| 发明名称 | Aircraft electric braking system | ||
| 摘要 | An electrically actuated braking system for an aircraft, including: 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 first motor controller for generating a first drive signal for the EMAbrake, and a second motor controller for generating a second drive signal for the EMAbrake, wherein the first motor controller and the second motor controller are dissimilar so as to provide protection against common mode failure of the first and second motor controllers. | ||
| 申请公布号 | US9611035(B2) | 申请公布日期 | 2017.04.04 |
| 申请号 | US201414554572 | 申请日期 | 2014.11.26 |
| 申请人 | Airbus Operations Limited | 发明人 | Iordanidis George;Rees John |
| 分类号 | B60T8/86;B64C25/44;B60T8/17;B60T8/88;B64C25/46;F16D65/14;B60T13/74;F16D121/24 | 主分类号 | B60T8/86 |
| 代理机构 | Nixon & Vanderhye P.C. | 代理人 | Nixon & Vanderhye P.C. |
| 主权项 | 1. An electrically actuated braking system for an aircraft, comprising: an electro-mechanical brake actuator proximate a wheel of the aircraft, the electro-mechanical brake actuator including a motor; an electro-mechanical actuator controller (EMAC) including a first motor controller for generating a first drive signal for the electro-mechanical brake actuator, and a second motor controller for generating a second drive signal for the electro-mechanical brake actuator, wherein the first motor controller and the second motor controller are dissimilar so as to provide protection against common mode failure of the first and second motor controllers. | ||
| 地址 | Bristol GB | ||