发明名称 ELECTRICAL AUGMENTATION OF A GAS TURBINE ENGINE
摘要 One aspect is an electrical augmentation system for a gas turbine engine. The electrical augmentation system includes an electric motor operably coupled to a shaft of the gas turbine engine, and an energy storage device operable to provide a temporary increased current source to the electric motor. The electrical augmentation system includes a control system having a torque demand anticipation circuit operable to determine an anticipated torque increase condition for the gas turbine engine. Based on the anticipated torque increase condition, the torque demand anticipation circuit commands a temporary torque increase by the electric motor using the energy storage device.
申请公布号 WO2015133994(A1) 申请公布日期 2015.09.11
申请号 WO2014US20084 申请日期 2014.03.04
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 BOURNE, FREDERICK L.;BYSTRY, MARK DENTON, JR.;SIMONETTI, JOSEPH LAWRENCE
分类号 F01D15/10;F02C6/14;H02P9/00 主分类号 F01D15/10
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