| 摘要 |
<p>The method involves installing a bypass (500) on brake systems of an aircraft, where the bypass is associated with insulation valves (400, 501) maintained in a normal mode in an insulation state. Each insulation valve is controllable to be placed in an open state in which power supply ports of fixing cases (106, 206, 306) are supplied by the bypass of the brake system. The insulation valves are directly placed on the bypass. The brake systems are defined by two hydraulic systems (C) of the aircraft. Actuators are supplied by the bypass of the brake system and closed by the insulation valves.</p> |
