Ex Parte GROSS et al - Page 4




         Appeal No. 2003-1788                                                       
         Application No. 09/403,081                                                 


              A “burner” is a device that produces a flame.  It must mix            
         the fuel and an oxidizing agent in proportions that are within             
         the limits of flammability for ignition as well as for steady              
         combustion.  See page 9-15 of Chemical Engineers’ Handbook, fifth          
         edition, 1973.1                                                            
              The aforementioned definition of a “burner” reinforces                
         appellants’ position made on page 7 of the Brief that their                
         reaction chamber 8 functions differently from a burner.  The               
         definition also reinforces our finding that Gitman’s chamber 102           
         is part of the burner means.  Gitman can introduce the remaining           
         feed gas, if any, to chamber 102 via line 108, in combination              
         with oxygen feed.  See page 13, lines 5-25.                                
              On the other hand, no feed gas is introduced into                     
         appellants’ region 8.  For example, figures 1-3 of the                     
         specification each depicts that there are no lines for feeding             
         feed gas into combustion chamber 8.  Only inner tube 11 exists             
         for feeding only oxygen gas (or an oxygen-rich gas) to combustion          
         reactor 8.  No lines are indicated for use in introducing a feed           
         gas.  Outer tube 12 (depicted in each of appellant’s figures) is           
         used to introduce a protecting gas to cool nozzle (9).                     
              Appellant’s specification also indicates that an                      
         afterburning zone is produced in reaction chamber 8 by highly              
         turbulent self-priming oxygen jets.  In this way, the already              
         processed gas from the burner is subjected to complete                     
         afterburning in combustion reactor 8.  In this way, the reactions          
         taking place in the combustion chamber 8 proceed closer to the             
         thermodynamic equilibrium.  See specification page 7, line 37              
         through page 8, line 6.  The oxygen is blown in, at high                   
         velocity, into the combustion reactor 8.  See specification, page          

                                                                                   
         1 A copy of pages 9-15 from Chemical Engineers’ Handbook, Fifth            
         Edition, 1973, is provided herewith.                                       
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