发明名称 |
Aircraft electric brake actuation system and method |
摘要 |
Aircraft brakes in an aircraft that includes a brake pedal and an electric brake actuator are controlled by at least determining an aircraft operational state and determining an application force that is supplied to the brake pedal. When the determined aircraft operational state is a ground-idle state and the determined application force is greater than a set force magnitude, an actuator brake is moved to engage the electric brake actuator and the electric brake actuator is de-energized. |
申请公布号 |
EP2353951(B8) |
申请公布日期 |
2016.02.24 |
申请号 |
EP20110150347 |
申请日期 |
2011.01.06 |
申请人 |
HONEYWELL INTERNATIONAL INC. |
发明人 |
HANLON, CASEY;QUITMEYER, JAMES NEIL;BLUNT, ALLAN |
分类号 |
B60T8/17;B60T13/74 |
主分类号 |
B60T8/17 |
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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