Method for making gas turbine engine blade attachment slots

Metal working – Method of mechanical manufacture – Impeller making

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29558, 409244, 451 54, 451 55, 451 57, B23P 1500

Patent

active

054309360

ABSTRACT:
Blade attachment slots for gas turbine engines are prepared by grinding to a stepped, generally straight sided configuration, semi-finish grinding to an envelope about 0.005 inches to 0.010 inches above the blueprint configuration, and finishing by broaching. This reduces the overall cost of the manufacturing process, permits a more economical use of existing broach machines, and allows greater versatility for short model runs and "just-in-time" production.

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Antwerp, Catherine Van, CNC Grinding of Flat Broaches, Technical Paper, Society of Manufacturing Engineers 1990, 10 pgs.
Letter to Pratt & Whitney dated Oct. 3, 1991 from Baltz Kloeti of Maegerle, Inc., re: Rough grinding of slots in turbine discs, 10 pgs.

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