
Hi every body... I seek your assistance in analytically analysing one problem we are facing in the stacking of armature lamination on shaft. Both the lamination and the shaft is without key way; and the laminations are stacked on to the shaft; by following process.. 1. Shaft is thermally cooled by immersing in the liquid nitrogen; which brings down the shaft diameter below the diameter of bore in lamination 2. Laminations are stacked to the required corelength in a mandrel; and stacking is inserted onto the shaft. However; in some of the stacked aramtures; the stacked corelength are seen to develop gaps; along the periphery of the rotor; after the shaft comes back to ambient temperature. But this phenomenon is not noticed in all stacked armatures. Tolerances presently are as below: 1. Lamination : 78 +0.03 h7, 2. Shaft : 78 +0.048 to 0.062 (Shrinked by Nitrogen cooling, prior to shaft pressing) Shaft Material : EN8 Lamination Grade : M45/ M43. Is it possible to correlelate the effects of the variation in bore dimensions of shaft and stacked laminations; to the observed gaps in the stacking; by analysis. And find out the best possible tolerance for the shaft, from this analysis. Any link to relevant literatures.
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