Abstract A reverse flow cooled dynamoelectric machine if provided with cooling gas passages extending through a fan ring and a portion of the rotor spindle to the end turns of the rotor winding in a direction substantially corresponding to the direction of flow of the cooling gas as modified by a tangential component imparted to the gas by the rotation of the fan ring. This direction is the vector sum of the longitudinal component of the velocity of the gas as it approaches the passages and the tangential component imparted by the rotation of the fan ring. The exit end of each passage is circumferentially displaced from the inlet end opposite to the direction of rotation. The centerlines of the gas passages lie in planes spaced around the axis of rotation of the rotor and parallel to this axis.
In a dynamoelectric machine including a rotor having a reduced diameter spindle, a fan ring formed integrally with the rotor and a turbine coupling fixed to said rotor and spaced axially from said fan ring, the method of forming passages for flow of cooling gas in said fan ring and a portion of said spindle comprising: (a) locating the positions of inlets for said cooling passages on said fan ring; (b) positioning a boring tool in engagement with one of said inlet positions with said boring tool disposed in a plane parallel to the axis of the rotor and on a line extending radially outwardly of said turbine coupling; (c) boring a passage through said fan ring and a portion of said spindle, the alignment of said boring tool obviating any interference with said boring tool by said turbine coupling during such boring operation; and (d) positioning said boring tool successively in engagement with the remaining inlet portions in similar alignment and repeating the boring operation.
Claim 2
Dependent Claim
166 words
In a dynamoelectric machine including a rotor having a reduced diameter spindle, a fan ring formed integrally with the rotor and a turbine coupling fixed to said rotor and spaced axially from said fan ring, the method of forming passages for flow of cooling gas in said fan ring and a portion of said spindle comprising: (a) locating the positions of inlets for said cooling passages on said fan ring; (b) positioning a boring tool in engagement with one of said inlet positions with said boring tool disposed in a plane parallel to the axis of the rotor and on a line extending radially outwardly of said turbine coupling; (c) boring a passage through said fan ring and a portion of said spindle, the alignment of said boring tool obviating any interference with said boring tool by said turbine coupling during such boring operation; and (d) positioning said boring tool successively in engagement with the remaining inlet portions in similar alignment and repeating the boring operation.
Claim 3
Dependent Claim
50 words
The method of claim 1, wherein said boring tool is positioned at an acute angle to said axis such that the exit end of the passage formed by the boring tool is circumferentially displaced from the inlet position of that passage opposite to the direction of rotation of said rotor.