发明名称 |
Aircraft electric braking system |
摘要 |
An electrically actuated braking system for an aircraft. The system includes: an electro-mechanical brake actuator (EMAbrake) proximate a wheel of the aircraft, the EMAbrake including a motor; an electro-mechanical actuator controller (EMAC) including a motor controller for generating a drive signal for the EMAbrake; a braking control unit (BCU) for generating a braking force command signal for the EMAC during a normal mode of operation; and an emergency braking control unit (eBCU) for generating a braking force command signal for the EMAC during an emergency operating mode. The eBCU is disposed together with the EMAC in a common line replaceable unit (LRU). |
申请公布号 |
EP2878502(A1) |
申请公布日期 |
2015.06.03 |
申请号 |
EP20140195202 |
申请日期 |
2014.11.27 |
申请人 |
AIRBUS OPERATIONS LIMITED |
发明人 |
IORDANIDIS, GEORGE;REES, JOHN |
分类号 |
B60T8/17;B64C25/46 |
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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