Ex parte BRUN et al. - Page 2




          Appeal No. 1995-4981                                                        
          Application No. 08/248,583                                                  


          the application.  This appeal is related to Appeal No. 96-                  
          2829, an appeal from the final rejection of claims 10 through               
          12 in Application 08/403,356, which is directed to a fiber                  
          reinforced silicon carbide matrix.                                          
               Claim 10, the broadest claim in this application, reads                
          as follows:                                                                 
               10.  A method for forming a fiber reinforced composite,                
          the fibers being at least one of elemental carbon, or silcon                
          carbide, in a matrix of silicon carbide containing at least a               
          silicon carbide phase and elemental silicon phase formed by                 
          molten silicon infiltration comprising: depositing a                        
          continuous metal nitride coating on the fibers wherein the                  
          metal is selected from the group consisting of silicon,                     
          aluminum, titanium, zirconium, hafnium, niobium, or tantalum,               
          the metal nitride coating preventing reaction between the                   
          reinforcement fiber and molten silicon;                                     
               admixing a carbonaceous material with the coated fibers                
          so that at least 5 volume percent of the mixture is the coated              
          fibers;                                                                     
               forming the mixture into a preform having an open                      
          porosity ranging from about 25 volume percent to about 90                   
          volume percent of the preform;                                              
               heating the preform in an inert atmosphere or partial                  
          vacuum; and                                                                 
               infiltrating the heated preform with molten silicon to                 
          form the silicon carbide matrix composite.                                  
               As evidence of obviousness, the examiner relies on the                 
          following prior art:                                                        

                                          2                                           





Page:  Previous  1  2  3  4  5  6  7  Next 

Last modified: November 3, 2007