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 GB201320939(D0) 申请公布日期 2014.01.08
申请号 GB20130020939 申请日期 2013.11.27
申请人 AIRBUS OPERATIONS LTD 发明人
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