发明名称 Gas Turbine Air Mass Flow Measuring System and Methods for Measuring Air Mass Flow in a Gas Turbine Inlet Duct
摘要 A method and system for measuring a mass flow rate in a portion of a flow path in an inlet duct of a gas turbine engine is provided. The system includes a sensor assembly attached to the inlet duct. The sensor assembly includes a tube with a longitudinal axis disposed in a substantially laminar flow region of the inlet duct, and a flow conditioner disposed in the tube. A hot wire sensor disposed in the tube is also provided.
申请公布号 US2014208755(A1) 申请公布日期 2014.07.31
申请号 US201314060839 申请日期 2013.10.23
申请人 General Electric Company 发明人 Ekanayake Sanji;Scipio Alston Ilford;Morgan Rex Allen;Schieke Sascha;Billheimer Thomas C.
分类号 G01M15/14;F02C7/00 主分类号 G01M15/14
代理机构 代理人
主权项 1. A system for measuring a mass flow in an inlet duct of a turbine engine, comprising: a sensor assembly attached to the inlet duct, the sensor assembly comprising: a tube with a longitudinal axis disposed in a substantially laminar flow region of the inlet duct;a flow conditioner disposed in the tube; anda hot wire sensor disposed in the tube.
地址 Schenectady NY US