Invention Application
US20120044969A1 ENGINE TURBINE TEMPERATURE MEASUREMENT 有权
发动机涡轮温度测量

ENGINE TURBINE TEMPERATURE MEASUREMENT
Abstract:
An assembly for sensing temperature in a gas turbine engine includes a first array of RTDs connected in parallel, a second array of RTDs connected in parallel, and a circuit electrically connected to the first and second arrays. The circuit determines an approximate temperature of a medium as a function of resistance of the first and second arrays.
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