Invention Grant
- Patent Title: Actively cooled gas turbine sensor probe housing
- Patent Title (中): 主动冷却燃气轮机传感器探头外壳
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Application No.: US14134603Application Date: 2013-12-19
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Publication No.: US09116051B2Publication Date: 2015-08-25
- Inventor: Thomas N. Slavens , Charles W. Haldeman
- Applicant: United Technologies Corporation
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Miller Matthias & Hull LLP
- Main IPC: G01K1/12
- IPC: G01K1/12 ; G01D11/24 ; G01K13/02

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.
Public/Granted literature
- US20140254631A1 Actively Cooled Gas Turbine Sensor Probe Housing Public/Granted day:2014-09-11
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