Ex parte SHIBAN et al. - Page 5




                     Appeal No.  1996-1141                                                                                                                                             
                     Application 08/109,166                                                                                                                                            


                     a second gas mixture comprising  pyrophoric gas (silane) into said chamber through a                                                                              
                     second outlet at a second position 16 (Fig. 1).  Soneta discloses that the second gas                                                                             
                                                                                                                                                  4                                    
                     mixture flows through a second inlet which is downstream of said first position.   Soneta                                                                         
                     teaches that the first flow of gas (air) and the second flow of gas (silane) are combined                                                                         
                     (column 6, lines 23-25).  Soneta discloses the first flow of gas (air) and the second flow of                                                                     
                     gas (silane) are burned through the reaction of the first flow of gas (air) and the second flow                                                                   
                     of gas (silane) in the combustion chamber (column 8, lines 10-13, and claim 1).                                                                                   
                                Soneta does not disclose the use of turbulence as required by appellants’ claim 20                                                                     
                     as a step within their method of burning exhaust gases containing gaseous silane.                                                                                 
                     Coldren teaches the use of turbulence to initiate a reaction between reactive gases                                                                               
                     in a reaction process which occurs at supersonic velocity (column 4, lines 70-73).  Coldren                                                                       
                     teaches a process for mixing reactive gases such as oxygen and hydrocarbons in which                                                                              
                     source streams of difference gases are divided into narrow small streams which                                                                                    
                     accelerate to supersonic velocity and then discharged into an elongated mixing zone so                                                                            
                     that each (except those at the periphery of the zone) is laterally adjacent to a plurality of                                                                     
                     narrow streams of another gas (column  1, lines 28-30 and column 2, lines 14-20).                                                                                 



                                4 We note that Figure 1 shows that air (first gas mixture) enters air feed pipe 9 and                                                                  
                     flows into air chamber 7 where air permeates through air permeable porous filler material                                                                         
                     19 and into the combustion chamber 5 downstream of the silane (second gas mixture)                                                                                
                     which enters the combustion chamber through exhaust introduction pipe 13.                                                                                         
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