Ex parte BOUZIDI et al. - Page 3




                 Appeal No. 1998-2265                                                                                                                   
                 Application No. 08/498,482                                                                                                             


                                   wherein said precipitation heat treating is                                                                          
                                   conducted at a temperature of 730-800EC for 1-2                                                                      
                                   hours, and                                                                                                           
                                   said alloy 718 consists essentially of, in                                                                           
                                   percent by weight:                                                                                                   
                                   Cr 17 to 21; Fe 16.5 to 20.5; Nb + Ta 4.75 to                                                                        
                                   5.5;                                                                                                                 
                                   Mo 2.8 to 3.3; Ti 0.75 to 1.15; Al 0.3 to 0.7;                                                                       
                                   C 0.02 to 0.08; Mn below 0.35; Cu below 0.3; Co                                                                      
                                   below 1;                                                                                                             
                                   B below 0.006; P below 0.015; S below 0.015;                                                                         
                                   Si below 0.35; Bi below 0.0001; Ag below 0.0005;                                                                     
                                   Pb below 0.001; and Ni as the remainder.                                                                             
                          The examiner relies upon the following prior art                                                                              
                 reference as evidence of unpatentability:                                                                                              
                 Daniel A. DeAntonio, David Duhl, Timothy Howson, and Michael                                                                           
                 F. Rothman, Heat Treating of Superalloys, in 4 ASM HANDBOOK                                                                            
                 793-814 (Steven R. Lampman, Theodore B. Zorc, Janice L.                                                                                
                 Daquila, Alice W. Ronke, Kari L. Henniger, Robert T. Kiepura,                                                                          
                 Heather F. Lampman, Penelope Thomas & Nikki D. Wheaton eds.                                                                            
                 1990) (ASM Handbook).2                                                                                                                 




                          2Notwithstanding the statement on page 3 of the                                                                               
                 examiner’s answer that “[n]o prior art is relied upon... in                                                                            
                 the rejection of the claims under appeal” (p. 3), the examiner                                                                         
                 refers to the ASM Handbook in the rejection (p. 4) and in the                                                                          
                 “Response to argument” section (p. 6).                                                                                                 
                                                                           3                                                                            





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