US2002079623A1PendingUtilityA1

Method of forming a fiber-reinforced ceramic matrix composite

Priority: Nov 24, 1998Filed: Dec 18, 2001Published: Jun 27, 2002
Est. expiryNov 24, 2018(expired)· nominal 20-yr term from priority
C04B 2235/5268C04B 2235/96C04B 2235/9684C04B 2235/656C04B 2235/616C04B 2235/386C04B 2235/3826C04B 35/581C04B 35/62894C04B 2235/486C04B 2235/5264C04B 2235/5256C04B 2235/77C04B 2235/9615C04B 35/62863C04B 35/62873C04B 35/62868C04B 35/62871C04B 35/62897C04B 35/80C04B 35/6269C04B 2235/5244Y10T428/2938Y10T428/2964Y10T428/2971Y10T428/2916
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Claims

Abstract

This invention pertains to a method of forming a fiber-reinforced ceramic matrix composite comprising: (a) impregnating a ceramic fiber coated with at least one layer binary coating comprised of boron nitride and silicon nitride wherein the silicon nitride is applied over the boron nitride with a preceramic composition comprising a curable preceramic polymer; (b) forming the impregnated fibers into a desired shape; (c) curing the formed impregnated fibers; (d) heating the cured impregnated fibers of (c) to a temperature of at least 1000° C. in an inert atmosphere for a time effective to convert the preceramic polymer to a ceramic.

Claims

exact text as granted — not AI-modified
What is claimed is:  
     
         1 . A method of forming a fiber-reinforced ceramic matrix composite comprising: 
 (a) impregnating a ceramic fiber coated with at least one layer binary coating comprised of boron nitride and silicon nitride wherein the silicon nitride is applied over the boron nitride with a preceramic composition comprising a curable preceramic polymer;    (b) forming the impregnated fibers into a desired shape;    (c) curing the formed impregnated fibers;    (d) heating the cured impregnated fibers of (c) to a temperature of at least 1000° C. in an inert atmosphere for a time effective to convert the preceramic polymer to a ceramic.    
     
     
         2 . The method of  claim 1  wherein the cured impregnated fibers are heated in step (d) to a temperature of at least 1200° C.  
     
     
         3 . The method of  claim 1  wherein the preceramic composition additionally comprises fillers.  
     
     
         4 . The method of  claim 1  wherein there is an additional coating over the binary coating.  
     
     
         5 . The method of  claim 1  wherein the additional coating is silicon carbide.

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