Ex Parte Grossklaus et al - Page 3



                Appeal 2007-0164                                                                             
                Application 10/286,122                                                                       

                      We have thoroughly reviewed each of Appellants’ arguments for                          
                patentability.  However, we are in complete agreement with the Examiner                      
                that the claimed subject matter would have been obvious to one of ordinary                   
                skill in the art within the meaning of § 103 in view of the applied prior art.               
                Accordingly, we will sustain the Examiner’s rejections for the reasons set                   
                forth in the Answer, which we incorporate herein, and we add the following                   
                for emphasis only.                                                                           
                      Appellants do not dispute the Examiner’s factual determination that:                   
                            Mehta et al[.] teach repair of metallic portions of metal                        
                      articles by a laser cladding process that concurrently applies a                       
                      powder metal and the laser beam to the surface to be repaired,                         
                      that was damaged during manufacture, thermal cycling, wear,                            
                      etc., noting that alternative conventional localized repair means,                     
                      such as electron beam welding or arc welding, adversely affect                         
                      properties of materials of construction due to relatively high                         
                      heat input that results in distortion in affected zones (col. 1,                       
                      especially ll. 21-31).                                                                 
                Answer 3, last paragraph.  As pointed out by the Examiner, Mehta expressly                   
                teaches that the disclosed process can be used to repair “aircraft gas turbine               
                engine components” that are damaged “from manufacturing error as well as                     
                from operational thermal cycling, wear, part interference, etc.” (col. 2,                    
                ll. 41-43).  In addition, Mehta teaches that “[a]lthough such damage can                     
                occur to stationary as well as rotating parts, damage is particularly critical in            
                the rotating components because of the stresses generated in operation,                      
                during rotation (col. 2, ll. 46-50, emphasis added).                                         


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