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Title: Gas turbine bucket with impingement cooled platform

Patent ·
OSTI ID:874645

In a turbine bucket having an airfoil portion and a root portion, with a substantially planar platform at an interface between the airfoil portion and root portion, a platform cooling arrangement including at least one bore in the root portion and at least one impingement cooling tube seated in the bore, the tube extending beyond the bore with an outlet in close proximity to a targeted area on an underside of the platform.

Research Organization:
General Electric Co., Schenectady, NY (United States)
DOE Contract Number:
FC21-95MC31176
Assignee:
General Electric Company (Schenectady, NY)
Patent Number(s):
US 6431833
OSTI ID:
874645
Country of Publication:
United States
Language:
English

References (2)

Development Requirements for an Advanced Gas Turbine System journal October 1995
Advances in Steam Path Technology journal April 1996