Ex Parte Gregg et al - Page 8



             Appeal 2007-0118                                                                                    
             Application 10/175,612                                                                              
                          disclosure is unlikely to be productive of the result                                  
                          sought by the applicant.                                                               
             In re Gurley, 27 F.3d 551, 552-53, 31 USPQ2d 1130, 1131 (Fed. Cir. 1994)                            
             (citations omitted).                                                                                

                                                  ANALYSIS                                                       
                   The Examiner has failed to set forth a prima facie case of obviousness                        
             because he failed to explain how Henne teaches or suggests coupling a baseline                      
             trailing edge wedge to a wing, as required in independent claims 1, 2, 11, and 12,                  
             and a trailing edge wedge coupled to a wing structure, as required in independent                   
             claims 6 and 16.  While we agree with the Examiner that Allen and Vijgen                            
             demonstrate that it was known at the time of the invention to provide spanwise                      
             modificiations to trailing edges of wings to optimize the aerodynamic properties of                 
             an airfoil (Findings of Fact 9-16), we find that Henne fails to teach or suggest                    
             coupling a trailing edge wedge to a wing and, in fact, Henne teaches away from                      
             such a coupling (Finding of Fact 6).  We also find no motivation in the prior art to                
             modify the airfoil design of Henne by coupling a trailing edge wedge to Henne’s                     
             airfoil (Finding of Fact 8).                                                                        

                                                  REMAND                                                         
                   With regard to claims 1-20, we note that U.S. Patent No. 4,542,868 to Boyd                    
             (“Boyd”) discloses a wedge-shaped flap (20) for attachment to or near the trailing                  
             edge (14) of an airfoil (10) to improve the coefficient of lift and reduce the                      
             coefficient of drag providing an overall increase in fuel economy at cruise                         

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