An aircraft brake temperature control system (BTCS) for controlling the temperature of a brake of a landing gear of an aircraft is disclosed. The system includes a controller configured to cause the at least one fluid moving device to selectively drive a flow of fluid onto the brake in one of a plurality of modes to control a temperature of the brake. Also disclosed are: an aircraft system comprising an aircraft brake temperature control system and at least one fluid moving device; an aircraft including an aircraft brake temperature control system or an aircraft system; and a method of controlling the temperature of a brake of a landing gear of an aircraft. Also disclosed is a non-transitory computer-readable storage medium comprising a set of computer-readable instructions stored thereon that, when executed by a controller, cause the controller to execute the above method. A fluid movement system for moving fluid along a surface of a brake of an aircraft wheel is also disclosed.
本发明公开了一种用于对飞行器的起落架的制动器的温度进行控制的飞行器制动器温度控制系统(BTCS)。该系统包括控制器,控制器配置成使至少一个流体移动装置选择性地以多个模式中的一个模式将一定流量的流体驱动到制动器上,以对制动器的温度进行控制。还公开了:包括飞行器制动器温度控制系统和至少一个流体移动装置的飞行器系统;包括飞行器制动器温度控制系统或飞行器系统的飞行器;以及对飞行器的起落架的制动器的温度进行控制的方法。此外公开了包括存储于其上的一组计算机可读指令的一种非暂时性计算机可读存储介质,该指令在由控制器执行时使控制器运行上述方法。也公开了一种用于使流体沿着飞行器机轮的制动器的表面移动的流体移动系统。
Aircraft brake temperature control system
飞行器制动器温度控制系统
14.06.2022
Patent
Elektronische Ressource
Chinesisch