发明名称 INLET DOOR CONTROL FOR STARTUP OF GAS TURBINE ENGINE
摘要 A gas turbine engine inlet door control system includes an actuator, an engine controller and a door controller. The actuator opens and closes an inlet door of a gas turbine engine. The engine controller determines an intermediate door position based upon one or more engine start factors. The door controller operates the actuator to open the inlet door to the intermediate door position based on the one or more engine start factors.
申请公布号 US2016090915(A1) 申请公布日期 2016.03.31
申请号 US201414787068 申请日期 2014.04.30
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Wolff Eric L.;Sherill Brent L.;Ajami Andre M.;Winston Kenneth W.;Pascu Victor;Vessa Phillip;DaCunha Nelson
分类号 F02C7/268;F02C7/04 主分类号 F02C7/268
代理机构 代理人
主权项 1. A gas turbine engine inlet door control system comprising: an actuator for opening and closing an inlet door of a gas turbine engine; an engine controller for determining an intermediate door position based upon one or more engine start factors; and a door controller for operating the actuator to open the inlet door to the intermediate door position based on the one or more engine start factors.
地址 Hartford CT US