Closed circuit steam cooled turbine shroud and method for steam cooling turbine shroud
Patent
·
OSTI ID:874445
- Schenectady, NY
- Simpsonville, SC
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
Similar Records
Exit chimney joint and method of forming the joint for closed circuit steam cooled gas turbine nozzles
Cooling circuit for steam and air-cooled turbine nozzle stage
Gas turbine row {number{underscore}sign}1 steam cooled vane
Patent
·
Tue Jan 01 00:00:00 EST 2002
·
OSTI ID:874445
Cooling circuit for steam and air-cooled turbine nozzle stage
Patent
·
Tue Jan 01 00:00:00 EST 2002
·
OSTI ID:874445
Gas turbine row {number{underscore}sign}1 steam cooled vane
Patent
·
Tue Feb 01 00:00:00 EST 2000
·
OSTI ID:874445