comprising one or more metals and having a melting point above 1600°C, said oxide not exhibiting solid solubi ⁇ lity, eutecticum below the temperature of manufacture or use or reactivity with any of the other oxides in the interface or the matrix or reinforcing materials.
- such oxides there can be mentioned A1 2 0 3 , Zr0 2 , Hf0 2 , Al 2 Ti0 5 , Sn0 2 , Y 2 ° 3 ' BeA -'-2 0 4' y ttr i u:ra aluminium garnet (YAG) , LaCrO.-, mullite, BeO and Cr 2 0 3 .
- the reinforcing material is present as fibres but also particulate and layer form are possible.
- the interface material In combination with the matrix and possibly reinfor- cing materials the interface material has to form a stress field which either results into micro cracks in the inter ⁇ face material or into cracks between the latter and the matrix/reinforcing material.
- the stress field might cause crack deflection as such also without micro cracks occuring.
- the desired stress field occurs either by the difference in thermal expansion coefficient between the interface material and the matrix/reinforcing materials or by differences in thermal expansion coefficient between various inherent phases of the interface material. Stresses also might be generated by the fact that the interface material as such has an anisotropic structure with diffe ⁇ rent thermal expansion coefficients in various crystal directions.
- a further possibility to form stresses is that phases of the interface material undergo a phase conversion which results in a change of volume.
- the interface material also might be a composite in which the two inherent phases have different elastic characteristics or different thermal expansion coefficients which creates the desired stress situation.
- Some well-serving interface mate- rials it might be mentioned Al 2 Ti0 5 , cordierite, unstabili- zed Zr0 2 , Sn0 2 , Bf0 2 , mullite, YAG, YAG+Zr0 2 , Al 2 0 3 +Zr0 2 and l 2 i0 5 + l 2 0 3 .
- l 2 iO s and cordierite act as interface materials due to their anisotropy, while Zr0 2 and Sn0 2 act by micro-cracks.
- the interface material has a thickness of at least 2 ⁇ m.
- the interface material is r0 2 it is used in the form of powder or sol during coating of a fibre reinforcing material in order to avoid chemical binding of Zr0 2 to the fibres.
- Fibres of 1 2 0 3 were covered with a thin layer of Al 2 Ti0 5 . This was made by immersing the fibres into a Al-Ti-alkoxide. After gelling and drying the coated fibres were stacked in a plaster mould and a Al 2 0 3 powder slurry was poured thereon.
- Single-crystal-fibres of A1 2 0 3 (from Saphicon, USA) were coated with a thin layer of Zr0 2 . This was made by immersing the fibres in an aqueous Zr0 2 ⁇ sol. After gelling and drying the coated fibres were stacked in a plaster mould and an Al 2 0 3 -powder slurry was poured thereon. After drying the slip-cast bodies were sintered by hot-pressing at 1500°C for 4 hours. After sintering the Zr0 2 layer was about 3 ⁇ m thick . Stress-induced micro-cracks occurred between the layer and the 1 2 0 3 -material. These deflected cracks which was proved by diamond indentation or bending tests.
Abstract
Description
Claims
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/331,630 US5567518A (en) | 1992-05-07 | 1992-05-07 | Ceramic composite, particularly for use at temperatures above 1400 degrees celsius |
DE69218260T DE69218260T2 (en) | 1992-05-07 | 1992-05-07 | CERAMIC COMPOSITE MATERIAL, ESPECIALLY FOR USE AT TEMPERATURES OVER 1400 o C |
JP5519161A JPH08501266A (en) | 1992-05-07 | 1992-05-07 | Ceramic composites used especially at temperatures above 1400 ° C |
EP92916352A EP0639165B1 (en) | 1992-05-07 | 1992-05-07 | A CERAMIC COMPOSITE, PARTICULARLY FOR USE AT TEMPERATURES ABOVE 1400 oC |
PCT/SE1992/000297 WO1993022258A1 (en) | 1992-05-07 | 1992-05-07 | A ceramic composite, particularly for use at temperatures above 1400 °c |
ES92916352T ES2098522T3 (en) | 1992-05-07 | 1992-05-07 | A CERAMIC COMPOSITE MATERIAL, PARTICULARLY FOR USE AT TEMPERATURES HIGHER THAN 1400 DEGREES C. |
CA002135061A CA2135061C (en) | 1992-05-07 | 1992-05-07 | A ceramic composite, particularly for use at temperatures above 1400.degre.c |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/SE1992/000297 WO1993022258A1 (en) | 1992-05-07 | 1992-05-07 | A ceramic composite, particularly for use at temperatures above 1400 °c |
CA002135061A CA2135061C (en) | 1992-05-07 | 1992-05-07 | A ceramic composite, particularly for use at temperatures above 1400.degre.c |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1993022258A1 true WO1993022258A1 (en) | 1993-11-11 |
Family
ID=25677591
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/SE1992/000297 WO1993022258A1 (en) | 1992-05-07 | 1992-05-07 | A ceramic composite, particularly for use at temperatures above 1400 °c |
Country Status (3)
Country | Link |
---|---|
CA (1) | CA2135061C (en) |
ES (1) | ES2098522T3 (en) |
WO (1) | WO1993022258A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2181974A1 (en) * | 2008-10-31 | 2010-05-05 | AVIO S.p.A. | Method for the production of components made of ceramic-matrix composite material |
US11686208B2 (en) | 2020-02-06 | 2023-06-27 | Rolls-Royce Corporation | Abrasive coating for high-temperature mechanical systems |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4298385A (en) * | 1976-11-03 | 1981-11-03 | Max-Planck-Gesellschaft Zur Forderung Wissenschaften E.V. | High-strength ceramic bodies |
EP0202504A2 (en) * | 1985-05-24 | 1986-11-26 | Max-Planck-Gesellschaft zur Förderung der Wissenschaften e.V. | Composite ceramic |
US5017528A (en) * | 1988-02-04 | 1991-05-21 | Martin Marietta Energy Systems, Inc. | Modified silicon carbide whiskers |
US5110771A (en) * | 1991-03-13 | 1992-05-05 | Northrop Corporation | Method of forming a precracked fiber coating for toughening ceramic fiber-matrix composites |
-
1992
- 1992-05-07 WO PCT/SE1992/000297 patent/WO1993022258A1/en active IP Right Grant
- 1992-05-07 ES ES92916352T patent/ES2098522T3/en not_active Expired - Lifetime
- 1992-05-07 CA CA002135061A patent/CA2135061C/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4298385A (en) * | 1976-11-03 | 1981-11-03 | Max-Planck-Gesellschaft Zur Forderung Wissenschaften E.V. | High-strength ceramic bodies |
EP0202504A2 (en) * | 1985-05-24 | 1986-11-26 | Max-Planck-Gesellschaft zur Förderung der Wissenschaften e.V. | Composite ceramic |
US5017528A (en) * | 1988-02-04 | 1991-05-21 | Martin Marietta Energy Systems, Inc. | Modified silicon carbide whiskers |
US5110771A (en) * | 1991-03-13 | 1992-05-05 | Northrop Corporation | Method of forming a precracked fiber coating for toughening ceramic fiber-matrix composites |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2181974A1 (en) * | 2008-10-31 | 2010-05-05 | AVIO S.p.A. | Method for the production of components made of ceramic-matrix composite material |
US8309013B2 (en) | 2008-10-31 | 2012-11-13 | Avio S.P.A. | Method for the production of components made of ceramic-matrix composite material |
US11686208B2 (en) | 2020-02-06 | 2023-06-27 | Rolls-Royce Corporation | Abrasive coating for high-temperature mechanical systems |
Also Published As
Publication number | Publication date |
---|---|
CA2135061C (en) | 2004-02-10 |
CA2135061A1 (en) | 1993-11-11 |
ES2098522T3 (en) | 1997-05-01 |
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