Ex parte BANKS et al. - Page 10




                 Appeal No. 95-4237                                                                                                                     
                 Application 07/887,002                                                                                                                 


                 device to function in the manner called for in claim 1.   In                                       2                                   
                 light of these disclosures, the examiner anticipation                                                                                  
                 rejections based on Anxionnaz, Miller or Eknes are, at best,                                                                           
                 speculative.  Accordingly, a prima facie case of anticipation                                                                          
                 based on Anxionnaz, Miller or Eknes has not been established.                                                                          
                 See In re Oelrich, supra.                                                                                                              
                                              The § 102 rejection based on Lurz                                                                         
                                                              (rejection (d))                                                                           
                          We will sustain this rejection.                                                                                               
                          Lurz pertains to a method for stabilizing laminar flow                                                                        
                 over a disturbance in the surface contour of a body in the                                                                             
                 flow, e.g., where sheet metal layers overlap in the surface of                                                                         
                 an aircraft wing.  This is accomplished by providing a suction                                                                         
                 inlet section 6 in the form of a series of small openings in                                                                           
                 the body just upstream from the surface disturbance 1 in a                                                                             
                 high pressure zone 4, a blowing outlet section 6’ in the form                                                                          


                          2With respect to Eknes, while Figure 9 thereof                                                                                
                 illustrates fluid flow both into the plenum chamber via holes                                                                          
                 13 and out of the plenum chamber via holes 13a, the examiner                                                                           
                 is not understood to be relying on this embodiment in his                                                                              
                 anticipation rejection.  In any event, this embodiment does                                                                            
                 not appear to include anything that can be regarded as                                                                                 
                 corresponding to the transpirational control device required                                                                           
                 by claim 1.                                                                                                                            
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