Ex parte AGAHI et al. - Page 8




          Appeal No. 1997-0287                                                        
          Application 08/263,034                                                      

          pressurized fluid to hydrostatic journal bearings 50, 51 and                
          thrust bearings 52, 53 as backup for magnetic journal                       
          bearings 20, 21 and magnetic thrust bearings 22, 23 to support              
          the shaft temporarily.  The source of the pressurized fluid                 
          may be taken from the process fluid outlet duct 15 by the                   
          fluid line 62 .  The hydrostatic bearing system does not                    
                       1                                                              
          provide a control passage between a high-pressure zone and a                
          low-pressure zone to control the axial displacement of the                  
          rotor.  Accordingly, the rejection of claims 5, 11, and 14-18               
          over Andres and New is reversed.                                            

          Andres and Swearingen '689 or Swearingen '768                               
               Swearingen '689 and Swearingen '768, which are assigned                
          to the assignee of the present application and disclosed as                 
          prior art (specification, page 2), disclose turbo machinery                 
          having mechanisms for adjusting thrust loading in conjunction               
          with conventional thrust bearings.  Swearingen '689 and '768                
          show a passage between high- and low-pressure zones, a control              
          valve in the passage, and a controller for controlling the                  
          axial thrust by opening and closing the valve.  Swearingen                  
          '689 controls the valve based on sensing the pressure of oil                
          between the thrust bearing parts, which is a measure of axial               
                                        - 8 -                                         





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