System for tuning a combustor of a gas turbine
Patent
·
OSTI ID:1337666
A system for tuning a combustor of a gas turbine includes a flow sleeve having an annular main body. The main body includes an upstream end, a downstream end, an inner surface and an outer surface. A cooling channel extends along the inner surface of the main body. The cooling channel extends at least partially between the downstream end and the upstream end of the main body.
- Research Organization:
- General Electric Co., Schenectady, NY (United States)
- Sponsoring Organization:
- USDOE
- DOE Contract Number:
- FC26-05NT42643
- Assignee:
- GENERAL ELECTRIC COMPANY (Schenectady, NY
- Patent Number(s):
- 9,528,701
- Application Number:
- 13/833,878
- OSTI ID:
- 1337666
- Resource Relation:
- Patent File Date: 2013 Mar 15
- Country of Publication:
- United States
- Language:
- English
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