Method for detecting gas turbine engine flashback
Abstract
A method for monitoring and controlling a gas turbine, comprises predicting frequencies of combustion dynamics in a combustor using operating conditions of a gas turbine, receiving a signal from a sensor that is indicative of combustion dynamics in the combustor, and detecting a flashback if a frequency of the received signal does not correspond to the predicted frequencies.
- Inventors:
- Publication Date:
- Research Org.:
- GE Global Research, Niskayuna, New York (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1078286
- Patent Number(s):
- 8,260,523
- Application Number:
- 12/434,695
- Assignee:
- General Electric Company (Niskayuna, NY)
- DOE Contract Number:
- FC26-05NT42643
- Resource Type:
- Patent
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING
Citation Formats
Singh, Kapil Kumar, Varatharajan, Balachandar, Kraemer, Gilbert Otto, Yilmaz, Ertan, and Lacy, Benjamin Paul. Method for detecting gas turbine engine flashback. United States: N. p., 2012.
Web.
Singh, Kapil Kumar, Varatharajan, Balachandar, Kraemer, Gilbert Otto, Yilmaz, Ertan, & Lacy, Benjamin Paul. Method for detecting gas turbine engine flashback. United States.
Singh, Kapil Kumar, Varatharajan, Balachandar, Kraemer, Gilbert Otto, Yilmaz, Ertan, and Lacy, Benjamin Paul. 2012.
"Method for detecting gas turbine engine flashback". United States. https://www.osti.gov/servlets/purl/1078286.
@article{osti_1078286,
title = {Method for detecting gas turbine engine flashback},
author = {Singh, Kapil Kumar and Varatharajan, Balachandar and Kraemer, Gilbert Otto and Yilmaz, Ertan and Lacy, Benjamin Paul},
abstractNote = {A method for monitoring and controlling a gas turbine, comprises predicting frequencies of combustion dynamics in a combustor using operating conditions of a gas turbine, receiving a signal from a sensor that is indicative of combustion dynamics in the combustor, and detecting a flashback if a frequency of the received signal does not correspond to the predicted frequencies.},
doi = {},
url = {https://www.osti.gov/biblio/1078286},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Sep 04 00:00:00 EDT 2012},
month = {Tue Sep 04 00:00:00 EDT 2012}
}
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Works referenced in this record:
9 ppm NOx / CO Combustion System for “F” Class Industrial Gas Turbines
conference, August 2014
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- ASME Turbo Expo 2000: Power for Land, Sea, and Air, Volume 2: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
Flame Ionization Sensor Integrated Into a Gas Turbine Fuel Nozzle
journal, January 2005
- Benson, Kelly; Thornton, Jimmy D.; Straub, Douglas L.
- Journal of Engineering for Gas Turbines and Power, Vol. 127, Issue 1