Ex Parte RIOJA et al - Page 14


               Appeal No. 2004-0109                                                                                                   
               Application 09/324,549                                                                                                 

               of alloys B and D are virtually identical at Aging Conditions 4 through 7, including Aging                             
               Condition 6, the so-called “T8 condition,” and within 1 ksi at Aging Conditions 2, 3 and 8;  and                       
               that the ksi of alloys C and D are virtually identical at Aging Condition 8, the difference between                    
               alloys C and D being about 1 ksi at Aging Condition 7, about 2 ksi at Aging Conditions 2, 3 and                        
               6, and about 3 ksi at Aging Conditions 4 and 5.                                                                        
                       Based on the limitation “the alloy is capable of attaining a yield strength (L) above about                    
               80 ksi” (emphasis supplied), we find that alloys B and D achieved this level when worked at                            
               Aging Conditions 2 through 5, 7 and 8, alloys B and D being at about 78 ksi when worked at                             
               Aging Condition 6, with alloy C being at about 80 ksi for each of the Aging Conditions.                                
                       We find no explanation in the specification of the significance of the differences in the                      
               Aging Conditions employed.  Appellants disclose that “t]he aluminum alloy comprises . . . from                         
               about 0.10 to about 0.99% lithium” and that “[i]t has been found . . . ancillary additions of low                      
               levels of lithium to aluminum-zinc alloys provided a high strength . . . that exhibits good fracture                   
               toughness . . . over aluminum-zinc alloys without lithium additions and those aluminum-zinc                            
               alloys having lithium additions above 1.0 wt %” (page 1, line 27, to page 2, line 7).  Appellants                      
               further disclose with respect to “strength” that “the alloy of the invention has good strength . . . .                 
               The yield strength (L) of the alloys of the invention are preferably above about 80 ksi and more                       
               preferably above about 85 ksi” (id., page 4, lines 7-10).                                                              
                       Appellants, in describing the results shown in specification FIG. 1, state only that “[i]t                     
               will be seen that the alloys having lithium additions[, that is, alloys B, C and D,] exhibit greater                   
               strength than those without lithium[, that is, alloy A], while at the same time exhibiting thermal                     
               stability” (id., page 9, lines 15-17).  No distinction in result between alloys B, C and D is set                      
               forth in the specification, the distinction being drawn only with respect to alloys B, C and D as a                    
               whole vis-à-vis alloy A in support of the disclosure of the disclosed aluminum alloy having                            
               lithium between 0.10 and 0.99 wt % lithium.  There is no other evidence in the specification with                      
               respect to alloy D.                                                                                                    
                       With respect to the disclosure that “[t]he alloy of the invention will also preferably have a                  
               combination of (i) good strength and (ii) fracture toughness of preferably (i) above 80 ksi and (ii)                   
               above 30 ksi√inch” (specification, page 4, lines 13-16), and the claimed limitation “the alloy is                      


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