Assembly method for induction rotors
A method of assembling an induction rotor includes inserting a plurality of conductor bars into a stack of disks whereby distal ends of the conductor bars project from respective axial ends of the stack, placing first and second end rings onto the respective axial ends of the stack so that the ends of the conductor bars fit into slots in the respective end rings, and compressing the slots against the conductor bars by impacting at least one of the end rings. The method may include selectively adjusting an amount of end ring material being compressed by varying heights of respective areas of a top surface of the end ring and/or selectively adjusting an amount of end ring material being compressed by varying heights of respective areas of an impacting surface.
1. A method of assembling an induction rotor, comprising:
providing a plurality of conductor bars in a rotor core so that distal ends of the conductor bars project from respective axial ends of the core;
providing first and second end rings each having a plurality of circumferentially-spaced, longitudinal slots;
placing the first and second end rings onto the respective axial ends of the core so that the ends of the conductor bars fit into the slots in the respective end rings; and
impacting at least one of the placed end rings, thereby locking the at least one end ring to the conductor bars.
2. The method of claim 1 , further comprising, prior to the impacting, providing a protruding portion on at least one of the end rings adjacent respective ones of the slots, whereby the impacting compresses the protruding portion so that the respective slot is urged against a corresponding one of the conductor bars.
3. The method of claim 2 , wherein convex portions are provided on both top and bottom surfaces of the end ring.
4. The method of claim 1 , further comprising providing an impact tool having an impact surface substantially parallel to an axially outward-facing surface of the at least one end ring, the impact surface having a plurality of cavities respectively aligned with the slots, wherein the impacting includes striking the end ring with the impact surface without directly impacting the conductor bars.
5. The method of claim 4 , wherein the impact surface has a footprint substantially the same as that of the end ring surface.
6. The method of claim 1 , wherein the impacting includes a series of individual impacts.
7. The method of claim 1 , further comprising providing a plurality of protruding or recessed portions on at least one of the end rings adjacent respective ones of the slots, whereby the impacting compresses the protruding or recessed portions so that material about the slots fills in gaps between the slots and the conductor bars.
8. The method of claim 7 , wherein the one end ring has both protruding and recessed portions.
9. The method of claim 7 , wherein the protruding or recessed portions include alternating concave and convex portions formed about the respective slots.
10. The method of claim 1 , wherein the impacting compresses the slots against the conductor bars.
11. The method of claim 10 , further comprising selectively adjusting an amount of end ring material being compressed by varying heights of respective areas of a top surface of the end ring.
12. The method of claim 10 , wherein the end ring includes a protrusion surrounding a slot, the protrusion having a volume distribution proportional to volume distribution of void space between the slot and a corresponding conductor bar.
13. The method of claim 10 , wherein the compressing includes impacting each end ring outer axial face with a respective impact surface having a shape substantially the same as that of the corresponding axial face.
14. The method of claim 10 , further comprising selectively adjusting an amount of end ring material being compressed by varying heights of respective areas of an impacting surface performing the impacting.
15. The method of claim 1 , wherein the impacting includes striking respective locations about ones of the slots, the striking being at an angle with respect to a longitudinal axis of the induction rotor.
16. The method of claim 1 , wherein impact locations of the impacting are interposed between adjacent ones of the end ring slots.
17. The method of claim 1 , further comprising pressing the end rings toward each other prior to the impacting step, thereby axially biasing the stack against the end rings.
18. The method of claim 1 , further comprising pressing the end rings toward each other prior to the impacting step, thereby axially biasing the rotor core against the end rings.
19. The method of claim 1 , further comprising providing an impacting tool having a plurality of contoured impact surfaces, wherein the impacting includes the impact surfaces striking end ring portions adjacent the respective slots, thereby impressing the respective contours into the corresponding end ring portions.
20. The method of claim 1 , wherein the impacting compresses the end ring and reduces the size of the slots.