发明名称 |
Auxiliary ignition system and method for aircraft engines |
摘要 |
An auxiliary ignition system comprising a first magneto having a normal operating mode and a start-up mode, and a second magneto having a normal operating mode and a start-up mode. A primary starter switch is operably wired to the first and second magnetos. Engagement of the primary starter switch activates the second magneto start-up mode and the first magneto start-up mode. Auxiliary ignition switches are operably connected to the primary starter switch wiring such that engagement of the auxiliary ignition switches after engagement of the starter switch causes the first and second magnetos to initiate engine ignition in their respective normal operating mode.
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申请公布号 |
US5331935(A) |
申请公布日期 |
1994.07.26 |
申请号 |
US19930040900 |
申请日期 |
1993.03.31 |
申请人 |
ASAP - AIRCRAFT SERVICE AND PARTS, INC. |
发明人 |
DAINO, JOHN |
分类号 |
F02N11/08;F02P15/00;F02P15/12;(IPC1-7):F02P1/08 |
主分类号 |
F02N11/08 |
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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