Rotor Assembly

• US 20110215669A1
• Filed: 09/09/2010
• Published: 09/08/2011
• Est. Priority Date: 09/10/2009
• Status: Abandoned Application

• Current Assignee: Goodrich Control Systems (Rtx Corporation)
• Original Assignee: Goodrich Control Systems (Rtx Corporation)
• Inventors: Spitz, Daniel Jonathan, Hill, Peter Martin
• Application Number:
  US12/878,441
• Publication Number:
  US 20110215669A1
• Time in Patent Office: Days
• US Class Current: 310/214
• CPC Class Codes: H02K 3/527 applicable to rotors only
• CPC Class Codes: Y10T 29/49012 Rotor

Abstract

A rotor assembly comprises a rotor body defining a pole, a winding encircling the pole, a compression member located radially inwards of the winding, and compression means located between the compression member and the rotor body and operable to urge the compression member in an outward direction to apply a compressive load to the winding. A method of assembly of the rotor is also disclosed.

Claims

1. A rotor assembly comprising a rotor body defining a pole, a winding encircling the pole, a compression member located radially inwards of the winding, and compression means located between the compression member and the rotor body and operable to urge the compression member in an outward direction to apply a compressive load to the winding.

2. An assembly according to claim 1, wherein the compressive load applied by the compression member to the winding acts in a direction substantially parallel to a pole face of the pole.

3. An assembly according to claim 1, wherein the compression means comprises a pair of taper wedges, relative movement of which changes the position of the compression member relative to the rotor body.

4. An assembly according to claim 1, further comprising a closure member arranged to close a rotor slot through which the winding extends.

5. An assembly according to claim 4, wherein the closure member is of an aluminium metal matrix material.

6. An assembly according to claim 5, wherein the aluminium metal matrix material comprises an aluminium silicon carbide mix containing up to 40% silicon carbide.

7. An assembly according to claim 4, further comprising a compression wedge located radially inward of the closure member and urged in an inward direction to apply a compressive load to the winding, compressing the winding against the respective pole face.

8. A method of assembly of a rotor, the method comprising steps of:

(a) positioning a compression member adjacent a pole of a rotor body;

(b) encircling at least part of the pole with a winding; and

(c) urging the compression member in an outward direction to apply a compressive load to the winding.

9. A method according to claim 8, wherein the step of urging the compression member is achieved by adjusting the relative positions of a pair of taper wedges.

10. A method according to claim 8, further comprising a step of providing a closure member to close a rotor slot through which the winding extends.

11. A method according to claim 10, wherein the closure member is of extruded form.

12. A method according to claim 11, where the closure member is of aluminium metal matrix material form.