ASME 1969 Gas Turbine Conference and Products Show 1969
DOI: 10.1115/69-gt-30
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High Temperature Sensors for Gas Turbines

Abstract: Gas turbines with turbine inlet temperatures of 2500 to 3000 F are planned for the future. A critical element of the advanced controls needed for a turbine of this type is the turbine inlet temperature sensor to protect vital engine hardware and the registration of gas temperature for power controls. The paper discusses the requirements for high temperature sensor advancements, since currently developed sensors have short life, slow response, and are not sufficiently accurate. Considerable discussion is devote… Show more

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“…The measured values under dynamic operating conditions differ from actual uid properties due to the response time of sensors, unlike the measurement under steady-state conditions [30,31]. Speci cally in the case of temperature sensors located in the turbine exhaust, additional structures were employed to prevent direct contact of hot combustion gases so as to increase sensor life [32]. A time delay in the measured temperature occurs because of heat conduction in the structures.…”
Section: Introductionmentioning
confidence: 99%
“…The measured values under dynamic operating conditions differ from actual uid properties due to the response time of sensors, unlike the measurement under steady-state conditions [30,31]. Speci cally in the case of temperature sensors located in the turbine exhaust, additional structures were employed to prevent direct contact of hot combustion gases so as to increase sensor life [32]. A time delay in the measured temperature occurs because of heat conduction in the structures.…”
Section: Introductionmentioning
confidence: 99%