Ex parte SANSONE - Page 9




          Appeal No. 1997-4044                                       Page 9           
          Application No. 08/504,233                                                  


               process operations. The pressure is then released                      
               allowing the inflatable mandrel to deflate and collapse,               
               facilitating removal of the mandrel from the interior of               
               the composite shell. Upon removal from the composite                   
               shell, the inflatable mandrel may be immediately readied               
               for another composite fabrication process.                             

          Lastly, Davis teaches that the hollow inflatable, elastomer                 
          mandrel can be reinforced with only polar windings (column 8,               
          lines 25-26) which are shown in Figure 8.                                   


               Boxmeyer discloses an inflatable structural                            
          column/member.  As set forth in the abstract, the inflatable                
          structural column/member has                                                
               a substantially tubular shape and sealed at both ends,                 
               includes an inner lining to maintain internal pressure                 
               upon inflation. The inner lining is covered with a                     
               filament reinforced matrix structure comprising resin                  
               impregnated filaments of high tensile strength. The                    
               uninflated structural member is stowable in a collapsed                
               condition. Curing of the resin matrix is inhibited by                  
               storing the collapsed member at a low temperature. Prior               
               to use, the member is inflated with a fluid and heated to              
               enable curing of the resin matrix.                                     

          As shown in Figure 3, and enlarged in Figure 3A, the filament               
          reinforced matrix structure includes a first layer of                       
          filaments 304 spirally wound in the first direction 204 (see                
          Figure 2), a second layer of longitudinal filaments 306 which               







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