公开(公告)号：US07274974B2

公开(公告)日：2007-09-25

申请号：US11063184

申请日：2005-02-22

申请人： Scott R. Brown ,  Gary M. Kuzkin

发明人： Scott R. Brown ,  Gary M. Kuzkin

IPC分类号： H02J7/00

CPC分类号： H02J3/14 ,  H02J9/06 ,  Y02B70/3225 ,  Y04S20/222 ,  Y10T307/647 ,  Y10T307/68

摘要： An independent automatic shedding system that automatically allows any combination of loads to powered under limited power availability (such as a standby power source) without overloading the generator or rewiring, while contributing to the stability of the power grid. A motorized disconnection actuation mechanism under control of a controller disconnects or recloses the contacts of a branch circuit breaker. A sensor detects the presence or absence of a power source and the type of power source, which is classified according to its type. A power source classification program is executed by the controller that interprets the sensor data and causes disconnection or reclosing of the disconnection actuation mechanism depending on a desired status (ON or OFF) of the branch circuit breaker when standby power is available. Conventional circuit protection is provided an optional advanced circuit protection such as ground or arc fault circuit interruption.

摘要翻译： 一个独立的自动脱落系统，可自动允许任何组合的负载在有限的功率可用性（例如备用电源）下供电，而不会使发电机重新接线或重新布线，同时有助于电网的稳定性。 在控制器下的电动断开致动机构断开或重新连接分支断路器的触点。 传感器检测电源的存在或不存在以及根据其类型分类的电源的类型。 电源分类程序由解释传感器数据的控制器执行，并且当备用电源可用时，根据分支断路器的期望状态（ON或OFF）导致断开致动机构的断开或重新闭合。 传统的电路保护提供了可选的高级电路保护，例如接地或电弧故障电路中断。

公开(公告)号：US5386147A

公开(公告)日：1995-01-31

申请号：US184774

申请日：1994-01-21

申请人： Victor B. Bonneau ,  Gary M. Kuzkin ,  Robert G. Wagoner ,  John A. Overman

发明人： Victor B. Bonneau ,  Gary M. Kuzkin ,  Robert G. Wagoner ,  John A. Overman

IPC分类号： H01H9/54 ,  H01H9/56 ,  H02J3/38 ,  H02J9/06 ,  H02J3/06

CPC分类号： H02J3/38 ,  H02J9/061 ,  H01H9/548 ,  H01H9/563 ,  H02J2009/068 ,  Y10T307/615 ,  Y10T307/735

摘要： An aerospace power control system switches an aerospace load from a faulty ac power bus to a good ac power bus of two or more ac power buses if the currently connected ac power bus is about to fail. The voltage level and frequency of the power provided on the buses are monitored to determine which of the power buses are within required limits to provide power to the aerospace load. If monitoring of the currently connected ac power bus indicates that the bus is not within the required limits and may be shut down in the immediate future, the connection of the aerospace load is switched to another ac power bus which is within the required limits. The current provided to the load is monitored to determine zero-crossing points of the current with the switch from the currently connected faulty bus to a good bus being performed at a zero-crossing point of the load current. The level of the current being provided to the aerospace load is also monitored to detect a faulty load condition. If the load current exceeds defined limits, the load will be disconnected from all ac power buses to shut down the faulty load. The aerospace power control system is generally applicable to single phase and three phase ac power, with switch over at zero-crossing points being performed on a phase-by-phase basis for three phase ac power.

摘要翻译： 如果当前连接的交流电源总线即将发生故障，航空航天电源控制系统将航空负载从故障交流电源总线切换到两个或多个交流电源总线的良好交流电源总线。 对总线上提供的电源的电压电平和频率进行监控，以确定哪些电力总线处于所需的限制范围内以向航空航天负载提供电力。 如果当前连接的交流电源总线的监控指示总线不在要求的限制范围内，并且可能在不久的将来关闭，则航空航天负载的连接将切换到所需限制内的另一个交流电源总线。 监测提供给负载的电流，以确定电流与当前连接的故障总线之间的电流的过零点到在负载电流的零交叉点执行的良好总线。 还监测提供给航空航天负载的电流的电平以检测故障负载状况。 如果负载电流超过规定限值，则负载将与所有交流电源总线断开，以关闭故障负载。 航空航天电力控制系统通常适用于单相和三相交流电源，在过零点切换为三相交流电源逐相进行。