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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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