US Patent 6983603 Detection of gas turbine engine hot section condition
Patent 6983603 was granted and assigned to Pratt & Whitney Canada on January, 2006 by the United States Patent and Trademark Office.
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Patent abstract
A system and a method for detecting gas turbine engine hot section condition using temperature measurements during engine operation. The system comprises a sensing unit for sensing a temperature distribution across a hot combustion gas stream generated by a gas turbine engine combustor. A signal processor receives temperature signals from the sensing unit and generates a combustor malfunction signal when the difference between a maximal temperature and a minimal temperature of the sensed temperature distribution is greater than a predetermined acceptable delta value.
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Patent Inventor Names
Enzo Macchia0
Date of Patent
January 10, 2006
0Patent Application Number
102788970
Date Filed
October 24, 2002
0Patent Primary Examiner
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US Patent 6983603 Detection of gas turbine engine hot section condition
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