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Title: Closed circuit steam cooled turbine shroud and method for steam cooling turbine shroud

Patent ·
OSTI ID:874445

A turbine shroud cooling cavity is partitioned to define a plurality of cooling chambers for sequentially receiving cooling steam and impingement cooling of the radially inner wall of the shoud. An impingement baffle is provided in each cooling chamber for receiving the cooling media from a cooling media inlet in the case of the first chamber or from the immediately upstream chamber in the case of the second through fourth chambers and includes a plurality of impingement holes for effecting the impingement cooling of the shroud inner wall.

Research Organization:
General Electric Co., Schenectady, NY (United States)
DOE Contract Number:
FC21-95MC31176
Assignee:
General Electric Company (Schenectady, NY)
Patent Number(s):
US 6390769
OSTI ID:
874445
Country of Publication:
United States
Language:
English