US Patent 9121309 Gas turbine and method of operating a gas turbine
Patent 9121309 was granted and assigned to MTU Aero Engines on September, 2015 by the United States Patent and Trademark Office.
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Patent abstract
A gas turbine including at least one compressor, one combustion chamber, and at least one turbine including at least one rotor and at least one generator coupled to the at least one rotor is provided. The at least one turbine is coupled to the at least one compressor. Once the gas turbine is shut down, the at least one generator can be used as a motor in order to drive the at least one rotor for a predetermined time period following shutdown of the gas turbine and thereby effect a uniform cooling of the rotor. A method of operating a gas turbine is also provided.
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US Patent 09121309 Gas turbine and method of operating a gas turbine US Patent 9121309 Gas turbine and method of operating a gas turbine
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Patent Number
0912130900
Patent Number
912130900
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Current Assignee
Patent Jurisdiction
Patent Number
091213090
Date of Patent
September 1, 2015
0Patent Application Number
123082110
Date Filed
June 10, 2006
0Official Website
Patent Primary Examiner
Edits on 27 Sep, 2022
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Is a
Current Assignee
Patent Jurisdiction
Patent Number
091213090
Date of Patent
September 1, 2015
0Patent Application Number
123082110
Date Filed
June 10, 2006
0Official Website
Patent Primary Examiner
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US Patent 09121309 Gas turbine and method of operating a gas turbine
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
09121309
Date of patent
September 1, 2015
Patent application number
12308211
Date Filed
June 10, 2006
Patent primary examiner
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