Claims
- 1. 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.
- 2. 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.
Parent Case Info
This application is a division of our copending application Ser. No. 691,360, filed June 1, 1976, now U.S. Pat. No. 4,071,790 and assigned to the same assignee.
US Referenced Citations (2)
Number |
Name |
Date |
Kind |
3489040 |
Westhoff |
Jan 1970 |
|
3739208 |
Shartrand |
Jun 1973 |
|
Divisions (1)
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Number |
Date |
Country |
Parent |
691360 |
Jun 1976 |
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