| 发明名称 |
PARKING BRAKE CONTROL SYSTEM FOR AN AIRCRAFT |
| 摘要 |
A system for providing control to a parking brake for an aircraft (10) having a power source includes a panel (28) accessible from an exterior of the aircraft (10) and a parking brake switch (32) disposed on the panel (28) providing control over the engagement and disengagement of the parking brake on the aircraft (10), a method operating such a system for providing control to a parking brake is also disclosed. |
| 申请公布号 |
US2016009384(A1) |
申请公布日期 |
2016.01.14 |
| 申请号 |
US201414770653 |
申请日期 |
2014.02.25 |
| 申请人 |
Bombardier Inc. |
发明人 |
DI ZAZZO Marco;PLANTE Bertrand |
| 分类号 |
B64C25/42;B64D47/02;B60T17/22;B64F1/22 |
主分类号 |
B64C25/42 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system for providing control to a parking brake for an aircraft having a power source during a towing operation of the aircraft, comprising:
a panel of the aircraft accessible from an exterior of the aircraft; a parking brake switch disposed on the panel and configured to provide control over the engagement and disengagement of the parking brake on the aircraft; and a tow status indicator configured to provide an indication to the exterior of the aircraft as to whether or not the aircraft may be towed. |
| 地址 |
Dorval CA |
