| 发明名称 |
AIRCRAFT ELECTRIC BRAKING SYSTEM |
| 摘要 |
An electrically actuated braking system for an aircraft, comprising: 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; and a braking control unit for generating a braking force command signal for the EMAC; wherein the braking control unit and the EMAC are disposed together with the EMAbrake in a common line replaceable unit (LRU). |
| 申请公布号 |
US2015291280(A1) |
申请公布日期 |
2015.10.15 |
| 申请号 |
US201414554609 |
申请日期 |
2014.11.26 |
| 申请人 |
AIRBUS OPERATIONS LIMITED |
发明人 |
Iordanidis George;Rees John |
| 分类号 |
B64C25/44 |
主分类号 |
B64C25/44 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An electrically actuated braking system for an aircraft, comprising:
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; and a braking control unit for generating a braking force command signal for the EMAC; wherein the braking control unit and the EMAC are disposed together with the EMAbrake in a common line replaceable unit (LRU). |
| 地址 |
Bristol GB |
