FR2649393A1 - BORON NITRIDE COATING, PROCESS FOR PRODUCING SUCH A COATING ON FIBERS AND COMPOSITE MATERIAL COMPRISING FIBERS SO COATED - Google Patents
BORON NITRIDE COATING, PROCESS FOR PRODUCING SUCH A COATING ON FIBERS AND COMPOSITE MATERIAL COMPRISING FIBERS SO COATED Download PDFInfo
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- FR2649393A1 FR2649393A1 FR9008623A FR9008623A FR2649393A1 FR 2649393 A1 FR2649393 A1 FR 2649393A1 FR 9008623 A FR9008623 A FR 9008623A FR 9008623 A FR9008623 A FR 9008623A FR 2649393 A1 FR2649393 A1 FR 2649393A1
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- B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
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- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
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- C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
- C04B35/628—Coating the powders or the macroscopic reinforcing agents
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Abstract
La présente invention concerne un revêtement de nitrure de bore, ledit revêtement ayant une épaisseur d'au moins 0,40 micromètre, entourant des fibres destinées à être enrobées à l'intérieur d'une matrice. Ce revêtement est caractérisé en ce qu'il est suffisant pour inhiber à la fois la liaison physique et l'interaction chimique entre la matrice et les fibres, la résistance à la rupture étant augmentée par déviation et émoussement des criques, ce qui provoque une saillie des fibres, lorsqu'une contrainte est appliquée au système de matrice/fibres.The present invention relates to a boron nitride coating, said coating having a thickness of at least 0.40 microns, surrounding fibers to be coated within a matrix. This coating is characterized in that it is sufficient to inhibit both the physical bond and the chemical interaction between the matrix and the fibers, the tensile strength being increased by deflection and blunting of the cracks, causing protrusion. fibers, when stress is applied to the matrix / fiber system.
Description
La présente invention concerne le revêtement de fibres et spécialement leThe present invention relates to the coating of fibers and especially the
revêtement de fibres au moyen d'une couche épaisse de nitrure de bore ainsi que les fibres fiber coating by means of a thick layer of boron nitride and the fibers
revêtues résultantes.resulting coatings.
Le renforcement, au moyen de fibres, de matériaux en verre, vitrocéramique, céramique, métal, thermodurcissables et thermoplastiques, peut augmenter leur résistance, en The reinforcement, by means of fibers, of glass, glass-ceramic, ceramic, metal, thermosetting and thermoplastic materials, can increase their resistance,
élargissant ainsi l'éventail de leurs applications possibles.. thus expanding the range of their possible applications.
Cependant des forces de liaison élevées entre fibres et matrice, spécialement dans le cas de matériaux composites en céramique, peuvent provoquer une rupture de fragilité qui se traduit par des surfaces de rupture sensiblement planes, ne possédant pratiquement pas de fibres en saillie, et provoquant une diminution de la résistance à la rupture. Des fibres en saillie augmentent la distance traversée par les fissures amorces de rupture, augmentant leur surface However, high bonding strengths between fibers and matrix, especially in the case of ceramic composite materials, can cause a brittle fracture which results in substantially planar failure surfaces having substantially no protruding fibers and causing decrease in breaking strength. Projecting fibers increase the distance traversed by the crack initiation cracks, increasing their surface
spécifique et la résistance du composite. specific and the strength of the composite.
L'application d'un revêtement, par exemple de carbone, sur les fibres, préalablement à la formation d'une matrice, peut réduire la force de liaison entre fibres et matrice et l'interaction chimique, améliorant la résistance à la rupture. Les revêtements de carbone (voir par exemple les brevets US NO 4 425 407 et 4 731 298 cités en tant que référence) qui sont facilement oxydés et sont de bons conducteurs électriques, ont vu leur utilisation limitée dans Applying a coating, for example carbon, to the fibers, prior to matrix formation, can reduce the bond strength between fibers and matrix and the chemical interaction, improving the breaking strength. Carbon coatings (see, e.g., U.S. Patent Nos. 4,425,407 and 4,731,298 cited as reference) which are readily oxidized and are good electrical conductors, have seen their limited use in
certaines conditions.certain conditions.
Le nitrure de bore, possédant une grande résistance électrique, une résistance excellente aux chocs thermiques et une non-combustibilité, est, de façon similaire, utilisé en tant que revêtement de fibres (voir le brevet US N 4 642 271 cité à titre de référence). En raison de sa structure plane hexagonale similaire au graphite, le nitrure de bore est similaire au carbone, sans présenter certaines des limitations de celuici, et il constitue un produit de remplacement intéressant. Les revêtements de nitrure de bore peuvent être appliqués en utilisant la technique DCV (dépôt chimique sous vapeur) dans des domaines de température d'environ 850"C à environ 2200 C. Cependant des revêtements stoechiométriques en nitrure de bore n'ont été obtenus qu'à des températures de dépôt supérieures à 17000C, températures qui, habituellement, provoquent une dégradation significative de la fibre. Lorsque les fibres sont chauffées à de telles températures, refroidies, et testées à température ambiante, elles ne conservent pas leur résistance originelle. De plus les revêtements en nitrure de bore, tels que ceux réalisés suivant l'art antérieur, sont des revêtements fins, généralement inférieurs à 0,35 micromètre, et des revêtements épais sont seulement obtenus à des températures au-dessus de 1400"C (brevet US 4 481 257 cité à titre de référence). En conséquence on continue les recherches pour améliorer les Boron nitride, having high electrical resistance, excellent thermal shock resistance and non-combustibility, is similarly used as a fiber coating (see US Patent No. 4,642,271 cited for reference ). Because of its hexagonal planar structure similar to graphite, boron nitride is similar to carbon without any of its limitations, and it is an interesting substitute. Boron nitride coatings can be applied using DCV (Chemical Vapor Deposition) in temperature ranges from about 850 ° C to about 2200 ° C. However, stoichiometric boron nitride coatings have only been obtained on at deposition temperatures above 17000C, temperatures which usually cause significant fiber degradation When the fibers are heated to such temperatures, cooled, and tested at room temperature, they do not retain their original strength. more boron nitride coatings, such as those made in the prior art, are thin coatings, generally less than 0.35 micron, and thick coatings are only obtained at temperatures above 1400 ° C (patent US 4,481,257 cited for reference). As a result, research is continuing to improve
revêtements de fibres et les méthodes d'application. fiber coatings and methods of application.
La présente invention concerne le revêtement de fibres avec du nitrure de bore afin d'augmenter la résistance à la rupture et de diminuer les réactions chimiques entre les fibres et la matrice. Les fibres sont placées à l'intérieur d'un réacteur DCV et sont chauffées. Les gaz réactifs, contenant à la fois du bore et de l'azote, sont introduits dans le réacteur au moyen d'un gaz vecteur. Les gaz réagissent pour produire du nitrure de bore, le dépôt se réalise, et un revêtement épais (c'est-àdire supérieur à 0,40 micromètre) de nitrure de bore est formé autour des fibres; cette épaisseur étant nécessaire pour obtenir la résistance désirée et diminuer la réaction chimique entre les fibres et la matrice. On décrira ci-après, à titre d'exemple non limitatif, une forme d'exécution de ia présente invention, en référence au dessin annexé sur lequel: La figure 1 représente un graphique de la variation de la résistance à la flexion, en fonction de la température, de fibres revêtues et non-revêtues à l'intérieur d'un The present invention relates to the coating of fibers with boron nitride in order to increase the tensile strength and to decrease the chemical reactions between the fibers and the matrix. The fibers are placed inside a DCV reactor and are heated. The reactive gases, containing both boron and nitrogen, are introduced into the reactor by means of a carrier gas. The gases react to produce boron nitride, deposition occurs, and a thick (ie, greater than 0.40 micron) coating of boron nitride is formed around the fibers; this thickness being necessary to obtain the desired resistance and to reduce the chemical reaction between the fibers and the matrix. One embodiment of the present invention will be described hereinafter by way of nonlimiting example, with reference to the appended drawing, in which: FIG. 1 represents a graph of the variation of the bending strength, as a function of temperature, coated and uncoated fibers inside a
matériau composite.composite material.
Les figures 2A,2B et 2C représentent une comparaison des surfaces de rupture pour différentes épaisseurs du FIGS. 2A, 2B and 2C show a comparison of the fracture surfaces for different thicknesses of the
revêtement en nitrure de bore.boron nitride coating.
La figure 3 représente un ensemble réacteur DCV FIG. 3 represents a DCV reactor assembly
utilisé dans l'application du revêtement en nitrure de bore. used in the application of boron nitride coating.
La rupture de fragilité est un problème important dans les matériaux composites en céramique constitués de fibres non-revêtues, ou revêtues très finement, enrobées dans une matrice de céramique. La fragilité des matériaux composites provoque des criques, provenant de fissures dues aux contraintes, qui se propagent en ligné droite à travers le matériau composite. Cependant, si les fibres à l'intérieur de la matrice sont suffisamment revêtues de nitrure de bore, le revêtement de nitrure de bore augmente la résistance à la rupture, par une déviation et un émoussement des criques, empêchant la rupture de fragilité. L'application d'une contrainte au matériau composite comportant des fibres revêtues de nitrure de bore provoque une saillie des fibres, a l'opposé d'une surface de rupture lisse. Cependant tous les revêtements de nitrure de bore n'aboutissent pas à une saillie des fibres. En effet si l'épaisseur du revêtement de nitrure de bore se situe autour ou au-dessous de 0,30 micromètre, il en résulte une surface de fracture lisse, similaire à celle des matériaux composites contenant des Brittle fracture is a significant problem in ceramic composite materials made of uncoated fibers, or very finely coated, embedded in a ceramic matrix. The fragility of composite materials causes cracks, resulting from cracks due to stresses, which propagate in a straight line through the composite material. However, if the fibers inside the matrix are sufficiently coated with boron nitride, the boron nitride coating increases the breaking strength, by deflection and blunting of the cracks, preventing breakage of brittleness. The application of a stress to the composite material comprising boron nitride-coated fibers causes the fibers to protrude away from a smooth fracture surface. However, all boron nitride coatings do not result in a protrusion of the fibers. Indeed, if the thickness of the boron nitride coating is around or below 0.30 micrometer, a smooth fracture surface results, similar to that of composite materials containing
fibres non-revêtues.uncoated fibers.
La figure 1 représente la variation de la résistance à la flexion de matériaux composites à fibres connues sous le nom de "NEXTEL", revêtues et non-revêtues, enrobées dans une matrice de verre. Le matériau composite comportant des fibres revêtues de nitrure de bore suivant l'invention (courbe 1), possède une résistance à la flexion significativemenit plus grande que celle du matériau composite comportant des fibres Figure 1 shows the variation in flexural strength of fiber composite materials known as "NEXTEL", coated and uncoated, embedded in a glass matrix. The composite material comprising boron nitride-coated fibers according to the invention (curve 1) has a significantly greater flexural strength than that of the composite material comprising fibers.
non-revêtues ( courbe 5).uncoated (curve 5).
Les figures 2A,2B, et 2C montrent une comparaison de surfaces de rupture pour un revêtement de nitrure de bore d'une épaisseur de 0,08 micromètre (figure 2A) et de 0,16 micromètre (figure 2B) (comme revendiqué dans le brevet US N04 642 271). Les deux surfaces montrent des surfaces de rupture relativement lisses. La figure 2C, quant à elle, montre une saillie sensible des fibres pourvues d'un revêtement de nitrure de bore d'une épaisseur de 1,14 micromètre. Différentes fibres; telles que des fibres à base de nitrure de silicium, de mullite et d'alumine, peuvent être utilisées dans ce procédé, des fibres en "Nextel 480" produites par la Société 3M, Co., MN et A1203 de SUMITOMO étant préférées. Des matrices telles que des matrices de verre, vitrocéramique, céramique, (incluant le carbure de silicium CVI et le nitrure de silicium), de matériaux thermoplastiques, de matériaux thermodurcissables et de métal, peuvent être utilisées pour enfermer les fibres FIGS. 2A, 2B, and 2C show a comparison of fracture surfaces for a boron nitride coating with a thickness of 0.08 micrometer (FIG. 2A) and 0.16 micrometer (FIG. 2B) (as claimed in FIG. U.S. Patent No. 4,642,271). Both surfaces show relatively smooth fracture surfaces. As for FIG. 2C, it shows a sensitive projection of the fibers provided with a boron nitride coating with a thickness of 1.14 microns. Different fibers; such as silicon nitride, mullite and alumina fibers can be used in this process, "Nextel 480" fibers produced by SUMITOMO Company 3M, Co., MN and A1203 being preferred. Matrices such as glass, glass-ceramic, ceramic matrices (including CVI silicon carbide and silicon nitride), thermoplastic materials, thermosetting materials and metal can be used to enclose the fibers.
mentionnées précédemment.previously mentioned.
De plus, différents gaz réactifs contenant du bqre et de l'azote peuvent également être utilisés; BC13 (trichlorure de bore) et NH3 (ammoniac) ont démontré leur capacité. Ces gaz réactifs sont introduits dans le réacteur In addition, different reactive gases containing beer and nitrogen may also be used; BC13 (boron trichloride) and NH3 (ammonia) have demonstrated their capacity. These reactive gases are introduced into the reactor
par un gaz vecteur.by a vector gas.
L'hydrogène (H2), souvent utilisé comme gaz vecteur, a démontré son incapacité pour ce procédé. L'hydrogène provoque une dégradation et un affaiblissement des fibres. Un gaz inerte, tel que de l'argon (Ar), dégrade habituellement moins les fibres que le gaz habituel H2. Il en résulte qu'un gaz inerte, l'argon en particulier, a été utilisé comme gaz Hydrogen (H2), often used as a carrier gas, has demonstrated its inability for this process. Hydrogen causes degradation and weakening of the fibers. An inert gas, such as argon (Ar), usually degrades the fibers less than the usual H2 gas. As a result, an inert gas, argon in particular, has been used as a gas
vecteur pour cette invention.vector for this invention.
Le tableau suivant montre les résultats de fibres de "Nextel 480" revêtues portées à la température indiquée The following table shows the results of coated "Nextel 480" fibers at the specified temperature
pendant 3 minutes avec H2 ou Ar comme gaz vecteur. for 3 minutes with H2 or Ar as carrier gas.
à____________at____________
Gaz vecteur: Temp.OC: Résistance à la traction RT (MPa) Vector gas: Temp.OC: RT tensile strength (MPa)
H2: 1050: 1068H2: 1050: 1068
H2: 1080: 841H2: 1080: 841
H2: 1100: trop faible pour être testé Ar: 1050: 2604 Ar: 1060: 1729 Ar: 1100: 889 Ar: 1150: 675 Ar: 1200: 579 La présente invention sera clarifiée par référence H2: 1100: too weak to be tested Ar: 1050: 2604 Ar: 1060: 1729 Ar: 1100: 889 Ar: 1150: 675 Ar: 1200: 579 The present invention will be clarified by reference
aux exemples ci-après.to the examples below.
Exemple 1:Example 1
5. La procédure suivante a été utilisée (figure 3) pour former un revêtement en nitrure de bore sur des fibres "Nextel 480", 1. Un mandrin de graphite 10, de 5,8 cm de diamètre (0,3 mm d'épaisseur de paroi) et 10, 2 cm de long, qui comporte des fibres "Nextel" 11 disposées à l'intérieur, est chargé dans un réacteur DCV 12 de 7,6 cm de diamètre et de 40,6 cm de longueur (voir 5. The following procedure was used (FIG. 3) to form a boron nitride coating on "Nextel 480" fibers. 1. A graphite mandrel 10, 5.8 cm in diameter (0.3 mm diameter wall thickness) and 10.2 cm long, which has "Nextel" fibers 11 disposed therein, is loaded into a DCV reactor 12 7.6 cm in diameter and 40.6 cm in length (see FIG.
figure 3).Figure 3).
2. Le réacteur est mis sous pression à 27 Pa, par un générateur de vide 13 et chauffé à 2. The reactor is pressurized to 27 Pa, by a vacuum generator 13 and heated to
10500C.10500C.
3. Les gaz réactif et vecteur sont amenés à s'écouler dans le réacteur 12, en passant à travers des vannes à trois voies 14, des débitmètres 15 et des vannes à aiguille 16: BC13 à 67 cm3/min, NH3 à 67 cm3/min et Ar à approximativement 208 cm3/min, pendant 3 minutes, ce qui produit un revêtement de nitrure de bore d'approximativement 1,3 3. The reactant and carrier gases are allowed to flow into the reactor 12, passing through three-way valves 14, flow meters 15 and needle valves 16: BC13 at 67 cc / min, NH3 at 67 cc / min and Ar at approximately 208 cm3 / min, for 3 minutes, resulting in a coating of approximately 1.3 boron nitride
micromètre d'épaisseur.micrometer thickness.
Exemple 2:Example 2
Les paramètres donnés dans l'exemple 1 sont suivis, et en changeant la fibre "Nextel 480" pour une fibre "Sumitomo", on peut obtenir un revêtement d'approximativement The parameters given in Example 1 are followed, and by changing the fiber "Nextel 480" for a fiber "Sumitomo", it is possible to obtain a coating of approximately
0,80 micromètre d'épaisseur.0.80 micrometer thick.
L'épaisseur du revêtement, donnée dans les exemples 1 et 2, peut être augmentée en modifiant la concentration de BC13 et de NE3 (diminution de la quantité de gaz vecteur Ar) The thickness of the coating, given in Examples 1 and 2, can be increased by modifying the concentration of BC13 and NE3 (reduction of the amount of carrier gas Ar)
ou en augmentant le temps de réaction. or by increasing the reaction time.
Claims (7)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US37737789A | 1989-07-07 | 1989-07-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2649393A1 true FR2649393A1 (en) | 1991-01-11 |
Family
ID=23488872
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9008623A Pending FR2649393A1 (en) | 1989-07-07 | 1990-07-06 | BORON NITRIDE COATING, PROCESS FOR PRODUCING SUCH A COATING ON FIBERS AND COMPOSITE MATERIAL COMPRISING FIBERS SO COATED |
Country Status (4)
Country | Link |
---|---|
JP (1) | JPH03115140A (en) |
DE (1) | DE4021243A1 (en) |
FR (1) | FR2649393A1 (en) |
GB (1) | GB2236540A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0453704A2 (en) * | 1990-04-23 | 1991-10-30 | Corning Incorporated | Coated silicon nitride fiber reinforcement materials and glass or glass-ceramic composites comprising the same |
Families Citing this family (13)
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US5842342A (en) * | 1997-02-21 | 1998-12-01 | Northrop Grumman Corporation | Fiber reinforced ceramic matrix composite internal combustion engine intake/exhaust port liners |
US8105690B2 (en) | 1998-03-03 | 2012-01-31 | Ppg Industries Ohio, Inc | Fiber product coated with particles to adjust the friction of the coating and the interfilament bonding |
US6593255B1 (en) | 1998-03-03 | 2003-07-15 | Ppg Industries Ohio, Inc. | Impregnated glass fiber strands and products including the same |
US6419981B1 (en) | 1998-03-03 | 2002-07-16 | Ppg Industries Ohio, Inc. | Impregnated glass fiber strands and products including the same |
US6770176B2 (en) | 2002-08-02 | 2004-08-03 | Itn Energy Systems. Inc. | Apparatus and method for fracture absorption layer |
US8062746B2 (en) | 2003-03-10 | 2011-11-22 | Ppg Industries, Inc. | Resin compatible yarn binder and uses thereof |
EP1640352B1 (en) * | 2004-09-28 | 2007-05-30 | General Electric Company | Low cost manufacturing process for high performance ceramic matrix composites |
US7867554B2 (en) * | 2005-01-06 | 2011-01-11 | United Technologies Corporation | Boron nitride coated fibers and composite articles containing same |
US8242375B2 (en) | 2008-09-18 | 2012-08-14 | United Technologies Corporation | Conductive emissions protection |
US8524317B2 (en) * | 2010-09-30 | 2013-09-03 | United Technologies Corporation | Composite article and method therefor |
CA2974485C (en) | 2014-12-12 | 2024-01-16 | Kyoto University | Silicon carbide fiber reinforced silicon carbide composite material |
CN105016631A (en) * | 2015-07-20 | 2015-11-04 | 湖北菲利华石英玻璃股份有限公司 | Boron nitride-coated quartz fiber preparation method |
CN107326648A (en) * | 2017-06-30 | 2017-11-07 | 长兴泓矿炉料有限公司 | A kind of bibulous mullite fiber fire smothering blanket |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2505009A1 (en) * | 1974-02-07 | 1975-08-14 | Ciba Geigy Ag | PROCESS FOR COATING INORGANIC SUBSTRATES WITH CARBIDES, NITRIDES AND / OR CARBONITRIDES |
EP0172082A1 (en) * | 1984-07-20 | 1986-02-19 | SOCIETE EUROPEENNE DE PROPULSION (S.E.P.) Société Anonyme dite: | Method of making a composite material with refractory fibre reinforcement and ceramic matrix, and structure obtained thereby |
EP0209320A1 (en) * | 1985-07-10 | 1987-01-21 | Hitachi, Ltd. | Fiber-reinforced ceramics |
US4642271A (en) * | 1985-02-11 | 1987-02-10 | The United States Of America As Represented By The Secretary Of The Navy | BN coating of ceramic fibers for ceramic fiber composites |
EP0216932A1 (en) * | 1985-03-04 | 1987-04-08 | Research Development Corporation of Japan | Rhombohedral polycrystalline boron nitride and process for its production |
EP0222960A1 (en) * | 1985-11-18 | 1987-05-27 | Battelle Memorial Institute | Method and apparatus for the on-line coating of silica based fibers with boron-nitride |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1358140A (en) * | 1962-05-31 | 1964-04-10 | Gen Electric | High strength fused silica fibers |
GB2014972B (en) * | 1977-12-29 | 1982-04-28 | Defence Secret Of State For | Boron nitride fibre |
US4481257A (en) * | 1979-11-26 | 1984-11-06 | Avco Corporation | Boron coated silicon carbide filaments |
ZA833150B (en) * | 1982-05-28 | 1984-01-25 | Int Standard Electric Corp | Coating an optical fibre |
-
1990
- 1990-07-03 GB GB9014729A patent/GB2236540A/en not_active Withdrawn
- 1990-07-04 DE DE4021243A patent/DE4021243A1/en not_active Withdrawn
- 1990-07-06 JP JP2179400A patent/JPH03115140A/en active Pending
- 1990-07-06 FR FR9008623A patent/FR2649393A1/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2505009A1 (en) * | 1974-02-07 | 1975-08-14 | Ciba Geigy Ag | PROCESS FOR COATING INORGANIC SUBSTRATES WITH CARBIDES, NITRIDES AND / OR CARBONITRIDES |
EP0172082A1 (en) * | 1984-07-20 | 1986-02-19 | SOCIETE EUROPEENNE DE PROPULSION (S.E.P.) Société Anonyme dite: | Method of making a composite material with refractory fibre reinforcement and ceramic matrix, and structure obtained thereby |
US4642271A (en) * | 1985-02-11 | 1987-02-10 | The United States Of America As Represented By The Secretary Of The Navy | BN coating of ceramic fibers for ceramic fiber composites |
EP0216932A1 (en) * | 1985-03-04 | 1987-04-08 | Research Development Corporation of Japan | Rhombohedral polycrystalline boron nitride and process for its production |
EP0209320A1 (en) * | 1985-07-10 | 1987-01-21 | Hitachi, Ltd. | Fiber-reinforced ceramics |
EP0222960A1 (en) * | 1985-11-18 | 1987-05-27 | Battelle Memorial Institute | Method and apparatus for the on-line coating of silica based fibers with boron-nitride |
Non-Patent Citations (1)
Title |
---|
PATENT ABSTRACTS OF JAPAN, File supplier JAPS. &JP-A-62070533(Toyota Motor Co.)01.04.1987 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0453704A2 (en) * | 1990-04-23 | 1991-10-30 | Corning Incorporated | Coated silicon nitride fiber reinforcement materials and glass or glass-ceramic composites comprising the same |
EP0453704A3 (en) * | 1990-04-23 | 1993-03-10 | Corning Incorporated | Coated silicon nitride fiber reinforcement materials and glass or glass-ceramic composites comprising the same |
Also Published As
Publication number | Publication date |
---|---|
GB2236540A (en) | 1991-04-10 |
JPH03115140A (en) | 1991-05-16 |
DE4021243A1 (en) | 1991-01-17 |
GB9014729D0 (en) | 1990-08-22 |
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