发明名称 |
Aircraft engine electric start system without a separate exciter field inverter |
摘要 |
An aircraft engine start system eliminates the need of a separate exciter field inverter by rearranging the exciter field windings and by utilizing external AC power. The aircraft engine is started by external AC power and once the engine has started, the engine can supply power back to a variable frequency AC bus as well as back to a constant frequency AC bus through the start/generator converter mode.
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申请公布号 |
US5546742(A) |
申请公布日期 |
1996.08.20 |
申请号 |
US19940282698 |
申请日期 |
1994.07.29 |
申请人 |
ALLIEDSIGNAL INC. |
发明人 |
SHEKHAWAT, SAMPAT;TUMPEY, JOHN J.;WIDDIS, JAMES C. |
分类号 |
F02N11/04;(IPC1-7):F02C7/268 |
主分类号 |
F02N11/04 |
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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