Invention Grant
US09116051B2 Actively cooled gas turbine sensor probe housing 有权
主动冷却燃气轮机传感器探头外壳

Actively cooled gas turbine sensor probe housing
Abstract:
An actively cooled turbine sensor assembly is designed to withstand post-combustion gas-path conditions of gas turbine engines. The housing forms part of a cooling system and includes an elongated tubular structure that may be inserted into the hot flow path. The distal end portion of the sensor assembly is contoured to minimize heat transfer. The housing also includes leading and trailing plenums for flowing cooling air through the housing and out through the distal end portion. Additional side cavities may also be provided for active cooling of the sensor and reducing possible heat conduction paths to the sensor.
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