Ex parte KELLY et al. - Page 12




          Appeal No. 1997-0538                                                        
          Application No. 08/262,168                                                  


          Nilssen, 851 F.2d 1401, 1403, 7 USPQ2d 1500, 1502 (Fed. Cir.                
          1988)).  Rather, the test for obviousness is what the combined              
          teachings of the prior art references would have fairly                     
          suggested to those of ordinary skill in the art.  In re Young,              
          927 F.2d 588, 591, 18 USPQ2d 1089, 1091 (Fed. Cir. 1991); In                
          re Keller, 642 F.2d 413, 425, 208 USPQ 871, 881 (CCPA 1981).                
          In evaluating the prior art references, it is proper to take                
          into account not only the specific teachings of the references              
          but also the inferences which one skilled in the art would                  
          reasonably be expected to draw therefrom.  In re Preda, 401                 
          F.2d 825, 826, 159 USPQ 342, 344 (CCPA 1968).                               
               Here, as indicated supra, we find that Kim discloses                   
                    a method for producing articles of gamma                          
               titanium aluminide alloy having improved properties                    
               which comprises the steps of:(a)shaping the article                    
               at a temperature in the approximate range of about                     
               130° C. below the titanium-aluminum eutectoid                          
               temperature of  the alloy to about 20° C. below the                    
               alpha-transus temperature of the alloy for about 15                    
               to 120 minutes; (b) heat treating the thus-shaped                      
               article at about the alpha-transus temperature of                      
               the alloy for about 15 to 20 minutes; and (c) aging                    
               the thus-heat treated article at a temperature                         
               between about 750° and 1050° C. for about 4 to 300                     
               hours.                                                                 
          See column 2, lines 47-57.                                                  

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