发明名称 TOTAL AIR TEMPERATURE SENSORS
摘要 A total air temperature sensor includes an airfoil body extending from an airfoil base to an opposed airfoil tip along a longitudinal axis. The airfoil body defines a leading edge and opposed trailing edge. The airfoil body defines an interior flow passage with an inlet for fluid communication of fluid into the interior flow passage and an outlet for exhausting fluid out from the interior flow passage, and wherein the airfoil body defines a bleed passage through the airfoil body between the leading edge and the interior flow passage. A temperature probe is mounted within the interior flow passage for measuring temperature of flow through the interior flow passage to determine total air temperature.
申请公布号 US2015093244(A1) 申请公布日期 2015.04.02
申请号 US201414178351 申请日期 2014.02.12
申请人 ROSEMOUNT AEROSPACE INC. 发明人 Wigen Scott
分类号 F01D25/02;F01D21/00 主分类号 F01D25/02
代理机构 代理人
主权项 1. A total air temperature sensor comprising: an airfoil body extending from an airfoil base to an opposed airfoil tip along a longitudinal axis and defining a leading edge and opposed trailing edge, wherein the airfoil body defines an interior flow passage with an inlet for fluid communication of fluid into the interior flow passage and an outlet for exhausting fluid out from the interior flow passage, and wherein the airfoil body defines a bleed passage through the airfoil body between the leading edge and the interior flow passage; and a temperature probe mounted within the interior flow passage for measuring temperature of flow through the interior flow passage to determine total air temperature.
地址 Burnsville MN US