发明名称 TURBOFAN ENGINE WITH GENERATOR
摘要 A turbofan engine includes a turbine engine having a rotatable fan and a generator. The generator further includes a main machine, an exciter, and a generator control unit for controlling the excitation of the main machine. A rotor assembly is located within one of the blades, and a stator assembly that is along a rotational path of the rotor assembly whereby the operation of the turbine engine rotates the fan, which rotates the rotor assembly along its rotational path past the stator assembly to generate electricity.
申请公布号 EP3004564(A1) 申请公布日期 2016.04.13
申请号 EP20130886178 申请日期 2013.06.07
申请人 GE AVIATION SYSTEMS LLC 发明人 JIA, XIAOCHUAN;ETTRIDGE, DAVID GRAHAM
分类号 F01D15/10;F01D19/00;F02C6/00;F02C7/00 主分类号 F01D15/10
代理机构 代理人
主权项
地址