Ex parte HENSELER et al. - Page 3




          Appeal No. 95-2124                                                          
          Application 08/076,789                                                      


               Rather than reiterate the arguments of the appellants and              
          the examiner, reference is made to the brief, reply brief, the              
          examiner’s answer and supplemental answer for the full details              
          thereof.                                                                    
                                       OPINION                                        
               We have carefully reviewed the rejection on appeal in light            
          of the arguments of the appellants and the examiner.  As a result           
          of this review, we have reached the determination that the                  
          applied prior art does not establish a prima facie case of                  
          obviousness with respect to the subject matter of the claims on             
          appeal.  Therefore, the rejections of the claims on appeal are              
          reversed.  Our reasoning follows.                                           
               The examiner has rejected claim 5 under 35 U.S.C. § 103 as             
          unpatentable over Bishop.                                                   
               We are in agreement with the examiner that Bishop discloses            
          a casing 56 covering the airbag which is stored in a folded                 
          condition.  The following is Bishop’s disclosure with respect               
          to the casing 56:                                                           
                    The material (sack, band, etc.) 56 is chosen                      
                    of a material having a tensile strength                           
                    sufficient to maintain the bag 32 in its                          
                    predeployment condition.  The strength of the                     
                    material 56 is such that during initial                           
                    deployment thereof, the deployment forces are                     
                    sufficient to rupture it thereby permitting                       
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