Ex Parte Bray - Page 5




               Appeal No. 2006-1669                                                                        Page 5                
               Application No. 10/476,257                                                                                        


               retracted, its extended position 12a or 14a during cruise, and its retracted position when the                    
               aircraft is undergoing severe flight loads.                                                                       
                      The examiner considers Allen’s winglet to correspond to the “winglet” recited in claim 1                   
               and the aileron illustrated thereon in Figure 1 but not numbered or discussed by Allen to be a                    
               control surface meeting the limitations of the “air flow control arrangement …” limitation of                     
               claim 1 (answer, p. 4).  As discussed more fully below, we agree with the examiner.                               
                      The appellant argues throughout the brief and reply brief that Allen’s winglet, despite                    
               Allen’s use of the terminology “winglet,” is not in fact a “winglet” as one of ordinary skill in the              
               art would understand that term, because it is not fixed in an upturned or vertical position on the                
               wing.  Even accepting the definition of “winglet” as “a small, nearly vertical surface mounted at                 
               the tip of an aircraft wing to decrease drag resistance” urged by the appellant on page 8 of the                  
               brief, we find nothing in this definition that requires the winglet to be fixedly mounted to the                  
               wing as the appellant contends.  Furthermore, even assuming that one of ordinary skill in the art                 
               would have an understanding that winglets are typically upturned surfaces fixed at the tip of an                  
               aircraft wing, Allen evidences a recognition in the art at the time of the appellant’s invention that             
               winglets need not be fixedly mounted and that, indeed, there are advantages to winglets which                     
               can be moved between upturned and extended positions during flight.  Although not relied upon                     
               by the examiner in the rejection of claim 1 as being anticipated by Allen, the patents to Daude                   
               (US Pat. No. 4,457,479, issued July 3, 1984) and Brix (US Pat. No. 6,345,790, issued February                     
               12, 2002) alluded to by the examiner on page 8 of the answer are further evidence of the                          
               recognition in the art at the time of the appellant’s invention of the advantages of moveably                     
               mounting winglets or portions of winglets on aircraft wings.                                                      
                      Allen’s disclosed improvement of an actuator and control system for moving the winglet                     
               between retracted or folded and extended positions no more detracts from it being a “winglet”                     
               than does appellant’s improvement of a control surface on the winglet detract from it being a                     









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