AIRCRAFT CONTROL SYSTEM ARCHITECTURE
    21.
    发明申请

    公开(公告)号:US20180105261A1

    公开(公告)日:2018-04-19

    申请号:US15293667

    申请日:2016-10-14

    Abstract: A controller unit for an aircraft control system includes an interface that is electrically connectable to a controller slot of an electronics bay of the aircraft control system, a processor coupled to the interface, and a tangible non-transitory computer-readable medium having instructions stored thereon that, in response to execution by the processor, cause the processor to perform various operations. The various operations include identifying, by the processor, a first aircraft assembly in electrical communication with the controller slot of the electronics bay, identifying, by the processor, a first program code stored on the tangible non-transitory computer-readable medium corresponding to the first aircraft assembly, and selecting, by the processor, the first program code to control the first aircraft assembly.

    Brake control system with disabling features

    公开(公告)号:US10179576B2

    公开(公告)日:2019-01-15

    申请号:US15490605

    申请日:2017-04-18

    Abstract: A brake system may comprise a controller, a vehicle management system (VMS) in communication with the controller, a valve in communication with the controller, and a tangible, non-transitory memory configured to communicate with the controller, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller, cause the controller to perform operations comprising determining, by the controller, that a first enable signal is received by the controller from the VMS, determining, by the controller, that a second enable signal is received by the controller from the VMS, and disabling, by the controller, the controller from control of the valve in response to the first enable signal and the second enable signal.

    Hydraulic park brake system and method

    公开(公告)号:US10093291B2

    公开(公告)日:2018-10-09

    申请号:US15423174

    申请日:2017-02-02

    Abstract: A hydraulic park brake system for an aircraft may include a hydraulic park brake controller having a processor and a tangible, non-transitory memory configured to communicate with the processor. The tangible, non-transitory memory may have instructions stored thereon that, in response to execution by the processor, cause the hydraulic park brake system to perform various operations. Such operations may include receiving, by the processor, a hydraulic park brake condition, comparing, by the processor, the hydraulic park brake condition with a predetermined condition to yield comparison data, and determining, by the processor and based on the comparison data, a hydraulic park brake adjustment status. Such operations may further include generating, by the processor and based on the hydraulic park brake adjustment status, an adjustment command and transmitting, by the processor, the adjustment command to a hydraulic park brake of the aircraft.

    Systems and methods for detection of dragging brake

    公开(公告)号:US10005566B2

    公开(公告)日:2018-06-26

    申请号:US15180663

    申请日:2016-06-13

    Abstract: A landing gear assembly may include a first wheel and a second wheel, a first wheel sensor coupled to the first wheel and a second wheel sensor coupled to the second wheel, and a controller coupled to the first wheel sensor and the second wheel sensor. A tangible, non-transitory memory may have instructions for detecting a dragging brake. The controller may perform operations including receiving data from the first wheel sensor and the second wheel sensor, calculating a wheel speed characteristic for each of the first wheel and the second wheel based on the data, identifying a lowest value for the wheel speed characteristic, determining a moving average for the wheel speed characteristic, comparing the lowest value to the moving average, and whether the lowest value for the wheel speed characteristic indicates a dragging brake.

    Tire inflate/deflate indication method and system
    29.
    发明授权
    Tire inflate/deflate indication method and system 有权
    轮胎充气/放气指示方法和系统

    公开(公告)号:US09193225B2

    公开(公告)日:2015-11-24

    申请号:US14075785

    申请日:2013-11-08

    CPC classification number: B60C23/0476 B60C23/0486 B60C23/20 B60C2200/02

    Abstract: Systems and methods for indicating conditions for the appropriate inflation and/or deflation of tires are disclosed. Some systems and methods include measuring a variable affecting the internal gas temperature of a tire, calculating by the processor an estimated internal gas temperature of a tire, and determining whether a tire is appropriate to inflate and/or deflate.

    Abstract translation: 公开了用于指示轮胎适当的充气和/或放气的条件的系统和方法。 一些系统和方法包括测量影响轮胎内部气体温度的变量,由处理器计算轮胎的估计内部气体温度,以及确定轮胎是否适合于膨胀和/或放气。

    TIRE PRESSURE INDICATOR
    30.
    发明申请
    TIRE PRESSURE INDICATOR 有权
    轮胎压力指示器

    公开(公告)号:US20150231936A1

    公开(公告)日:2015-08-20

    申请号:US14184020

    申请日:2014-02-19

    Abstract: System and methods for indicating a tire pressure condition are disclosed. Some systems and methods include receiving, by a control unit comprising a processor and a tangible, non-transitory memory, a tire pressure data, determining, by the control unit, a relationship of the tire pressure data to a predetermined tire pressure, and causing, by the control unit, an output device to display a value in accordance with the relationship, wherein the output device is externally located on an aircraft.

    Abstract translation: 公开了用于指示轮胎压力条件的系统和方法。 一些系统和方法包括由包括处理器和有形的非暂时性存储器的控制单元接收轮胎压力数据,由控制单元确定轮胎压力数据与预定轮胎压力的关系,并且引起 由所述控制单元输出根据所述关系显示值的输出装置,其中所述输出装置在外部位于飞行器上。

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