Ex Parte BOUTAGHOU et al - Page 2




          Appeal No. 2001-1268                                                        
          Application No. 09/100,698                                                  


          the advantage over the prior art lies in the reduction of static            
          friction, or “stiction,” caused by formation of a liquid meniscus           
          between the air bearing structure and the disc surface, due to              
          the unavoidable presence of water vapor within the disc drive               
          housing.  While the prior art sought to overcome the stiction               
          problem by adding landing pads extending beyond the air bearing             
          surfaces in the direction of the disc, reducing contact area                
          between the head assembly and the disc, this also served to limit           
          the proximity of the transducer on the head assembly to the disc.           
          In attempts to increase proximity of transducer to disc, the                
          height of the landing pads was reduced, but this increased                  
          stiction.                                                                   
               While prior art designers were faced with mutually                     
          contradictory alternatives for allowing for increased areal                 
          recording density by lowering the height of the landing pads, or            
          reducing the stiction by raising the height of the landing pads,            
          the instant invention is said to overcome this mutually exclusive           
          requirement by decoupling the overall height of the landing pads            
          from the extent by which the landing pads extend below the air              
          bearing surfaces.  This is accomplished by providing recessed               
          surfaces from which the landing pads extend.  Accordingly, the              
          overall height of the landing pad features can be optimized to              

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