发明名称 AIRCRAFT BRAKE CONTROL ARCHITECTURE HAVING IMPROVED ANTISKID REDUNDANCY
摘要 <p>An electromechanical braking system includes first and second electromechanical actuator controllers (EMACs) that each independently generate a complete set of drive control signals for an associated set of electromechanical actuators (EMAs). The drive control signals are generated in accordance with an antiskid algorithm to impart antiskid control to the braking of wheels associated with the EMAs. Drive signals for some of the EMAs from the set of EMAs are output by drivers of the first EMAC and drive signals for the other EMAs from the set of EMAs are output by drivers of the second EMAC. Drive control signals from one of the EMACs are used to control output the drive signals for all the EMAs from the set of EMAs, regardless of the EMAC in which the associated drivers are present. The drive control signals from the other of the EMACs are used as a backup set of drive control signals.</p>
申请公布号 EP2162325(B1) 申请公布日期 2010.10.27
申请号 EP20080755520 申请日期 2008.05.15
申请人 GOODRICH CORPORATION 发明人 MAY, BILL
分类号 B60T8/17;B60T8/88 主分类号 B60T8/17
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