Ex Parte MA - Page 7




            Appeal No. 2003-0659                                                                       
            Application 09/463,540                                                                     


            simultaneously reducing the concentrations of soot and oxides of                           
            nitrogen in internal combustion engine exhaust (col. 5, lines 29-                          
            32 and 45-48).  The thermal oxidizer (10a) includes a reductant                            
            delivery system (148) for injecting a reductant stream (7) into a                          
            process stream (9) which contains exhaust gas (col. 8, lines 12-                           
            17; col. 11, lines 4-6).  The reductant preferably is injected                             
            upstream of a matrix (14a), which is a bed of solid, heat                                  
            resistant media, to enable the reductant to be heated by the                               
            matrix and to enhance mixing (col. 8, lines 25-26; col. 11,                                
            lines 6-8).  The reductant also can be injected directly into the                          
            matrix, or can be combined with an air stream (4), fuel                                    
            stream (5) or hot gas stream (6), each of which is a component of                          
            the process stream (col. 11, lines 9-14; figure 1).                                        
                  The examiner argues that Martin discloses “periodically                              
            injecting reducing gases in bursts into the narrow chamber (88)”                           
            (answer page 6).  Martin calls chamber 88 a fuel vaporization                              
            chamber and discloses spraying supplemental fuel into that                                 
            chamber (col. 10, lines 38-53).  Even if the supplemental fuel                             
            can be considered a reducing gas,1 Martin does not disclose                                


                  1 Martin’s supplemental fuel stream (5) and reductant                                
            stream (7) are different streams (col. 10, lines 42-43; col. 11,                           
            lines 5-6).                                                                                
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