Segmented electrical machine
An electrical machine has a variable reluctance rotor, and a stator formed as an annular array of stator segments. The reluctance of the rotor-to-stator magnetic flux path varies with rotor position whereby the stator segments are magnetically energizable to rotate the rotor. The stator segments are arranged in the array such that, when energized to rotate the rotor, they produce an unbalanced force on the rotor. The machine further has a compensator including one or more balancing segments which are configured to be magnetically energizable to produce a balancing force on the rotor which balances the unbalanced force. The reluctance of the rotor-to-compensator magnetic flux path is substantially invariant with rotor position.
1. An electrical machine having:
a variable reluctance rotor, and
a stator formed as an annular array of stator segments, wherein reluctance of the rotor-to-stator magnetic flux path varies with rotor position, and wherein the stator segments are magnetically energizable to rotate the rotor;
wherein:
the stator segments are non-axisymmetrically distributed in the array such that, when energized to rotate the rotor, the stator segments produce an unbalanced force on the rotor; and
the electrical machine further has a compensator including one or more balancing segments, each balancing segment comprising a core structure and a conductor winding mounted to the core structure, the winding being configured to be magnetically energizable by electrical excitation by a control system to produce a balancing force on the rotor, wherein the balancing force balances the unbalanced force, wherein reluctance of a rotor-to-compensator magnetic flux path is substantially invariant with rotor position.
2. The electrical machine according to claim 1 , wherein the unbalanced force is radial or includes a radial component.
3. The electrical machine according to claim 1 , wherein the unbalanced force is axial or includes an axial component.
4. The electrical machine according to claim 1 , wherein the core structure of each of the one or more balancing segments has plural salient teeth projecting towards the rotor and arranged in a row that extends to either side of the conductor winding, and
wherein, to produce the substantially invariant reluctance of the rotor-to-compensator magnetic flux path, the teeth are unequally spaced to either side of the conductor winding and/or the teeth are of unequal width to either side of the conductor winding.
5. The electrical machine according to claim 1 , wherein, to produce the substantially invariant reluctance of the rotor-to-compensator magnetic flux path, the core structure of each of the one or more balancing segments forms air gaps with the rotor of unequal thickness to either side of the conductor winding.
6. The electrical machine according to claim 1 , wherein, to produce the substantially invariant reluctance of the rotor-to-compensator magnetic flux path, the core structure of each of the one or more balancing segments extends by different distances to either side of the conductor winding.
7. The electrical machine according to claim 1 , wherein the core structure of each of the one or more balancing segments is an E-core structure.
8. The electrical machine according to claim 1 , wherein the core structure of each of the one or more balancing segments is a U-core structure.
9. The electrical machine according to claim 8 , wherein the conductor winding has a thinner layer of conductors on a side of the winding distal from the rotor than on a side of the winding proximal the rotor.
10. The electrical machine according to claim 1 , wherein each of the one or more balancing segments incorporates a permanent magnet.
11. The electrical machine according to claim 1 , further having the control system for controlling the compensator to produce the balancing force.
12. A gas turbine engine including an electrical machine comprising:
a variable reluctance rotor, and
a stator formed as an annular array of stator segments, wherein reluctance of the rotor-to-stator magnetic flux path varies with rotor position, and wherein the stator segments are magnetically energizable to rotate the rotor;
wherein:
the stator segments are non-axisymmetrically distributed in the array such that, when energized to rotate the rotor, the stator segments produce an unbalanced force on the rotor; and
the electrical machine further has a compensator including one or more balancing segments, each balancing segment comprising a core structure and a conductor winding mounted to the core structure, the winding being configured to be magnetically energizable by electrical excitation by a control system to produce a balancing force on the rotor, wherein the balancing force balances the unbalanced force, wherein reluctance of a rotor-to-compensator magnetic flux path is substantially invariant with rotor position.
13. The gas turbine engine according to claim 12 , wherein the unbalanced force is radial or includes a radial component.
14. The gas turbine engine according to claim 12 , wherein the unbalanced force is axial or includes an axial component.
15. The gas turbine engine according to claim 12 , wherein the core structure of each of the one or more balancing segments has plural salient teeth projecting towards the rotor and arranged in a row that extends to either side of the conductor winding, and
wherein, to produce the substantially invariant reluctance of the rotor-to-compensator magnetic flux path, the teeth are unequally spaced to either side of the conductor winding and/or the teeth are of unequal width to either side of the conductor winding.
16. The gas turbine engine according to claim 12 , wherein, to produce the substantially invariant reluctance of the rotor-to-compensator magnetic flux path, the core structure of each of the one or more balancing segments forms air gaps with the rotor of unequal thickness to either side of the conductor winding.
17. The gas turbine engine according to claim 12 , wherein, to produce the substantially invariant reluctance of the rotor-to-compensator magnetic flux path, the core structure of each of the one or more balancing segments extends by different distances to either side of the conductor winding.
18. The gas turbine engine according to claim 12 , wherein the core structure of each of the one or more balancing segments is an E-core structure.
19. The gas turbine engine according to claim 12 , wherein the core structure of each of the one or more balancing segments is a U-core structure.
20. The gas turbine engine according to claim 19 , wherein the conductor winding has a thinner layer of conductors on a side of the winding distal from the rotor than on a side of the winding proximal the rotor.