Ex Parte SUNDHOLM - Page 5




              Appeal No. 2004-1977                                                               Page 5                
              Application No. 09/297,256                                                                               


                     We turn next to the rejection of claims 1-7 and 9-14 as being unpatentable over                   
              Diquattro in view of Lockwood.  Independent claim 1, as discussed above, calls for an                    
              extinguishing medium source consisting of a long (i.e., one hundred meters or more in                    
              length) tube.  Independent claims 13 and 14 recite an extinguishing medium source                        
              which consists essentially of a long tube which has a length of “at least two hundred                    
              meters” and “at least about 1 km,” respectively.                                                         
                     The examiner’s rejection of claims 1-7 and 9-14 suffers from the same deficiency                  
              as the above-discussed anticipation rejection of claim 1.  Specifically, the examiner has                
              not explained how Diquattro and Lockwood, even if combined, would have taught or                         
              suggested an extinguishing medium source which consists essentially of a tube of at                      
              least one hundred meters (claim 1), at least two hundred meters (claim 13) or at least                   
              about 1 km (claim 14).                                                                                   


                     Diquattro is directed to a coolant-dispensing system for preventing fire in, for                  
              example, a jet aircraft, by cooling hot metallic parts and comprises liquid coolant                      
              receptacles 16a-c in communication with medium under pressure in a receptacle 10 via                     
              a conduit 14 and manifold 12.  Valve 15 in conduit 14 is normally closed but is opened                   
              by a solenoid or other actuator under the control of a switch which responds to or is                    
              operated in anticipation of collision or crash of the aircraft to send the pressurized                   
              medium into receptacles 16a-c, thereby causing discs 28 in the outlets of the                            
              receptacles to burst releasing coolant to supply points 1-8.  The receptacles 16a-c may                  






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