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    • 51. 发明申请
    • METHOD FOR REDUCING REQUIREMENTS FOR AIRCRAFT BRAKE SIZE, COMPLEXITY, AND HEAT DISSIPATION
    • 用于减少飞机制动尺寸,复杂性和散热要求的方法
    • US20130112805A1
    • 2013-05-09
    • US13543768
    • 2012-07-06
    • Isaiah W. Cox
    • Isaiah W. Cox
    • B64C25/36B64C25/42
    • B64C25/36B64C25/405B64C25/42Y02T50/823
    • A method is provided for optimizing requirements for brake size, complexity, and heat dissipation capability in an aircraft, wherein the aircraft is powered during ground travel by an onboard wheel drive assembly, including controllable drive means, mounted on at least one aircraft wheel, and ground travel is controlled by the pilot to move the aircraft on the ground without relying on the operation of the aircraft engines, while substantially minimizing brake use between landing and takeoff. Brakes can be optimally sized and configured to meet landing and taxi requirements, resulting in reduced brake size and complexity and increased effective heat dissipation. Substantially minimizing brake use during taxi produces improved brake cooling, substantially eliminating delays caused by slow brake heat shedding and enables rapid aircraft turnaround between landing and takeoff.
    • 提供了一种用于优化飞行器中制动器尺寸,复杂性和散热能力的要求的方法,其中飞行器在地面行驶期间由安装在至少一个飞行器轮上的车载轮驱动组件(包括可控驱动装置)供电,以及 地面行驶由飞行员控制,以使飞机在地面上移动,而不依赖飞机发动机的操作,同时大幅度地最大限度地降低着陆和起飞之间的刹车使用。 制动器的最大尺寸和配置可以满足着陆和出租车的要求,从而减少制动器尺寸和复杂性,增加有效散热。 实际上最小化滑行器制动器使用时,产生改进的制动器冷却,从而大大消除了制动器散热缓慢所引起的延迟,并使得降落和起飞之间的飞机能够快速转向。