发明名称 Aircraft engine starter/generator
摘要 A rotor resistor and switch combination may cause a starter/generator device to function as an asynchronous device when in a start mode. Thus, starting torque may result. A starter/generator device may include an exciter rotor winding, a main rotor winding, and a resistor and switch combination positioned between the exciter rotor winding and the main rotor winding to control a flow of current in the main rotor winding during a start mode of the starter/generator device. A method of optimizing starting torque of a starter/generator device without a start controller unit during a start mode may include providing a main rotor winding of the starter/generator device, and providing a control to control a flow of current in the main rotor winding during the start mode.
申请公布号 US7592786(B2) 申请公布日期 2009.09.22
申请号 US20070837634 申请日期 2007.08.13
申请人 HONEYWELL INTERNATIONAL INC. 发明人 XU MINGZHOU;ANGHEL CRISTIAN E.;PEARSON WAYNE T.
分类号 H02P9/10;F02N11/04;H02K23/52;H02P9/04;H02P9/14 主分类号 H02P9/10
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