Ex parte KRAFT et al. - Page 3




          Appeal No. 97-2228                                                          
          Application 08/509,259                                                      


               The references relied upon by the examiner as evidence of              
          anticipation and obviousness are:                                           
          Parkes                        4,162,136           Jul. 24, 1979             
          Rimkunas et al. (Rimkunas)    5,407,321           Apr. 18, 1995             
                                                  (filed Nov. 29, 1993)               
               Claims 1 through 4 and 10 through 12 stand rejected under              
          35 U.S.C. § 102(e) as being anticipated by Rimkunas, and claims 5           
          through 9 stand rejected under 35 U.S.C. § 103 as being                     
          unpatentable over Rimkunas in view of Parkes.                               
               Reference is made to the appellants’ brief (Paper No. 10)              
          and to the examiner’s answer (Paper No. 14) for the respective              
          positions of the appellants and the examiner with regard to the             
          merits of these rejections.                                                 
               Turning first to the standing 35 U.S.C. § 102(e) rejection,            
          anticipation is established only when a single prior art                    
          reference discloses, expressly or under principles of inherency,            
          each and every element of a claimed invention.  RCA Corp. v.                
          Applied Digital Data Sys., Inc., 730 F.2d 1440, 1444, 221 USPQ              
          385, 388 (Fed. Cir. 1984).                                                  
               Rimkunas discloses an airfoil vibration damper.  Although              
          the damper is specifically described for use with hollow stator             
          vane airfoils disposed in the compressor section of a gas turbine           
          engine, Rimkunas indicates that the damper can be utilized in               

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