发明名称 |
Electric command spoiler system. |
摘要 |
<p>An aircraft spoiler control system wherein each of a plurality of spoilers is driven by an electrically responsive actuator. Sense signals representative of the aircraft's control wheel rotation, speedbrake lever deflection, flap position and air/ground status are processed by logic which produces a corresponding control signal for each actuator. Fault detection circuitry switches in a back-up actuator control signal if a fault occurs in the active control circuit.</p> |
申请公布号 |
EP0042653(A1) |
申请公布日期 |
1981.12.30 |
申请号 |
EP19810200708 |
申请日期 |
1981.06.22 |
申请人 |
THE BOEING COMPANY |
发明人 |
BUUS, HENNING;MACFIE, THOMAS DAVID;JUSTAD, ODD |
分类号 |
B64C13/50;B64C9/02;B64C3/58;B64C13/00;B64C13/16;G05D1/08;(IPC1-7):64C13/50;05D1/08 |
主分类号 |
B64C13/50 |
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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