An aircraft brake temperature control system (BTCS) for controlling the temperature of a brake of a landing gear of an aircraft is disclosed. An aircraft brake temperature control system includes a controller configured to cause a thermal management system to adjust a temperature of a brake based on a selection of a certain object of a plurality of objects for adjusting the brake temperature. An aircraft including the aircraft brake temperature control system, a method of controlling the temperature of a brake of a landing gear of an aircraft are also disclosed. Further disclosed is a non-transitory computer-readable storage medium comprising a set of computer-readable instructions stored thereon that, when executed by a controller of an aircraft brake temperature control system, cause the controller to operate the above method of controlling the temperature of the brake of the landing gear of an aircraft. A temperature control system for controlling the temperature 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)。飞行器制动器温度控制系统包括控制器,该控制器配置成基于对用于调节制动器温度的多个对象中的用于调节制动器温度的某一对象的选定,使热管理系统对制动器的温度进行调节。还公开了:包括飞行器制动器温度控制系统的飞行器、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,该指令在由飞行器制动器温度控制系统的控制器执行时使控制器运行上述对飞行器的起落架的制动器的温度进行控制的方法。也公开了一种用于对飞行器机轮的制动器的温度进行控制的温度控制系统。
Aircraft brake temperature control system
飞行器制动器温度控制系统
2022-06-14
Patent
Elektronische Ressource
Chinesisch