发明名称 |
Electro-mechanical sensor power up circuit |
摘要 |
An electrical circuit for allowing electrical power to be applied to the electro-mechanical sensors of an automatic flight control system of an aircraft only when either the Engine Start switch or AFCS Engage switch is closed separately or simultaneously. Upon the closing of either one or both of the switches, a pair of latching relays are energized which in turn provide electric power to the electro-mechanical sensors.
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申请公布号 |
US4314307(A) |
申请公布日期 |
1982.02.02 |
申请号 |
US19800146821 |
申请日期 |
1980.05.05 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY |
发明人 |
SIVAHOP, ALBERT;ADAMS, SR., DON L.;FISCHER, WILLIAM C. |
分类号 |
H01H47/00;H02H11/00;(IPC1-7):H01H63/36 |
主分类号 |
H01H47/00 |
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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