System for tuning a combustor of a gas turbine
Abstract
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.
- Inventors:
- Publication Date:
- Research Org.:
- General Electric Co., Schenectady, NY (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1337666
- Patent Number(s):
- 9,528,701
- Application Number:
- 13/833,878
- Assignee:
- GENERAL ELECTRIC COMPANY (Schenectady, NY
- DOE Contract Number:
- FC26-05NT42643
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 2013 Mar 15
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 33 ADVANCED PROPULSION SYSTEMS; 42 ENGINEERING
Citation Formats
Hughes, Michael John. System for tuning a combustor of a gas turbine. United States: N. p., 2016.
Web.
Hughes, Michael John. System for tuning a combustor of a gas turbine. United States.
Hughes, Michael John. 2016.
"System for tuning a combustor of a gas turbine". United States. https://www.osti.gov/servlets/purl/1337666.
@article{osti_1337666,
title = {System for tuning a combustor of a gas turbine},
author = {Hughes, Michael John},
abstractNote = {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.},
doi = {},
url = {https://www.osti.gov/biblio/1337666},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Dec 27 00:00:00 EST 2016},
month = {Tue Dec 27 00:00:00 EST 2016}
}
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