发明名称 |
ROTORCRAFT AUTOPILOT CONTROL |
摘要 |
A rotorcraft autopilot system includes a series actuator connecting a cockpit control component to a swashplate of a rotorcraft, the series actuator to modify a control input from the cockpit control component to the swashplate through a downstream control component. The rotorcraft autopilot system also includes a differential friction system connected to the cockpit control component, the differential friction system to control the series actuator to automatically adjust a position of the cockpit control component during rotorcraft flight based, in part, on a flight mode of the rotorcraft. |
申请公布号 |
CA2901482(A1) |
申请公布日期 |
2016.02.21 |
申请号 |
CA20152901482 |
申请日期 |
2015.08.21 |
申请人 |
BELL HELICOPTER TEXTRON INC. |
发明人 |
GRIFFITH, CARL D.;ATKINS, BRADY G.;RAZA, AWAIS;WILSON, PAUL M. |
分类号 |
B64C27/57;B64C13/18;B64C27/04;G05D1/10 |
主分类号 |
B64C27/57 |
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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