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
WO2014182519(A2)
申请公布日期
2014.11.13
申请号
WO2014US36087
申请日期
2014.04.30
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
WOLFF, ERIC L.;SHERRILL, BRENT L.;AJAMI, ANDRE M.;WINSTON, KENNETH W.;PASCU, VICTOR;VESSA, PHILLIP;DACUNHA, NELSON