Method and system for controlling and recovering short duration bridge power to maximize backup power
    1.
    发明授权
    Method and system for controlling and recovering short duration bridge power to maximize backup power 失效
    控制和恢复短时间桥梁功率以最大化备用电源的方法和系统

    公开(公告)号:US07060379B2

    公开(公告)日:2006-06-13

    申请号:US10065387

    申请日:2002-10-11

    Abstract: A power system, comprising: a primary power source in electrical communication with a bus and a bridging power source, wherein the bridging power source comprises at least one of a capacitor, a battery, and an electrolysis cell, and the bridging power source is in electrical communication with the bus; and a secondary power source in electrical communication with the bus. A method for operating a power system, comprising: monitoring a primary power source; if the primary power source exhibits selected characteristics, directing power from a bridging power source to a bus and initiating a secondary power source, and the bridging power source comprises at least one of a capacitor, a battery, and an electrolysis cell; and unless the secondary power source exhibits the selected characteristics, powering the bus with the secondary power source and ceasing the directing power from the bridging power source.

    Abstract translation: 一种电力系统,包括:与总线和桥接电源电通信的主电源,其中所述桥接电源包括电容器,电池和电解池中的至少一个,并且所述桥接电源处于 与公交车通电; 以及与总线电通信的次级电源。 一种用于操作电力系统的方法,包括:监测主电源; 如果主电源具有选定的特性,将功率从桥接电源引导到总线并启动次级电源,并且桥接电源包括电容器,电池和电解池中的至少一个; 并且除非次级电源具有所选择的特性,用二次电源为总线供电并停止来自桥接电源的引导电力。

    Aircraft Ground Run-Up Protection Barrier For Propeller Equipped Planes
    4.
    发明申请
    Aircraft Ground Run-Up Protection Barrier For Propeller Equipped Planes 审中-公开
    螺旋桨配备飞机的飞机地面润滑保护屏障

    公开(公告)号:US20130313362A1

    公开(公告)日:2013-11-28

    申请号:US13899506

    申请日:2013-05-21

    Applicant: Michael Cardin

    Inventor: Michael Cardin

    CPC classification number: B64F1/36 B64F5/60

    Abstract: A Protection Barrier adapted to provide a barrier between an aircraft propeller on one side, and an engine on the opposite side is disclosed. The protection barrier isolates a technician from a rotating propeller while performing engine maintenance, such as adjustments during an aircraft run-up procedure. The Protection Barrier includes a frame assembly supporting dual panels in an elevated position independently adjustable vertically, laterally, and for inclination.

    Abstract translation: 公开了一种适于在一侧的飞机螺旋桨和相对侧的发动机之间提供障碍物的保护屏障。 保护屏障在执行发动机维护时,例如在飞机启动程序期间的调整,将技术人员与旋转螺旋桨隔离。 保护屏障包括框架组件,该框架组件在竖立,横向和倾斜地独立地可升高的位置支撑双面板。

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