Ex Parte FORTUNA et al - Page 7




              Appeal No. 2001-1628                                                                  Page 7                
              Application No. 09/054,794                                                                                  


              particular findings related thereto.  See Dembiczak, 175 F.3d at 999, 50 USPQ2d at                          
              1617.  Broad conclusory statements standing alone are not "evidence."  Id.                                  


                     In this case, we find no motivation, suggestion or teaching in the combined                          
              teachings of the applied prior art (Koshoffer, Shekleton and Ekstedt (U.S. Patent No.                       
              3,899,884 incorporated by reference in Koshoffer)) to have modified the gas turbine                         
              engine combustion system of Koshoffer to have arrived at the claimed subject matter.                        
              In that regard, we note that the examiner has not produced any evidence that any of the                     
              fuel-air mixers of the applied prior art experienced coking problems.  While Ekstedt                        
              does discuss the problem of coking in his discussion of prior art nozzles, Ekstedt                          
              teaches (column 4, lines 19-23) that his combustion system is highly effective in                           
              preventing carbon buildup on fuel nozzles.  Since the examiner has not set forth any                        
              evidence that Koshoffer's venturi suffers from coking, there is no reason for a person of                   
              ordinary skill in the art at the time the invention was made to have modified Koshoffer's                   
              system to prevent coking on the venturi.  Moreover, Shekleton does not teach or                             
              suggest an air passage wherein purge airflow is discharged into the venturi substantially                   
              parallel to the longitudinal axis of the venturi sufficient to provide a boundary layer of air              
              along the inner surface of the wall of the venturi.  The airflow discharged from                            
              Shekleton's air assist tube 34 while flowing into the venturi 26 substantially parallel to                  
              the longitudinal axis of the venturi is not sufficient to provide a boundary layer of air                   








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