Rotor assembly for dynamo electric machines

• US 20040263019A1
• Filed: 06/24/2004
• Published: 12/30/2004
• Est. Priority Date: 06/24/2003
• Status: Active Grant

• Current Assignee: Safran Power UK Ltd.
• Original Assignee: Goodrich Control Systems (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Fakult, Joseph Paul, Buchan, Neil Fergus
• Granted Patent: US 6,933,648 B2
• Time in Patent Office: Days
• US Class Current: 310/214
• CPC Class Codes: H02K 3/527 applicable to rotors only

Abstract

A rotor assembly for a dynamo electric machine, the rotor assembly comprising a rotor core incorporating radially extending rotor poles, rotor windings encircling respective rotor poles, circumferentially extending pole tips at the outer end of each pole respectively, said tips overlying the rotor winding encircling the respective pole, a plurality of rotor slot closure members, each closure member spanning the gap between a pair of adjacent poles, and including lateral flanges interposed between the respective rotor windings and the associated pole tips, a spacer member positioned beneath each closure member and engaging the radially extending faces of the adjacent windings, and, a locking wedge assembly comprising a pair of locking wedges extending axially of the rotor assembly between each closure member and the associated spacer, the locking wedges extending with their tapers in opposite directions so that moving the wedges longitudinally towards one another increases the radial dimension of the combination of the locking wedges driving the associated spacer and closure apart in a radial direction. Also disclosed is a method of manufacturing a rotor assembly.

Claims

1. A rotor assembly for a dynamo electric machine, the rotor assembly comprising a rotor core incorporating radially extending rotor poles, rotor windings encircling respective rotor poles, circumferentially extending pole tips at the outer end of each pole respectively, said tips overlying the rotor winding encircling the respective pole, a plurality of rotor slot closure members, each closure member spanning the gap between a pair of adjacent poles, and including lateral flanges interposed between the respective rotor windings and the associated pole tips, a spacer member positioned beneath each closure member and engaging the radially extending faces of the adjacent windings, and, a locking wedge assembly comprising a pair of tapering locking wedges extending axially of the rotor assembly between each closure member and the associated spacer, the locking wedges extending with their tapers in opposite directions so that moving the wedges longitudinally towards one another increases the radial dimension of the combination of the locking wedges driving the associated spacer and closure apart in a radial direction.

2. A rotor assembly as claimed in claim 1 wherein the locking wedges are each received in an elongate channel formed in the respective closure member and spacer.

3. A rotor assembly as claimed in claim 1 wherein the locking wedges are each received in respective elongate oppositely facing channels formed in a respective elongate alignment member interposed between the respective closure member and spacer, the wedges being in sliding contact with each other through the intermediary of a dividing wall of the alignment member.

4. A rotor assembly as claimed in claim 1 wherein said closure members and said spacers are equal in length to the axial length of the poles of the rotor core, and said first and second locking wedges are initially of a length exceeding the axial length of the poles.

5. A rotor assembly as claimed in claim 1 wherein the first and second wedges are formed from a carbon fibre composite material.

6. A rotor assembly as claimed in claim 1 wherein the first and second wedges each have a 2°

taper over their whole length.

7. A rotor assembly as claimed in claim 1 wherein a single wedge shaped blank is cut to produce substantially identical first and second wedges.

8. A method of manufacturing a rotor assembly for a dynamo electric machine comprising, starting with a rotor core including a plurality of circumferentially spaced radially extending poles encircled by respective rotor windings, a respective spacer received in the gap between the windings of each circumferentially adjacent pair of windings, a respective closure member circumferentially spanning the gap between the poles of each adjacent pair of poles, each closure member including lateral flanges received between a respective winding and the underside of a respective circumferentially extending pole tip, and the method including introducing a respective locking wedge assembly between each spacer and its associated closure, each locking wedge assembly comprising first and second elongate tapering wedges with their tapers extending in opposite directions axially of the rotor assembly, said first and second wedges having their taper arranged radially of the rotor assembly, the first wedge having a face in contact with the respective closure member, the second wedge having a face in contact with the respective spacer, and the two wedges having their opposite face in sliding contact, and, driving the wedges axially of the rotor assembly to move their wider ends towards the transverse median plane of the rotor assembly so as to urge the respective closure member and the respective spacer radially apart.

9. A method as claimed in claim 8 wherein the locking wedges are each received in respective elongate oppositely facing channels formed in a respective elongate alignment member interposed between the respective closure member and spacer, and are in sliding contact with one another through the intermediary of a dividing wall of the alignment member.

10. A method as claimed in claim 8 wherein said closure members and said spacers are equal in length to the axial length of the poles of the rotor core, and said first and second locking wedges are initially of a length exceeding the axial length of the poles, the dimensions of the wedges, the closure members and the spacers being such that the first and second wedges are inserted substantially completely through the axial length of the rotor before significant radial force is applied to the respective spacer and closure member, the wedges then being pressed further to load the respective spacer and the respective closure member radially apart and subsequently trimming the protruding regions of the first and second wedges, at both axial ends of the rotor assembly, to be substantially flush with the axial ends of the spacers and closure members.

11. A method as claimed in claim 8 wherein a wedge insertion apparatus applies a predetermined force simultaneously to the wider ends of the first and second wedges of each wedge assembly to drive the wider ends of the first and second wedges towards one another, the predetermined force applied simultaneously to both wedges being calculated to move the wedges to a position in which a predetermined desired radial loading is applied to the respective spacer and closure member.

12. A method as claimed in claim 8 wherein a single wedge shaped blank is cut to produce substantially identical first and second wedges.