发明名称 |
Control apparatus for a starter/generator system |
摘要 |
A control apparatus (202) for a starter/generator (110) of an aircraft electrical power system is provided. During a start mode of operation, AC power is provided by the control apparatus (202) to an exciter stator (114) of the starter/generator (110) which is combined with controlled AC power supplied by a start converter (106) to a main stator (116) of the starter/generator (110) to rotate and start an aircraft engine. Alternatively, during a generate mode of operation after engine start, the control apparatus (202) provides DC power to the starter/generator (110) to produce a regulated voltage output from the starter/generator (110).
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申请公布号 |
US2005046398(A1) |
申请公布日期 |
2005.03.03 |
申请号 |
US20030649548 |
申请日期 |
2003.08.27 |
申请人 |
ANGHEL CRISTIAN E.;YUE EDWIN |
发明人 |
ANGHEL CRISTIAN E.;YUE EDWIN |
分类号 |
F02C7/268;F02N11/04;H02K19/26;H02P1/52;H02P9/08;H02P9/30;(IPC1-7):H02P9/10;H02P9/14 |
主分类号 |
F02C7/268 |
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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