Ex Parte Spiess - Page 2



          Appeal No. 2006-1692                                        Παγε 2          
          Application No. 10/068,243                                                  

                                     BACKGROUND                                       
               The appellant's invention relates to a roller for conveyor             
          belts, which provides means for immediate visual inspection                 
          (specification, page 1).                                                    
          Claim 1 is representative of the invention, and is reproduced as            
          follows:                                                                    
                    1. An aircraft roller system comprising:                          
                    (1) a roller adapted to communicate cargo into and                
                         out of an aircraft, the roller being                         
                         cylindrical    in shape having a length and a                
                         diameter, the     roller having a center aperture            
                         extending through   the length of the roller and             
                         the roller being     fabricated from a polymer,              
                         the polymer having a     burn rate of less than              
                         4.0 inches per minute, a     compressibility                 
                         strength of a least 200 psi,     impact strength             
                         of at least 0.5(ft.lbs.)/inch,      flexural                 
                         strength of at least 20 psi;                                 
                    (2) a shaft in the form of an elongate cylinder                   
                         having a diameter sized to rotatably fit within              
                         the central aperture of the roller, the shaft                
                         further having means for retention located upon              
                         the shaft ends;                                              
                    (3) an elongate “U” shaped roller rack, the roller                
                    rack sized to extend the length of the roller                     
                    and        having a pair of upwardly extending ends               
                    located         adjacent the ends of the roller, each             
                    end having         an aperture sized to receive the               
                    respective shaft        end and located the shaft in a            
                    fixed location the        rack being joined to an                 
                    aircraft.                                                         
                                                                                     






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