发明授权
- 专利标题: Actively cooled gas turbine sensor probe housing
- 专利标题(中): 主动冷却燃气轮机传感器探头外壳
-
申请号: US14134603申请日: 2013-12-19
-
公开(公告)号: US09116051B2公开(公告)日: 2015-08-25
- 发明人: Thomas N. Slavens , Charles W. Haldeman
- 申请人: United Technologies Corporation
- 申请人地址: US CT Hartford
- 专利权人: United Technologies Corporation
- 当前专利权人: United Technologies Corporation
- 当前专利权人地址: US CT Hartford
- 代理机构: Miller Matthias & Hull LLP
- 主分类号: G01K1/12
- IPC分类号: G01K1/12 ; G01D11/24 ; G01K13/02
摘要:
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.
公开/授权文献
- US20140254631A1 Actively Cooled Gas Turbine Sensor Probe Housing 公开/授权日:2014-09-11
信息查询