Ex Parte Hirzel - Page 2

                   Appeal 2006-3366                                                                                                 
                   Application 10/864,041                                                                                           
                                                       BACKGROUND                                                                   
                           Appellant’s invention relates to a radial airgap, transverse flux motor.                                 
                   An understanding of the invention can be derived from a reading of                                               
                   exemplary claim 1, which is reproduced below.                                                                    
                               1.    A dynamoelectric machine, comprising:                                                          
                               (a) at least one stator assembly, a plurality of stator                                              
                           windings, and at least one rotor assembly supported for rotation                                         
                           about a rotational axis, said rotor and stator assemblies being                                          
                           concentric with said rotational axis;                                                                    
                               (b) said at least one rotor assembly comprising at least one                                         
                           rotor magnet structure, said magnet structure providing                                                  
                           magnetic poles having north and south polarity, said poles                                               
                           being disposed in at least two rotor layers that are substantially                                       
                           planar, perpendicular to said rotational axis, and axially spaced                                        
                           apart, each of said layers having the same number of poles, and                                          
                           said poles in each of said layers being disposed equiangularly                                           
                           about the circumference of said rotor assembly on a cylindrical                                          
                           periphery thereof;                                                                                       
                               (c) said at least one stator assembly comprising a plurality                                         
                           of stator cores, each of said stator cores terminating in a first                                        
                           and a second stator poleface and being comprised of laminated                                            
                           layers composed of a material selected from the group                                                    
                           consisting of amorphous, nanocrystalline, and flux enhancing                                             
                           Fe-based metal, said stator cores being disposed equiangularly                                           
                           about the circumference of said stator assembly, such that:                                              
                               (i) said first and second stator polefaces of each of said                                           
                           stator cores are situated on a cylindrical periphery of said stator                                      
                           assembly in axial alignment;                                                                             
                               (ii) said first stator polefaces are in a first stator layer                                         
                           radially adjacent one of said rotor layers; and                                                          
                               (iii) said second stator polefaces are in a second stator layer                                      
                           adjacent another of said rotor layers; and                                                               



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