CA2284614C - Fibre-reinforced composite ceramics infiltrated with molten metal - Google Patents
Fibre-reinforced composite ceramics infiltrated with molten metal Download PDFInfo
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- CA2284614C CA2284614C CA002284614A CA2284614A CA2284614C CA 2284614 C CA2284614 C CA 2284614C CA 002284614 A CA002284614 A CA 002284614A CA 2284614 A CA2284614 A CA 2284614A CA 2284614 C CA2284614 C CA 2284614C
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- 239000000919 ceramic Substances 0.000 title claims abstract description 41
- 239000002131 composite material Substances 0.000 title claims abstract description 37
- 229910052751 metal Inorganic materials 0.000 title abstract description 3
- 239000002184 metal Substances 0.000 title abstract description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 69
- 238000000034 method Methods 0.000 claims abstract description 59
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 45
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims abstract description 43
- 239000010703 silicon Substances 0.000 claims abstract description 43
- 239000011651 chromium Substances 0.000 claims abstract description 34
- 229910052742 iron Inorganic materials 0.000 claims abstract description 33
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 31
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 31
- 238000004519 manufacturing process Methods 0.000 claims abstract description 26
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 19
- 239000011159 matrix material Substances 0.000 claims abstract description 14
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 11
- 239000010936 titanium Substances 0.000 claims abstract description 11
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 11
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims abstract description 10
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 10
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 10
- 239000011733 molybdenum Substances 0.000 claims abstract description 10
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 10
- 239000004411 aluminium Substances 0.000 claims abstract description 9
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 9
- 230000008569 process Effects 0.000 claims description 48
- 239000000835 fiber Substances 0.000 claims description 35
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 29
- 239000008187 granular material Substances 0.000 claims description 25
- 239000011230 binding agent Substances 0.000 claims description 19
- 229910052799 carbon Inorganic materials 0.000 claims description 18
- 238000005469 granulation Methods 0.000 claims description 14
- 230000003179 granulation Effects 0.000 claims description 14
- 238000000197 pyrolysis Methods 0.000 claims description 12
- 238000005453 pelletization Methods 0.000 claims description 11
- 238000003825 pressing Methods 0.000 claims description 11
- 230000002829 reductive effect Effects 0.000 claims description 10
- 239000000945 filler Substances 0.000 claims description 9
- 239000000203 mixture Substances 0.000 claims description 8
- 239000002245 particle Substances 0.000 claims description 8
- 239000006229 carbon black Substances 0.000 claims description 7
- 229910002804 graphite Inorganic materials 0.000 claims description 7
- 239000010439 graphite Substances 0.000 claims description 7
- 238000003475 lamination Methods 0.000 claims description 6
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- 229910000676 Si alloy Inorganic materials 0.000 claims description 3
- 229910052796 boron Inorganic materials 0.000 claims description 3
- 239000007789 gas Substances 0.000 claims description 3
- 238000000465 moulding Methods 0.000 claims description 3
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- 229910021332 silicide Inorganic materials 0.000 claims description 3
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- 229910000640 Fe alloy Inorganic materials 0.000 claims 1
- 238000007792 addition Methods 0.000 abstract description 14
- 238000001764 infiltration Methods 0.000 abstract description 5
- 238000006243 chemical reaction Methods 0.000 abstract description 4
- 230000008595 infiltration Effects 0.000 abstract description 4
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 18
- 229910010271 silicon carbide Inorganic materials 0.000 description 18
- 239000000463 material Substances 0.000 description 12
- 238000000626 liquid-phase infiltration Methods 0.000 description 10
- 229910045601 alloy Inorganic materials 0.000 description 7
- 239000000956 alloy Substances 0.000 description 7
- 239000011203 carbon fibre reinforced carbon Substances 0.000 description 6
- 239000000654 additive Substances 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 5
- 239000000155 melt Substances 0.000 description 5
- 238000002844 melting Methods 0.000 description 5
- 238000002156 mixing Methods 0.000 description 5
- 229910052582 BN Inorganic materials 0.000 description 4
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 description 4
- 229910005347 FeSi Inorganic materials 0.000 description 4
- 229910010293 ceramic material Inorganic materials 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 230000008018 melting Effects 0.000 description 4
- 230000003647 oxidation Effects 0.000 description 4
- 238000007254 oxidation reaction Methods 0.000 description 4
- PNEYBMLMFCGWSK-UHFFFAOYSA-N Alumina Chemical compound [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 3
- 229910000604 Ferrochrome Inorganic materials 0.000 description 3
- 230000008901 benefit Effects 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 230000009467 reduction Effects 0.000 description 3
- 238000005245 sintering Methods 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 230000002411 adverse Effects 0.000 description 2
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- 238000005260 corrosion Methods 0.000 description 2
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- 238000009826 distribution Methods 0.000 description 2
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- 239000007921 spray Substances 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- 229910017060 Fe Cr Inorganic materials 0.000 description 1
- 229910002544 Fe-Cr Inorganic materials 0.000 description 1
- 229910005331 FeSi2 Inorganic materials 0.000 description 1
- 229910000519 Ferrosilicon Inorganic materials 0.000 description 1
- 229910001060 Gray iron Inorganic materials 0.000 description 1
- 208000036366 Sensation of pressure Diseases 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 239000012298 atmosphere Substances 0.000 description 1
- YXTPWUNVHCYOSP-UHFFFAOYSA-N bis($l^{2}-silanylidene)molybdenum Chemical compound [Si]=[Mo]=[Si] YXTPWUNVHCYOSP-UHFFFAOYSA-N 0.000 description 1
- 238000003763 carbonization Methods 0.000 description 1
- 239000001913 cellulose Substances 0.000 description 1
- 229920002678 cellulose Polymers 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 229910000423 chromium oxide Inorganic materials 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
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- 150000002148 esters Chemical class 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
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- 230000006870 function Effects 0.000 description 1
- 238000005087 graphitization Methods 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 229910052735 hafnium Inorganic materials 0.000 description 1
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910001338 liquidmetal Inorganic materials 0.000 description 1
- YLGXILFCIXHCMC-JHGZEJCSSA-N methyl cellulose Chemical compound COC1C(OC)C(OC)C(COC)O[C@H]1O[C@H]1C(OC)C(OC)C(OC)OC1COC YLGXILFCIXHCMC-JHGZEJCSSA-N 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 229910021344 molybdenum silicide Inorganic materials 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 239000002243 precursor Substances 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 229910052702 rhenium Inorganic materials 0.000 description 1
- WUAPFZMCVAUBPE-UHFFFAOYSA-N rhenium atom Chemical compound [Re] WUAPFZMCVAUBPE-UHFFFAOYSA-N 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229920003002 synthetic resin Polymers 0.000 description 1
- 239000000057 synthetic resin Substances 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 238000009827 uniform distribution Methods 0.000 description 1
- 229920002554 vinyl polymer Polymers 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 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
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
- C04B35/565—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide
- C04B35/573—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide obtained by reaction sintering or recrystallisation
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
- F16D69/02—Composition of linings ; Methods of manufacturing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
- F16D69/02—Composition of linings ; Methods of manufacturing
- F16D69/023—Composite materials containing carbon and carbon fibres or fibres made of carbonizable material
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Manufacturing & Machinery (AREA)
- General Engineering & Computer Science (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Composite Materials (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Ceramic Products (AREA)
Abstract
The invention concerns fibre-reinforced composite ceramics infiltrated with molten metal and comprising high-temperature fibres in particular based on Si/C/B/N, which are bound in terms of reaction to an Si- based matrix. The invention also concerns a method of producing such ceramics. The molten silicon used for infiltration purposes contains additions of iron, chromium, titanium, molybdenum, nickel or aluminium, molten silicon containing approximately 5 to 50 weight % iron and approximately 1 to 10 weight % chromium being particularly preferred. The production method is simpler than conventional molten silicon infiltration methods and imparts improved properties to the composite ceramics.
Description
Fibre-Reinforced Composite Ceramics Infiltrated with Molten Metal Background of the Invention The invention relates to a melt-infiltrated fibre-s reinforced composite ceramic containing high-temperature-resistant fibres, in particular fibres based on Si/C/B/N, which are reaction-bonded to a matrix based on Si and containing at least one addition of another material, and also to a process for producing such a composite ceramic.
Such a process and such a composite ceramic are known from US-A-5 464 655.
Carbon fibre-reinforced carbon (C/C, also known as CFRC or in German language usage as CFC) is the first industrially successful development in the group consisting of fibre-reinforced composite ceramic materials.
Recently developed high-performance brake systems based on CFRC brake discs with specially developed friction linings, as are used, for instance, in motor racing, can only be produced using numerous impregnation or carbonization and graphitization cycles, so that the production process is extremely time-consuming, energy-intensive and costly and can take a number of weeks or months. In addition, CFRC brake discs have totally unsatisfactory braking properties for use in production vehicles which are not subjected to demanding operating conditions in the presence of moisture and at low temperatures. This manifests itself, inter alia, in decidedly non-constant coefficients of friction as a function of the operating temperature and the surface lining which makes regulation, as has hitherto been ' ~ CA 02284614 1999-09-21 27 168/P _ 2 _ customary in 4-channel ABS systems, extraordinarily difficult or even impossible. In view of this background, attempts are being made to develop improved fibre-rein-forced composite ceramic materials which can be used, for example, as brake discs for high-performance brake systems in motor vehicles or in railway vehicles. Fur thermore, such fibre-reinforced composite ceramic materi als are also of interest for numerous other applications, for instance as turbine materials or as materials for sliding bearings.
Although silicon-infiltrated reaction-bonded silicon carbide (SiSiC) containing from 2 to 15~ by mass of free silicon has been known since the 1960s and has also been introduced commercially for some applications in heat engineering. Problems in respect of internal stresses (internal stress due to cooling) occur in the :manufacture of large and thick-walled components because of a step increase in the volume of the semimetallic silicon when it solidifies in the microstructure of the material. The stressing of the solidified silicon mani-fests itself, in many cases, in the formation of microcracks and in a reduction in adhesion at internal interfaces, so that the strength of the material is reduced and critical crack propagation under cyclic 35 thermal and mechanical stress can be expected, particularly during prolonged use. In manufacture, the volume expansion on solidification leads to difficulties as have long been known when, for instance, water freezes in closed line systems, i.e. to rupture and breaking of the components and thus to high reject rates. In addition, the manufacture of SiSiC materials is relatively complicated and expensive.
US 5 079 195 A discloses a process in which a AMENDED SHEET
carbon-containing precursor body is infiltrated With a silicon melt which is alloyed with at least one element which is essentially insoluble in silicon and which forms high-melting phases, namely molybdenum, tungsten, rhenium, hafnium, zirconium, chromium, boron and titanium. In this way, only a minimum of free silicon remains in the composite body. As a result, the risk of crack formation in the material is reduced and the heat resistance is increased, so that the material is more mechanically and thermally stable.
EP 0 798 280 A2 discloses a composite ceramic material which is resistant to high temperatures and contains silicon carbide and molybdenum silicide.
However, a problem here is that these additives are expensive and therefore unsuitable for mass production.
Furthermore, these additives are unsuitable for use of the ceramic as brake disc material, since the friction pairing with customary brake linings is adversely affected.
Summary of the Invention It is therefore an object of the present invention to provide an improved fibre-reinforced composite ceramic containing high-temperature-resistant fibres and also a process for producing such a composite ceramic, which makes possible vary simple and inexpensive production of mass produced components such as brake discs, with high thermal stability and hot strength together with sufficient oxidation resistance and thermal shock resistance being prerequisites.
The object of the invention is achieved by, in a melt-infiltrated fibre-reinforced composite ceramic of the type described at the outset, the matrix containing additions of iron.
The object of the invention is completely achieved in this manner. According to the invention, it has been recognized that this measure makes it possible, in a particularly inexpensive and environmentally friendly manner, to avoid the volume increase which occurs in the case of pure silicon, and the additions of iron at the same time lead to improved braking performance in an application as a brake disc, since an improved friction pairing is obtained with conventional brake linings which are matched to brake discs based on grey cast iron. Brake systems based on such brake discs are thus more readily regulated since, in addition, they are less moisture-sensitive and are insensitive to low temperatures. Furthermore, there are no critical contact pressures which have an adverse effect on regulatability, as in the case of CFRC brake discs. In addition, the production process is simplified and made cheaper by the lowering of the melting point of the silicon melt by the addition of iron.
The alloying of the silicon melt used for melt infiltration with iron enables the step increase in volume on solidification of a pure silicon melt to be reduced or even largely avoided. In this way, the problems caused by the stressing of the solidified silicon are avoided, a higher strength, particularly with regard to cyclic thermal and mechanical stress, is achieved and at the same time the production process is simpler and less costly.
In an advantageous embodiment of the invention, preference is given to adding further additions of chromium, titanium, aluminium, nickel or molybdenum in a suitable ratio as passive layer formers to a matrix based on Si which contains additions of iron. These additives can effect the formation of protective passive layers, so ' ~ CA 02284614 1999-09-21 that the oxidation and corrosion resistance is improved.
In this case, different coefficients of thermal expansion of the alloying components lead to stress states in the matrix which compensate for the stresses caused by the fibres on cooling.
It is thus possible, according to the invention, to obtain a reaction-bonded, melt-infiltrated SiC ceramic {RB-SiC) in which the brittle Si as is present in hitherto customary RB-SiC ceramics is replaced by a phase enriched with Fe or Fe together with Cr and/or Ti, Mo, Ni or Al, which leads to a significant increase in strength and ductility of the ceramic.
In a further embodiment of the invention, the matrix is produced from a silicon alloy containing from 0.5 to 80% by weight of iron, preferably from about 5 to 50% by weight (based on the total mass of the alloy).
Since ferrosilicon in comparatively pure form is used on an industrial scale in steel production, with grades having the compositions Fe25Si75 and Fe35Si65 being commercially available, a considerable reduction in the raw material costs compared with the use of pure silicon is achieved. Furthermore, there is a lowering of the melting point from about 1410°C for pure silicon to about 1340°C when Fe25Si75 is used and to about 1275°C when Fe35Si65 is used.
In an additional embodiment of the invention, an additional 5-30% by weight of chromium, preferably about 7-12% by weight of chromium, based on the iron content, is added to the silicon melt which is used for melt infiltration.
This change to a three-material system consisting of Si-Fe-Cr enables the iron-containing,phases of the composite ceramic to be protected against corrosion and AMENDED SHEET
at the same time allows the melting point to be lowered to less than 1400°C. For this purpose, it is useful to add at least about 7% by Weight of chromium (based on the iron content), since from about 7 to 8% by weight of chromium is necessary to effect the formation of a passive layer of chromivm(III) oxide, as is known from stainless steels. (Based on the total mass of the alloy, the proportion by weight of chromium is preferably from about 1 to 30% by weight, preferably from about 1 to 10%
by weight.) However, for cost reasons it is preferable to select a chromium content which is not unnecessarily high. Although the corresponding metallic starting materials in the form of chromium-containing alloys (e. g.
FeCr) are slightly more expensive than iron silicides such as FeSi it FeSi2, they give considerable advantages as a result of the improved oxidation resistance.
Fibres which are suitable for the fibre rein-forcement include numerous high-temperature-resistant fibres, in particular fibres based on Si/C/8/N and having covalent bonds, with C fibres and SiC fibres being among the best known fibres which are suitable for the ceramics of the invention. In addition, use of, for instance, aluminium oxide fibres is also conceivable for particu-larly inexpensive products.
In an additional embodiment of the invention, the fibres are combined to form fibres bundles and are surface-impregnated.
In this way, commercially available rovings and multifilament strands (e. g. 12K bundles) can be used.
These are advantageously impregnated on their surface, e.g. by means of pitch, to protect the fibre bundles against mechanical damage during production and to avoid excessive reaction and thus damage during the silicon AMENDED SHEET
-infiltration by forming a carbon layer which can react to form SiC and thus protect the fibres.
In a further advantaaeo,~R a,t,~,~~;..,e.,~ ..~ aL_ invention, the fibres are collected together to form short fibre bundles and can comprise, for example, C
filaments having mean diameters of from about 5 to 12 ~cm and a length of from about 2 to 10 aan which are collected together to form fibre bundles containing from about 3000 to 14,000 filaments.
Such chopped carbon fibre bundles which are used for short-fibre reinforcement allow simplified production of a shaped body by pressing methods without costly lamination and post-impregnation having to be carried out. This makes possible inexpensive mass production and the parameters can be set so that virtually ao shrinkage occurs and only miaimal final machining, for example by grinding, of the finished components is necessary ("near net shape manufacture").
As regards to the process, the object of the invention is achieved by a process for producing a fibre-reinforced composite ceramic containing high-temperature-resistant fibres, in particular fibres based oa Si/C/H/N, which are reaction-bonded to a matrix based oa Si, which comprises the follov~ing steps:
- production of a green body from fibres using binders and fillers by winding, lamination or pressing;
- pyrolysis of the green body under reduced pres-sure or protective gas in a temperature range from about 800°C to 1200°C to produce a porous shaped body;
-- infiltration of the carbonized shaped body with a silicon melt which contains additions of iron.
As explained above, the volume increase which occurs when using pure silicon for the melt infiltration (about 10~ by volume) can be considerably reduced or even avoided by means of such additions, so that a material having improved properties is obtained by a simplified and cheaper production process.
The internal stresses which occur in conventional fibre-reinforced, reaction-bonded SiC materials (RB-SiC) and lead to numerous reject parts during manufacture are reduced or largely avoided in this way. In a preferred embodiment of the invention, additions of iron and, if desired, of chromium, titanium, aluminium, nickel or molybdenum as passive layer former are mixed in suitable mixing ratios into the silicon melt.
Iron additions in the range from about 0.5 to 80~
by weight of iron, preferably from about 5 to 50~ by weight of iron, and, if desired, chromium additions of from 0.03 to 40~ by weight of chromium, preferably from 1 to 30~ by weight of chromium, in particular from about 2 to 10~ by weight of chromium (based on the total mass of the alloy), give particularly advantageous properties, a favourable reduction in the melting point and a considerable improvement in the oxidation resistance of the iron-containing phases by formation of a passive chromium oxide layer. The abovementioned data are in each case based on the total weight of the final product.
As fibres for the production of the composite ceramic, it is possible to use any high-temperature resistant fibres, in particular fibres based on Si/C/B/N
having covalent bonding, but C fibres or SiC fibres which are collected together to form fibre bundles and are - 8a -surface-impregnated are among the technologically proven and commercially available fibres which, particularly when used in the form of short fibre bundles comprising from about 3000 to 14,000 filaments having mean diameters of from about 5 to 12 N,m and a length of from about 2 to 10 mm, preferably from about 3 to 6 mm, at a diameter of the fibre bundles of about 0.1 mm, can be employed advantageously.
The green bodies from which the porous shaped bodies are produced in the subsequent pyrolysis are, in an additional embodiment of the invention, produced by dry pressing or hot flow moulding of a granulated material which is obtained, in order to be particularly gentle with the fibres, by pan granulation.
Pan granulation allows the mechanically sensitive fibre bundles to be agglomerated with the other additives to produce a green body in a particularly gentle and relatively inexpensive way and at the same time achieves a good uniform distribution.
The pan granulation can be carried out continu-ously or batchwise, with the process preferably being controlled to produce a mean particle size of from about 2 to 6 mm.
In the production of the granulated material, SiC
powder, silicides and carbon-containing fillers, prefer-ably carbon black and/or graphite, are added in a further advantageous embodiment of the invention.
Here, the preferred procedure is first to premix a dry mixture of short-fibre bundles and fillers and subsequently to mix this with binders and further dissolved or dispersed additives in a pelletizing pan to produce the granulated material.
It has been found to be advantageous to produce the granulated material from about 20-60% by weight of SiC powder, about 2-20% by weight of carbon in the form of graphite powder and/or carbon black, and about 10-40%
by weight of C fibre bundles (12K bundles) which are premixed dry and to which about 15-40% by weight of a binder solution, based on the total initial charge of solid materials, are added in a pelletizing pan.
Here, an aqueous binder solution containing from about 0.01 to 10% by weight of methylcellulose esters and polyvinyl alcohol has been found to be a suitable binder.
In an advantageous embodiment of the invention, the granulated material is, after it has'been produced, first dried, preferably to residual moisture contents of less than 10% by weight of water, and then pressed to form green bodies.
A texture which may be obtained in the pressing procedure has, if the die is configured appropriately, an advantageous effect, for instance for use as a brake disc, since the C fibre bundles are preferentially aligned parallel to the flat surface of a flat disc, which also corresponds to the main stress direction.
In a preferred embodiment of the invention, such green bodies are then heated to from about 950 to 1050°C
under a protective gas atmosphere in a pyrolysis furnace or a vacuum reaction-sintering furnace to produce porous shaped bodies, preferably having a porosity of from about 30 to 50%, for a subsequent melt infiltration.
The melt infiltration which follows is preferably carried out using a silicon melt containing from about 10 to 50% by weight of iron and from about 0.5 to 10% by weight of chromium with the balance being silicon (based on the proportions by weight in the alloy).
Overall, this gives a reproducible and inexpen-sive manufacturing process which is suitable for mass production. Since virtually no shrinkage and internal stresses due to cooling occur, a significantly lower reject rate than in the case of conventional RB-SiC
ceramics is achieved and the need for final machining is considerably reduced, particularly in the case of iron-rich phases in the microstructure.
It will be self-evident to those skilled in the art that the features mentioned above and the features still to be described below can be used not only in the combination indicated in each case, but also in other combinations or alone without going outside the scope of the present invention.
In particular, it may be mentioned that the process of pan granulation is suitable not only for producing melt-infiltrated fibre-reinforced composite ceramics containing high-temperature-resistant ceramic fibres which are reaction-bonded to a matrix based on Si and containing additions of iron, chromium, titanium, molybdenum, nickel or aluminium, but can also be used With considerable advantage for producing such composite ceramics in which a pure silicon melt is used for melt infiltration.
Further features and advantages of the invention may be found in the following description of preferred illustrative embodiments with reference to the drawings.
Fig. 1 schematically shows a reaction-sintering furnace for melt infiltration;
Fig. 2 schematically shows a pelletizing pan which is used for pan granulation, with the path of individual particles being indicated;
Fig. 3 shows a plan view of the pelletizing pan of Fig. 2 from the front side;
Fig. 4 shows an optical micrograph of the microstructure of a composite ceramic according to the invention;
and Fig. 5 shows an enlarged section of the microstructure shown in Fig. 4.
A distinguishing aspect of the process of the invention is that the final step for producing the fibre-reinforced composite ceramic, namely the melt infilitration, is not carried out using a pure silicon melt as in the prior art, but instead additions of iron, chromium, titanium, molybdenum, nickel and/or aluminium are added to the melt.
Independently of this, the porous shaped body which is impregnated with liquid metal in the melt infiltration can be produced in various ways.
The process of the invention thus makes possible the infiltration of C hard felts and other fibre compo-sites and also the production of ceramics reinforced 2-and 3-dimensionally with continuous fibres.
The shaped bodies can thus be produced, for instance, by known lamination techniques, for example using synthetic resins, or else by pressing processes, with the green bodies being converted by pyrolysis into porous shaped bodies, is particular C-bonded shaped bodies, which are permeated by a complete pore network and thus, in the subsequent melt infiltration, draw in the liquid melt by means of the capillary forces within the porous.shaped body, in a similar manner to a wick or sponge.
Apart from the conventional lamination technique which, as described above, can be used for carrying out the invention, particular preference is given according to the invention to a pan granulation process for produc-ing short-fibre-reinforced melt-infiltrated composite ceramics.
The following description of the process variants for producing shaped bodies thus relates only to the production of short-fibre ceramics. However, it should be stated that it is also possible to use, as an alterna-tive, conventional lamination methods.
Example 1 The starting materials used are summarized in Table 1.
Compound Designation Source Data TM
SiC SM93 IndustriekeramikS,,.03:3.1 m~/a high-purity TM
Carbon black Printex 140 Degussa U
Graphite KS 6 Timcal Short C fibre SGL carbon 3aua, 12,000 bundles fil.
TM
Methyl- Tylose 4000 Hoechst I
cellulose G4 I
ester TM
Polyvinyl Moviol 10-74 Hoechst alcohol FeSi(65 or FeSi75 or FESIL Grain size:
' 75) FeSi65 5-30 ~n ~ FeCr(65 % Ferrochrom FESIL Grain size:
by mass of Cr) affine- 5-30 mm Table 1 1.1 Pan granulation In a tuanble mixer, 344 g of SiC powder, 48 g of graphite powder and 8 g of carbon black were intensively mixed at 50 rpm for three hours. Subsequently, 200 g of pitch-coated short C fibre bundles were added and mixed into the powder mixture for 5 minutes at 10 rpm. This mixture was transferred to a pelletizing pan 24 as shown in Fig. 2 and 3 and subjected to a rolling-mixing motion at 30 rpm and a pan inclination angle of about 40°. 240 g of the aqueous binder solution as per Tab3e 1 consisting of 1% by weight of Tylose 4000 G4 and 0.5% by weight of Moviol 10-74 dissolved in demineralized water were sprayed in via nozzles from spray lines 36 for a period of 3 minutes.
In Figs 2 and 3, the paths of small particles are indicated schematically by 28 and those of larger par-ticles are indicated schematically by 34. Additional mixing can be achieved by means of an additional mixing pan 26 as shown in Fig. 3. In this method of pan granu-lation, the distribution of the components in the granu-lated material being fozzned and also the granule size can be influenced by varying various parameters such as rotational speed and angle of inclination of the pellet-izing pan 24, rotational speed of the additional mixing pan 26, location of the spray nozzles for introduction of the binder solution, type and amount of binder solution added, etc.
Overall, the pan granulation can be adjusted so that granule-formation which is gentle on the carbon fibre bundles is obtained together with a uniform, homogeneous distribution of the individual components.
The granulated material produced preferably has a par-ticle size of from about 3 to 6 mm.
The pan granulation can be carried out either batchwise, in which case the granulated material obtained is subsequently sieved to obtain the desired particle size fraction, or else can be carried out continuously as shown in Fig. 3. In this variant, dry mix is continuously introduced as indicated by the reference numeral 32 and binder solution is sprayed in via the lines 36 and, at the same time, finished granulated material is discharged continuously in the region 30 of the pelletizing pan.
The granulated material formed in this way was dried to a moisture content of less than ~10~.
. CA 02284614 1999-09-21 1.2. Shapinc3 56.9 g of the granulated material were trans-ferred to a pressing die having a diameter of 60 xcan and pressed to a height of 13.6 mm by means of a hydraulic press using a pressure of 20 MPa. This gave a mechanic-ally stable green body which could be transported.
1.3. Pyrolysis The green body obtained above was taken from the pressing die, transferred to a pyrolysis furnace and heated at a rate of 10 K/min to 1000°C under a nitrogen atmosphere. In the pyrolysis, the organic binder consti-tuents were degraded to carbon. The resulting porous shaped body had a weight of 55.8 g and a porosity of 39%.
1.4. Melt infiltration A carbonized shaped body as obtained in section 1.3. and having a mass of 20 g was transferred to a graphite crucible coated with boron nitride, covered with 22 g of a granulated FeSi alloy consisting of 75% by weight of Si and 25% by weight of Fe and heated at 10 R/min to 1550°C under reduced pressure. This tempera-ture Was held for 30 minutes and the crucible was then cooled to room temperature.
This procedure gave a dense, crack- and pore-free shaped body having a density of 3.1 g/cm3 whose external geometric dimensions corresponded to those of the shaped body initially placed in the crucible.
Instead of placing the shaped body directly in a graphite crucible 20 coated with boron nitride, an alternative possibility is, as shown in Fig. 1, to use a porous SiC charging plate 16 in the furnace chamber 12 of a reaction-sintering furnace 10; this SiC'charging plate 16 stands on feet 18 in the melt 22 of the graphite .- CA 02284614 1999-09-21 crucible 20 coated with boron nitride or is connected therewith_via porous wicks. In this variant, a larger amount of granulated material for producing the melt 22 can be introduced into the crucible 20 since the melt 22 rises from below through the porous feet 18 and the porous charging plate 16 into the shaped body 14.
Example 2 A green body was produced as described above by pan granulation and subsequent pressing and subjected to pyrolysis in the above-described manner in a pyrolysis furnace.
The shaped body obtained in this way and having a mass of 20 g was again transferred to a graphite crucible coated with boron nitride, covered with 22 g of a mixture of 19 g of a granulated FeSi alloy consisting of 75% by weight of Si and 25% by weight of Fe to which 3 g of granulated FeCr (65% by weight of chromium) had been added and the crucible was heated at 10 K/min to 1700°C under reduced pressure. This temperature was held for 30 minutes. The crucible was then cooled to room temperature.
This procedure gave a dense, crack- and pore-free shaped body having a density of 3.2 g/cm' whose external geometric dimensions corresponded to those of the shaped body initially placed in the crucible.
Figs 4 and 5 show optical micrographs of polished sections of specimens which were produced as described in Example 1.
In Fig. 4, a C fibre bundle can be seen in the left-hand half of the picture while part of the next C
fibre bundle is visible at the bottom right-hand corner of the picture. The numeral 40 denotes carbon foxed by pyrolysis while the numeral 42 denotes C fibres.
Secondary SiC formed from the reaction of carbon fibres with silicon is present at the edge of the C fibre bundle;
this secondary SiC is denoted by the numeral 48.
The light-coloured phase denoted by the numeral 44 is silicon or Si/Fe/Cr. The dark grey phase denoted by 46 is SiC.
In the enlarged view shown in Fig. 5, in which a carbon fibre bundle is cut virtually perpendicularly across, the individual C fibres can readily be seen. The secondary SiC which has been formed from the reaction of C
fibres and is denoted by the numeral 48 can also be readily seen.
It can easily be seen that the carbon fibre bundle is retained virtually unscathed and only a few of the C
fibres in the outer region have been converted into secondary SiC.
This explains the considerable increase in strength which is achieved by the gentle treatment of the C fibre bundles in the pan granulation and in the subsequent process steps.
The foregoing disclosure has been set forth merely to illustrate the invention and is not intended to be limiting. Since modifications of the disclosed embodiments incorporating the spirit and substance of the invention may occur to persons skilled in the art, the invention should be construed to include everything within the scope of the appended claims and equivalents thereof.
Such a process and such a composite ceramic are known from US-A-5 464 655.
Carbon fibre-reinforced carbon (C/C, also known as CFRC or in German language usage as CFC) is the first industrially successful development in the group consisting of fibre-reinforced composite ceramic materials.
Recently developed high-performance brake systems based on CFRC brake discs with specially developed friction linings, as are used, for instance, in motor racing, can only be produced using numerous impregnation or carbonization and graphitization cycles, so that the production process is extremely time-consuming, energy-intensive and costly and can take a number of weeks or months. In addition, CFRC brake discs have totally unsatisfactory braking properties for use in production vehicles which are not subjected to demanding operating conditions in the presence of moisture and at low temperatures. This manifests itself, inter alia, in decidedly non-constant coefficients of friction as a function of the operating temperature and the surface lining which makes regulation, as has hitherto been ' ~ CA 02284614 1999-09-21 27 168/P _ 2 _ customary in 4-channel ABS systems, extraordinarily difficult or even impossible. In view of this background, attempts are being made to develop improved fibre-rein-forced composite ceramic materials which can be used, for example, as brake discs for high-performance brake systems in motor vehicles or in railway vehicles. Fur thermore, such fibre-reinforced composite ceramic materi als are also of interest for numerous other applications, for instance as turbine materials or as materials for sliding bearings.
Although silicon-infiltrated reaction-bonded silicon carbide (SiSiC) containing from 2 to 15~ by mass of free silicon has been known since the 1960s and has also been introduced commercially for some applications in heat engineering. Problems in respect of internal stresses (internal stress due to cooling) occur in the :manufacture of large and thick-walled components because of a step increase in the volume of the semimetallic silicon when it solidifies in the microstructure of the material. The stressing of the solidified silicon mani-fests itself, in many cases, in the formation of microcracks and in a reduction in adhesion at internal interfaces, so that the strength of the material is reduced and critical crack propagation under cyclic 35 thermal and mechanical stress can be expected, particularly during prolonged use. In manufacture, the volume expansion on solidification leads to difficulties as have long been known when, for instance, water freezes in closed line systems, i.e. to rupture and breaking of the components and thus to high reject rates. In addition, the manufacture of SiSiC materials is relatively complicated and expensive.
US 5 079 195 A discloses a process in which a AMENDED SHEET
carbon-containing precursor body is infiltrated With a silicon melt which is alloyed with at least one element which is essentially insoluble in silicon and which forms high-melting phases, namely molybdenum, tungsten, rhenium, hafnium, zirconium, chromium, boron and titanium. In this way, only a minimum of free silicon remains in the composite body. As a result, the risk of crack formation in the material is reduced and the heat resistance is increased, so that the material is more mechanically and thermally stable.
EP 0 798 280 A2 discloses a composite ceramic material which is resistant to high temperatures and contains silicon carbide and molybdenum silicide.
However, a problem here is that these additives are expensive and therefore unsuitable for mass production.
Furthermore, these additives are unsuitable for use of the ceramic as brake disc material, since the friction pairing with customary brake linings is adversely affected.
Summary of the Invention It is therefore an object of the present invention to provide an improved fibre-reinforced composite ceramic containing high-temperature-resistant fibres and also a process for producing such a composite ceramic, which makes possible vary simple and inexpensive production of mass produced components such as brake discs, with high thermal stability and hot strength together with sufficient oxidation resistance and thermal shock resistance being prerequisites.
The object of the invention is achieved by, in a melt-infiltrated fibre-reinforced composite ceramic of the type described at the outset, the matrix containing additions of iron.
The object of the invention is completely achieved in this manner. According to the invention, it has been recognized that this measure makes it possible, in a particularly inexpensive and environmentally friendly manner, to avoid the volume increase which occurs in the case of pure silicon, and the additions of iron at the same time lead to improved braking performance in an application as a brake disc, since an improved friction pairing is obtained with conventional brake linings which are matched to brake discs based on grey cast iron. Brake systems based on such brake discs are thus more readily regulated since, in addition, they are less moisture-sensitive and are insensitive to low temperatures. Furthermore, there are no critical contact pressures which have an adverse effect on regulatability, as in the case of CFRC brake discs. In addition, the production process is simplified and made cheaper by the lowering of the melting point of the silicon melt by the addition of iron.
The alloying of the silicon melt used for melt infiltration with iron enables the step increase in volume on solidification of a pure silicon melt to be reduced or even largely avoided. In this way, the problems caused by the stressing of the solidified silicon are avoided, a higher strength, particularly with regard to cyclic thermal and mechanical stress, is achieved and at the same time the production process is simpler and less costly.
In an advantageous embodiment of the invention, preference is given to adding further additions of chromium, titanium, aluminium, nickel or molybdenum in a suitable ratio as passive layer formers to a matrix based on Si which contains additions of iron. These additives can effect the formation of protective passive layers, so ' ~ CA 02284614 1999-09-21 that the oxidation and corrosion resistance is improved.
In this case, different coefficients of thermal expansion of the alloying components lead to stress states in the matrix which compensate for the stresses caused by the fibres on cooling.
It is thus possible, according to the invention, to obtain a reaction-bonded, melt-infiltrated SiC ceramic {RB-SiC) in which the brittle Si as is present in hitherto customary RB-SiC ceramics is replaced by a phase enriched with Fe or Fe together with Cr and/or Ti, Mo, Ni or Al, which leads to a significant increase in strength and ductility of the ceramic.
In a further embodiment of the invention, the matrix is produced from a silicon alloy containing from 0.5 to 80% by weight of iron, preferably from about 5 to 50% by weight (based on the total mass of the alloy).
Since ferrosilicon in comparatively pure form is used on an industrial scale in steel production, with grades having the compositions Fe25Si75 and Fe35Si65 being commercially available, a considerable reduction in the raw material costs compared with the use of pure silicon is achieved. Furthermore, there is a lowering of the melting point from about 1410°C for pure silicon to about 1340°C when Fe25Si75 is used and to about 1275°C when Fe35Si65 is used.
In an additional embodiment of the invention, an additional 5-30% by weight of chromium, preferably about 7-12% by weight of chromium, based on the iron content, is added to the silicon melt which is used for melt infiltration.
This change to a three-material system consisting of Si-Fe-Cr enables the iron-containing,phases of the composite ceramic to be protected against corrosion and AMENDED SHEET
at the same time allows the melting point to be lowered to less than 1400°C. For this purpose, it is useful to add at least about 7% by Weight of chromium (based on the iron content), since from about 7 to 8% by weight of chromium is necessary to effect the formation of a passive layer of chromivm(III) oxide, as is known from stainless steels. (Based on the total mass of the alloy, the proportion by weight of chromium is preferably from about 1 to 30% by weight, preferably from about 1 to 10%
by weight.) However, for cost reasons it is preferable to select a chromium content which is not unnecessarily high. Although the corresponding metallic starting materials in the form of chromium-containing alloys (e. g.
FeCr) are slightly more expensive than iron silicides such as FeSi it FeSi2, they give considerable advantages as a result of the improved oxidation resistance.
Fibres which are suitable for the fibre rein-forcement include numerous high-temperature-resistant fibres, in particular fibres based on Si/C/8/N and having covalent bonds, with C fibres and SiC fibres being among the best known fibres which are suitable for the ceramics of the invention. In addition, use of, for instance, aluminium oxide fibres is also conceivable for particu-larly inexpensive products.
In an additional embodiment of the invention, the fibres are combined to form fibres bundles and are surface-impregnated.
In this way, commercially available rovings and multifilament strands (e. g. 12K bundles) can be used.
These are advantageously impregnated on their surface, e.g. by means of pitch, to protect the fibre bundles against mechanical damage during production and to avoid excessive reaction and thus damage during the silicon AMENDED SHEET
-infiltration by forming a carbon layer which can react to form SiC and thus protect the fibres.
In a further advantaaeo,~R a,t,~,~~;..,e.,~ ..~ aL_ invention, the fibres are collected together to form short fibre bundles and can comprise, for example, C
filaments having mean diameters of from about 5 to 12 ~cm and a length of from about 2 to 10 aan which are collected together to form fibre bundles containing from about 3000 to 14,000 filaments.
Such chopped carbon fibre bundles which are used for short-fibre reinforcement allow simplified production of a shaped body by pressing methods without costly lamination and post-impregnation having to be carried out. This makes possible inexpensive mass production and the parameters can be set so that virtually ao shrinkage occurs and only miaimal final machining, for example by grinding, of the finished components is necessary ("near net shape manufacture").
As regards to the process, the object of the invention is achieved by a process for producing a fibre-reinforced composite ceramic containing high-temperature-resistant fibres, in particular fibres based oa Si/C/H/N, which are reaction-bonded to a matrix based oa Si, which comprises the follov~ing steps:
- production of a green body from fibres using binders and fillers by winding, lamination or pressing;
- pyrolysis of the green body under reduced pres-sure or protective gas in a temperature range from about 800°C to 1200°C to produce a porous shaped body;
-- infiltration of the carbonized shaped body with a silicon melt which contains additions of iron.
As explained above, the volume increase which occurs when using pure silicon for the melt infiltration (about 10~ by volume) can be considerably reduced or even avoided by means of such additions, so that a material having improved properties is obtained by a simplified and cheaper production process.
The internal stresses which occur in conventional fibre-reinforced, reaction-bonded SiC materials (RB-SiC) and lead to numerous reject parts during manufacture are reduced or largely avoided in this way. In a preferred embodiment of the invention, additions of iron and, if desired, of chromium, titanium, aluminium, nickel or molybdenum as passive layer former are mixed in suitable mixing ratios into the silicon melt.
Iron additions in the range from about 0.5 to 80~
by weight of iron, preferably from about 5 to 50~ by weight of iron, and, if desired, chromium additions of from 0.03 to 40~ by weight of chromium, preferably from 1 to 30~ by weight of chromium, in particular from about 2 to 10~ by weight of chromium (based on the total mass of the alloy), give particularly advantageous properties, a favourable reduction in the melting point and a considerable improvement in the oxidation resistance of the iron-containing phases by formation of a passive chromium oxide layer. The abovementioned data are in each case based on the total weight of the final product.
As fibres for the production of the composite ceramic, it is possible to use any high-temperature resistant fibres, in particular fibres based on Si/C/B/N
having covalent bonding, but C fibres or SiC fibres which are collected together to form fibre bundles and are - 8a -surface-impregnated are among the technologically proven and commercially available fibres which, particularly when used in the form of short fibre bundles comprising from about 3000 to 14,000 filaments having mean diameters of from about 5 to 12 N,m and a length of from about 2 to 10 mm, preferably from about 3 to 6 mm, at a diameter of the fibre bundles of about 0.1 mm, can be employed advantageously.
The green bodies from which the porous shaped bodies are produced in the subsequent pyrolysis are, in an additional embodiment of the invention, produced by dry pressing or hot flow moulding of a granulated material which is obtained, in order to be particularly gentle with the fibres, by pan granulation.
Pan granulation allows the mechanically sensitive fibre bundles to be agglomerated with the other additives to produce a green body in a particularly gentle and relatively inexpensive way and at the same time achieves a good uniform distribution.
The pan granulation can be carried out continu-ously or batchwise, with the process preferably being controlled to produce a mean particle size of from about 2 to 6 mm.
In the production of the granulated material, SiC
powder, silicides and carbon-containing fillers, prefer-ably carbon black and/or graphite, are added in a further advantageous embodiment of the invention.
Here, the preferred procedure is first to premix a dry mixture of short-fibre bundles and fillers and subsequently to mix this with binders and further dissolved or dispersed additives in a pelletizing pan to produce the granulated material.
It has been found to be advantageous to produce the granulated material from about 20-60% by weight of SiC powder, about 2-20% by weight of carbon in the form of graphite powder and/or carbon black, and about 10-40%
by weight of C fibre bundles (12K bundles) which are premixed dry and to which about 15-40% by weight of a binder solution, based on the total initial charge of solid materials, are added in a pelletizing pan.
Here, an aqueous binder solution containing from about 0.01 to 10% by weight of methylcellulose esters and polyvinyl alcohol has been found to be a suitable binder.
In an advantageous embodiment of the invention, the granulated material is, after it has'been produced, first dried, preferably to residual moisture contents of less than 10% by weight of water, and then pressed to form green bodies.
A texture which may be obtained in the pressing procedure has, if the die is configured appropriately, an advantageous effect, for instance for use as a brake disc, since the C fibre bundles are preferentially aligned parallel to the flat surface of a flat disc, which also corresponds to the main stress direction.
In a preferred embodiment of the invention, such green bodies are then heated to from about 950 to 1050°C
under a protective gas atmosphere in a pyrolysis furnace or a vacuum reaction-sintering furnace to produce porous shaped bodies, preferably having a porosity of from about 30 to 50%, for a subsequent melt infiltration.
The melt infiltration which follows is preferably carried out using a silicon melt containing from about 10 to 50% by weight of iron and from about 0.5 to 10% by weight of chromium with the balance being silicon (based on the proportions by weight in the alloy).
Overall, this gives a reproducible and inexpen-sive manufacturing process which is suitable for mass production. Since virtually no shrinkage and internal stresses due to cooling occur, a significantly lower reject rate than in the case of conventional RB-SiC
ceramics is achieved and the need for final machining is considerably reduced, particularly in the case of iron-rich phases in the microstructure.
It will be self-evident to those skilled in the art that the features mentioned above and the features still to be described below can be used not only in the combination indicated in each case, but also in other combinations or alone without going outside the scope of the present invention.
In particular, it may be mentioned that the process of pan granulation is suitable not only for producing melt-infiltrated fibre-reinforced composite ceramics containing high-temperature-resistant ceramic fibres which are reaction-bonded to a matrix based on Si and containing additions of iron, chromium, titanium, molybdenum, nickel or aluminium, but can also be used With considerable advantage for producing such composite ceramics in which a pure silicon melt is used for melt infiltration.
Further features and advantages of the invention may be found in the following description of preferred illustrative embodiments with reference to the drawings.
Fig. 1 schematically shows a reaction-sintering furnace for melt infiltration;
Fig. 2 schematically shows a pelletizing pan which is used for pan granulation, with the path of individual particles being indicated;
Fig. 3 shows a plan view of the pelletizing pan of Fig. 2 from the front side;
Fig. 4 shows an optical micrograph of the microstructure of a composite ceramic according to the invention;
and Fig. 5 shows an enlarged section of the microstructure shown in Fig. 4.
A distinguishing aspect of the process of the invention is that the final step for producing the fibre-reinforced composite ceramic, namely the melt infilitration, is not carried out using a pure silicon melt as in the prior art, but instead additions of iron, chromium, titanium, molybdenum, nickel and/or aluminium are added to the melt.
Independently of this, the porous shaped body which is impregnated with liquid metal in the melt infiltration can be produced in various ways.
The process of the invention thus makes possible the infiltration of C hard felts and other fibre compo-sites and also the production of ceramics reinforced 2-and 3-dimensionally with continuous fibres.
The shaped bodies can thus be produced, for instance, by known lamination techniques, for example using synthetic resins, or else by pressing processes, with the green bodies being converted by pyrolysis into porous shaped bodies, is particular C-bonded shaped bodies, which are permeated by a complete pore network and thus, in the subsequent melt infiltration, draw in the liquid melt by means of the capillary forces within the porous.shaped body, in a similar manner to a wick or sponge.
Apart from the conventional lamination technique which, as described above, can be used for carrying out the invention, particular preference is given according to the invention to a pan granulation process for produc-ing short-fibre-reinforced melt-infiltrated composite ceramics.
The following description of the process variants for producing shaped bodies thus relates only to the production of short-fibre ceramics. However, it should be stated that it is also possible to use, as an alterna-tive, conventional lamination methods.
Example 1 The starting materials used are summarized in Table 1.
Compound Designation Source Data TM
SiC SM93 IndustriekeramikS,,.03:3.1 m~/a high-purity TM
Carbon black Printex 140 Degussa U
Graphite KS 6 Timcal Short C fibre SGL carbon 3aua, 12,000 bundles fil.
TM
Methyl- Tylose 4000 Hoechst I
cellulose G4 I
ester TM
Polyvinyl Moviol 10-74 Hoechst alcohol FeSi(65 or FeSi75 or FESIL Grain size:
' 75) FeSi65 5-30 ~n ~ FeCr(65 % Ferrochrom FESIL Grain size:
by mass of Cr) affine- 5-30 mm Table 1 1.1 Pan granulation In a tuanble mixer, 344 g of SiC powder, 48 g of graphite powder and 8 g of carbon black were intensively mixed at 50 rpm for three hours. Subsequently, 200 g of pitch-coated short C fibre bundles were added and mixed into the powder mixture for 5 minutes at 10 rpm. This mixture was transferred to a pelletizing pan 24 as shown in Fig. 2 and 3 and subjected to a rolling-mixing motion at 30 rpm and a pan inclination angle of about 40°. 240 g of the aqueous binder solution as per Tab3e 1 consisting of 1% by weight of Tylose 4000 G4 and 0.5% by weight of Moviol 10-74 dissolved in demineralized water were sprayed in via nozzles from spray lines 36 for a period of 3 minutes.
In Figs 2 and 3, the paths of small particles are indicated schematically by 28 and those of larger par-ticles are indicated schematically by 34. Additional mixing can be achieved by means of an additional mixing pan 26 as shown in Fig. 3. In this method of pan granu-lation, the distribution of the components in the granu-lated material being fozzned and also the granule size can be influenced by varying various parameters such as rotational speed and angle of inclination of the pellet-izing pan 24, rotational speed of the additional mixing pan 26, location of the spray nozzles for introduction of the binder solution, type and amount of binder solution added, etc.
Overall, the pan granulation can be adjusted so that granule-formation which is gentle on the carbon fibre bundles is obtained together with a uniform, homogeneous distribution of the individual components.
The granulated material produced preferably has a par-ticle size of from about 3 to 6 mm.
The pan granulation can be carried out either batchwise, in which case the granulated material obtained is subsequently sieved to obtain the desired particle size fraction, or else can be carried out continuously as shown in Fig. 3. In this variant, dry mix is continuously introduced as indicated by the reference numeral 32 and binder solution is sprayed in via the lines 36 and, at the same time, finished granulated material is discharged continuously in the region 30 of the pelletizing pan.
The granulated material formed in this way was dried to a moisture content of less than ~10~.
. CA 02284614 1999-09-21 1.2. Shapinc3 56.9 g of the granulated material were trans-ferred to a pressing die having a diameter of 60 xcan and pressed to a height of 13.6 mm by means of a hydraulic press using a pressure of 20 MPa. This gave a mechanic-ally stable green body which could be transported.
1.3. Pyrolysis The green body obtained above was taken from the pressing die, transferred to a pyrolysis furnace and heated at a rate of 10 K/min to 1000°C under a nitrogen atmosphere. In the pyrolysis, the organic binder consti-tuents were degraded to carbon. The resulting porous shaped body had a weight of 55.8 g and a porosity of 39%.
1.4. Melt infiltration A carbonized shaped body as obtained in section 1.3. and having a mass of 20 g was transferred to a graphite crucible coated with boron nitride, covered with 22 g of a granulated FeSi alloy consisting of 75% by weight of Si and 25% by weight of Fe and heated at 10 R/min to 1550°C under reduced pressure. This tempera-ture Was held for 30 minutes and the crucible was then cooled to room temperature.
This procedure gave a dense, crack- and pore-free shaped body having a density of 3.1 g/cm3 whose external geometric dimensions corresponded to those of the shaped body initially placed in the crucible.
Instead of placing the shaped body directly in a graphite crucible 20 coated with boron nitride, an alternative possibility is, as shown in Fig. 1, to use a porous SiC charging plate 16 in the furnace chamber 12 of a reaction-sintering furnace 10; this SiC'charging plate 16 stands on feet 18 in the melt 22 of the graphite .- CA 02284614 1999-09-21 crucible 20 coated with boron nitride or is connected therewith_via porous wicks. In this variant, a larger amount of granulated material for producing the melt 22 can be introduced into the crucible 20 since the melt 22 rises from below through the porous feet 18 and the porous charging plate 16 into the shaped body 14.
Example 2 A green body was produced as described above by pan granulation and subsequent pressing and subjected to pyrolysis in the above-described manner in a pyrolysis furnace.
The shaped body obtained in this way and having a mass of 20 g was again transferred to a graphite crucible coated with boron nitride, covered with 22 g of a mixture of 19 g of a granulated FeSi alloy consisting of 75% by weight of Si and 25% by weight of Fe to which 3 g of granulated FeCr (65% by weight of chromium) had been added and the crucible was heated at 10 K/min to 1700°C under reduced pressure. This temperature was held for 30 minutes. The crucible was then cooled to room temperature.
This procedure gave a dense, crack- and pore-free shaped body having a density of 3.2 g/cm' whose external geometric dimensions corresponded to those of the shaped body initially placed in the crucible.
Figs 4 and 5 show optical micrographs of polished sections of specimens which were produced as described in Example 1.
In Fig. 4, a C fibre bundle can be seen in the left-hand half of the picture while part of the next C
fibre bundle is visible at the bottom right-hand corner of the picture. The numeral 40 denotes carbon foxed by pyrolysis while the numeral 42 denotes C fibres.
Secondary SiC formed from the reaction of carbon fibres with silicon is present at the edge of the C fibre bundle;
this secondary SiC is denoted by the numeral 48.
The light-coloured phase denoted by the numeral 44 is silicon or Si/Fe/Cr. The dark grey phase denoted by 46 is SiC.
In the enlarged view shown in Fig. 5, in which a carbon fibre bundle is cut virtually perpendicularly across, the individual C fibres can readily be seen. The secondary SiC which has been formed from the reaction of C
fibres and is denoted by the numeral 48 can also be readily seen.
It can easily be seen that the carbon fibre bundle is retained virtually unscathed and only a few of the C
fibres in the outer region have been converted into secondary SiC.
This explains the considerable increase in strength which is achieved by the gentle treatment of the C fibre bundles in the pan granulation and in the subsequent process steps.
The foregoing disclosure has been set forth merely to illustrate the invention and is not intended to be limiting. Since modifications of the disclosed embodiments incorporating the spirit and substance of the invention may occur to persons skilled in the art, the invention should be construed to include everything within the scope of the appended claims and equivalents thereof.
Claims (47)
1. ~A melt-infiltrated fibre-reinforced composite ceramic comprising high-temperature-resistant fibres reaction-bonded to a matrix comprising a silicon alloy of silicon and iron.
2. ~The melt-infiltrated fibre-reinforced composite ceramic of Claim 1, wherein the high-temperature-resistant fibres comprise Si, C, B or N.
3. ~The composite ceramic of Claim 1 or 2, further comprising chromium, titanium, aluminium, nickel or molybdenum or a combination of chromium with titanium, aluminium, nickel or molybdenum as passive layer formers.
4. ~The composite ceramic of Claim 1, wherein the matrix contains from 0:5 to 80% by weight of iron.
5. ~The composite ceramic of Claim 4, wherein the matrix contains from 5 to 50% by weight of iron.
6. ~The composite ceramic of Claim 3, wherein the silicon alloy contains from 0.03 to 40% by weight of chromium.
7. ~The composite ceramic of Claim 6, wherein the matrix contains from 1 to 40% by weight of chromium.
8. ~The composite ceramic of Claim 7, wherein the matrix contains from 1 to 10% by weight of chromium.
9. ~The composite ceramic of Claim 1, wherein the fibres are C fibres or SiC fibres.
10. ~The composite ceramic of Claim 1, wherein the fibres are collected together to form fibre bundles and are surface-impregnated.
11. ~The composite ceramic of Claim 10, wherein the fibre-bundles are short-fibre bundles.
12. ~The composite ceramic of Claim 11, wherein the fibres comprise C filaments having mean diameters of from about 5 to 12 µm and a length of from about 2 to 10 mm and the fibre bundles contain from about 3,000 to 14,000 filaments.
13. ~A process for producing a fibre-reinforced composite ceramic comprising high-temperature-resistant fibres reaction-bonded to a silicon-based matrix, comprising the following steps:
producing a green body from fibres using binders and fillers by winding, lamination or pressing;
pyrolysing the green body under reduced pressure or protective gas in a temperature range from about 800°C to 1,200°C to produce a porous shaped body and infiltrating the porous shaped body with a silicon melt which comprises silicon and iron.
producing a green body from fibres using binders and fillers by winding, lamination or pressing;
pyrolysing the green body under reduced pressure or protective gas in a temperature range from about 800°C to 1,200°C to produce a porous shaped body and infiltrating the porous shaped body with a silicon melt which comprises silicon and iron.
14. ~The process of Claim 13, wherein the high-temperature-resistant fibres comprise Si, C, B or N.
15. ~The process of Claim 13, wherein the silicon melt further comprises chromium, titanium, aluminium, nickel or molybdenum or a combination of chromium with titanium, aluminium, nickel or molybdenum as passive layer formers.
16. ~The process of Claim 13, wherein the silicon melt contains from 0.5 to 80% by weight of iron.
17. ~The process of Claim 15, wherein the silicon melt contains from 0.5 to 80% by weight of iron.
18. ~The process of Claim 16, wherein the silicon melt contains from 5 to 50% by weight of iron.
19. ~The process of Claim 17, wherein the silicon melt contains from 5 to 50% by weight of iron.
20. ~The process of Claim 19, wherein the silicon melt contains from 0.03 to 40% by weight of chromium.
21. ~The process of Claim 20, wherein the silicon melt contains from 1 to 40% by weight of chromium.
22. ~The process of Claim 21, wherein the silicon melt contains from 1 to 10% by weight of chromium.
23. ~The process of Claim 16, wherein the fibres used are C fibres or SiC fibres.
24. ~The process of Claim 16, wherein the fibres are collected together to form fibre bundles and are surface-impregnated.
25. ~The process of Claim 24, wherein the fibre bundles are short-fibre bundles.
26. The process of Claim 25, wherein the fibre bundles used are formed by from about 3,000 to 14,000 C filaments having mean diameters of from about 5 to 10 µm and a length of from about 2 to 10 mm.
27. The process of Claim 25, wherein the green body is produced by dry pressing or hot flow moulding of a granulated material.
28. The process of Claim 26, wherein the green body is produced by dry pressing or hot flow moulding of a granulated material.
29. The process of Claim 27, wherein the granulated material is produced by pan granulation.
30. The process of Claim 28, wherein the granulated material is produced by pan granulation.
31. The process of Claim 29, in which the granulated material is produced continuously or batchwise and has a mean particle size of from about 2 to 6 mm.
32. The process of Claim 30, in which the granulated material is produced continuously or batchwise and has a mean particle size of from about 2 to 6 mm.
33. The process of Claim 13, wherein carbon-containing fillers are added in the production of green body.
34. The process of Claim 33, wherein the carbon-containing fillers comprise carbon black or graphite.
35. The process of Claim 13, wherein fillers in the form of silicides are added in the production of the green body.
36. The process of Claim 29, wherein a dry mixture of short-fibre bundles and fillers is first premixed and is subsequently mixed with binders in a pelletizing pan to produce the granulated material.
37. The process of Claim 30, wherein a dry mixture of short-fibre bundles and fillers is first premixed and is subsequently mixed with binders in a pelletizing pan to produce the granulated material.
38. The process of Claim 34, wherein a granulated material is produced from about 20 to 60% by weight of SiC
powder, about 2 to 2% by weight of carbon in the form of graphite powder or carbon black, about 10 to 40% by weight of C fibre bundles (12K bundles) and about 15 to 40% by weight of a binder solution, with the latter being sprayed into a pelletizing pan.
powder, about 2 to 2% by weight of carbon in the form of graphite powder or carbon black, about 10 to 40% by weight of C fibre bundles (12K bundles) and about 15 to 40% by weight of a binder solution, with the latter being sprayed into a pelletizing pan.
39. The process of Claim 37, wherein the granulated material is produced from about 20 to 60% by weight of SiC
powder, about 2 to 20% by weight of carbon in the form of graphite powder or carbon black, about 10 to 40% by weight of C fibre bundles (12K bundles) and about 15 to 40% by weight of a binder solution, with the latter being sprayed into a pelletizing pan.
powder, about 2 to 20% by weight of carbon in the form of graphite powder or carbon black, about 10 to 40% by weight of C fibre bundles (12K bundles) and about 15 to 40% by weight of a binder solution, with the latter being sprayed into a pelletizing pan.
40. The process of Claim 38, wherein the binder solution is an aqueous binder solution containing from 0.01 to 10%
by weight of methylcellulose esters and polyvinyl alcohol.
by weight of methylcellulose esters and polyvinyl alcohol.
41. The process of Claim 39, wherein the binder solution is an aqueous binder solution containing from 0.01 to 10%
by weight of methylcellulose esters and polyvinyl alcohol.
by weight of methylcellulose esters and polyvinyl alcohol.
42. The process of Claim 29, wherein the granulated material is dried after it has been produced and is subsequently pressed to form the green body.
43. The process of Claim 30, wherein the granulated material is dried after it has been produced and is subsequently pressed to form the green body.
44. The process of Claim 13, wherein the green body is heated to from about 950 to 1,050°C under a nitrogen atmosphere in a pyrolysis furnace to produce the porous shaped body.
45. The process of Claim 13, wherein the green body is converted in the pyrolysis into a shaped body having a porosity of from about 30 to 50%.
46. The process of Claim 13, wherein the porous shaped body is infiltrated with a silicon melt containing from about 10 to 50% by weight of iron with the balance being silicon.
47. The process of Claim 15, wherein the porous shaped body is infiltrated with a silicon melt containing from about 10 to 50% by weight of iron, from 0.5 to 10% by weight of chromium and silicon as the balance.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19711831A DE19711831C2 (en) | 1997-03-21 | 1997-03-21 | Melt-infiltrated fiber-reinforced composite ceramics and method for producing such |
DE19711831.3 | 1997-03-21 | ||
PCT/EP1998/000951 WO1998042634A1 (en) | 1997-03-21 | 1998-02-19 | Fibre-reinforced composite ceramics infiltrated with molten metal |
Publications (2)
Publication Number | Publication Date |
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CA2284614A1 CA2284614A1 (en) | 1998-10-01 |
CA2284614C true CA2284614C (en) | 2005-11-29 |
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CA002284614A Expired - Fee Related CA2284614C (en) | 1997-03-21 | 1998-02-19 | Fibre-reinforced composite ceramics infiltrated with molten metal |
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EP (1) | EP0968151B1 (en) |
JP (1) | JP3309225B2 (en) |
KR (1) | KR20000076057A (en) |
CN (1) | CN1253537A (en) |
BR (1) | BR9808622A (en) |
CA (1) | CA2284614C (en) |
DE (2) | DE19711831C2 (en) |
ES (1) | ES2166157T3 (en) |
PL (1) | PL335817A1 (en) |
RU (1) | RU99122347A (en) |
WO (1) | WO1998042634A1 (en) |
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US7169465B1 (en) | 1999-08-20 | 2007-01-30 | Karandikar Prashant G | Low expansion metal-ceramic composite bodies, and methods for making same |
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US7104177B1 (en) * | 2000-01-11 | 2006-09-12 | Aghajanian Michael K | Ceramic-rich composite armor, and methods for making same |
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-
1997
- 1997-03-21 DE DE19711831A patent/DE19711831C2/en not_active Expired - Fee Related
-
1998
- 1998-02-09 JP JP54441298A patent/JP3309225B2/en not_active Expired - Lifetime
- 1998-02-19 WO PCT/EP1998/000951 patent/WO1998042634A1/en not_active Application Discontinuation
- 1998-02-19 DE DE59801773T patent/DE59801773D1/en not_active Expired - Lifetime
- 1998-02-19 ES ES98913564T patent/ES2166157T3/en not_active Expired - Lifetime
- 1998-02-19 CN CN98804449A patent/CN1253537A/en active Pending
- 1998-02-19 PL PL98335817A patent/PL335817A1/en unknown
- 1998-02-19 KR KR1019997008145A patent/KR20000076057A/en not_active Application Discontinuation
- 1998-02-19 EP EP98913564A patent/EP0968151B1/en not_active Expired - Lifetime
- 1998-02-19 RU RU99122347/03A patent/RU99122347A/en unknown
- 1998-02-19 BR BR9808622-7A patent/BR9808622A/en not_active IP Right Cessation
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EP0968151A1 (en) | 2000-01-05 |
JP3309225B2 (en) | 2002-07-29 |
JP2000512260A (en) | 2000-09-19 |
CN1253537A (en) | 2000-05-17 |
DE19711831A1 (en) | 1998-09-24 |
EP0968151B1 (en) | 2001-10-17 |
KR20000076057A (en) | 2000-12-26 |
DE59801773D1 (en) | 2001-11-22 |
PL335817A1 (en) | 2000-05-22 |
BR9808622A (en) | 2000-05-16 |
ES2166157T3 (en) | 2002-04-01 |
CA2284614A1 (en) | 1998-10-01 |
RU99122347A (en) | 2005-01-27 |
DE19711831C2 (en) | 2000-07-13 |
WO1998042634A1 (en) | 1998-10-01 |
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