BRIEF DESCRIPTION OF THE DRAWINGS
The invention, together with objects and advantages thereof, may best be understood by reference to the following description of the presently preferred embodiments together with the accompanying drawings in which:
FIG. 1A is a front cross-sectional view of a stator and a rotor of a motor according to a first embodiment embodying the present invention;
FIG. 1B is a partially enlarged front cross-sectional view of FIG. 1A;
FIG. 2 is a front cross-sectional view of the stator and the rotor of FIG. 1A;
FIG. 3 is a perspective view of the stator of FIG. 1A;
FIG. 4 is a view showing a wave winding of the windings in the stator of FIG. 1A;
FIG. 5A is a graph showing a FEM (Finite Element Method) analysis example of the torque constant of the rotor 15 and the first to the fourth comparative rotors 21 to 24;
FIG. 5B is a graph showing the FEM analysis example of the torque ripple of the rotor 15 and the first to the fourth comparative rotors 21 to 24;
FIG. 6 is a graph showing a relationship between angular width A of circumferential portions 19A, 19B of the rotor 15 and the torque ripple.
FIGS. 7(
a
1), 7(b1), 7(c1), 7(d1), 7(e1), and 7(f1) are graphs showing FEM (Finite Element Method) analysis examples of changes in magnetic flux of a single tooth when the angular range A is changed;
FIGS. 7(
a
2), 7(b2), 7(c2), 7(d2), 7(e2), and 7(f2) are graphs showing FEM (Finite Element Method) analysis examples of changes in the sum of magnetic fluxes at all the teeth when the angular range A is changed.
FIG. 8A is a graph showing a FEM (Finite Element Method) analysis example of changes in magnetic flux of a single tooth of the rotor 15 and rotor 24 when the angular range A is 20°.
FIG. 8B is a graph showing a FEM (Finite Element Method) analysis example of changes in magnetic flux of a single tooth of the rotor 15 and rotor 24 when the angular range A is 20°.
FIG. 9A is a partial cross-sectional view.
FIG. 9B is a partially enlarged cross-sectional view.
FIG. 10A is a graph showing an appropriate range of the inter-bridge angle Θb.
FIG. 10B is a graph showing an appropriate range of the angular width A.
FIG. 10C is a graph showing an appropriate range of the depth Dh.
FIGS. 10D, 10E and 10F are graphs showing force acting on the teeth.
FIG. 11A is a graph showing the force acting on the teeth;
FIG. 11B is a graph showing the torque fluctuation;
FIG. 12A is a partial front cross-sectional view showing a first comparative rotor 21;
FIG. 12B is a partial front cross-sectional view showing a second comparative rotor 22;
FIG. 12C is a partial front cross-sectional view showing a third comparative rotor 23;
FIG. 12D is a partial front cross-sectional view showing a fourth comparative rotor 24;
FIG. 13A is a graph showing the FEM analysis example of change in the torque ripple rate ratio Rx/Ri when the angular width A of the rotor 15 is changed;
FIG. 13B is a graph showing determination of an appropriate range of combination of the angular width A and depth Dh for obtaining a torque ripple rate ratio Rx/Ri of less than 1; and
FIG. 14 is side cross-sectional view of an entire compressor to which the present invention is applied.