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    METHOD OF CHARGING AND DISCHARGING OF SUPERCAPACITORS WITHOUT THE USE OF CONVERTERS OR CHARGERS
    2.
    发明申请
    METHOD OF CHARGING AND DISCHARGING OF SUPERCAPACITORS WITHOUT THE USE OF CONVERTERS OR CHARGERS 失效
    没有使用转换器或充电器的超级电容器的充电和放电方法

    公开(公告)号：US20090091302A1

    公开(公告)日：2009-04-09

    申请号：US11867253

    申请日：2007-10-04

    申请人： ILEANA RUSAN ,  David Lazarovich ,  Subodh Keshri ,  Srinivasa R. Dangeti ,  Hassan Ali Kojori ,  Ivan Vuk

    发明人： ILEANA RUSAN ,  David Lazarovich ,  Subodh Keshri ,  Srinivasa R. Dangeti ,  Hassan Ali Kojori ,  Ivan Vuk

    IPC分类号： H02J7/00

    CPC分类号： H02J7/345 ,  H01G11/10 ,  H01G11/14 ,  Y02E60/13 ,  Y02T10/7022 ,  Y10T307/505 ,  Y10T307/527

    摘要： An electrical power system may be provided with temporary power from a bank of supercapacitors connected to a bus of the power system. The supercapacitors may be charged from an output from a primary power source of the system during start-up of the power source. Output voltage of the primary power source may progressively increase and capacitor charging may occur at this progressively increasing voltage. Dedicated current-limiting devices are not required during charging. When temporary power is required the supercapacitors may be discharged sequentially in a series combination so that a high internal voltage of each capacitor is maintained and so that virtually all of the stored energy of the capacitor may be discharged to the bus at a usable voltage.

    摘要翻译： 电力系统可以从连接到电力系统的总线的超级电容器组提供临时电力。 在电源启动期间，超级电容器可以从系统的主电源的输出充电。 主电源的输出电压可能逐渐增加，并且在该逐渐增加的电压下可能发生电容器充电。 充电时不需要专用的限流装置。 当需要临时电力时，超级电容器可以以串联组合顺序放电，使得保持每个电容器的高内部电压，并且几乎所有的电容器的所存储的能量可以以可用的电压被放电到总线。

    Electronic load control unit (ELCU) used as bus tie breaker in electrical power distribution systems
    3.
    发明授权
    Electronic load control unit (ELCU) used as bus tie breaker in electrical power distribution systems 失效
    电力负荷控制单元（ELCU）用作配电系统中的总线断路器

    公开(公告)号：US07626798B2

    公开(公告)日：2009-12-01

    申请号：US12019474

    申请日：2008-01-24

    申请人： Ileana Rusan ,  David Lazarovich ,  Srinivasa R. Dangeti ,  Randy J. Fuller ,  Edwin Yue

    发明人： Ileana Rusan ,  David Lazarovich ,  Srinivasa R. Dangeti ,  Randy J. Fuller ,  Edwin Yue

    IPC分类号： H02H7/00

    CPC分类号： H02J9/06 ,  H02H7/26

    摘要： The present invention provides an electrical power distribution system that includes a first primary distribution panel (PDP) connected to a first source of electrical power and a second PDP connected to a second source of electrical power. The second PDP is connected to the first PDP by a conductor. A first ELCU receives signals corresponding to the flow of current through the first PDP to a load. A second ELCU receiving signals corresponding to the flow of current between the first PDP and the second PDP and a third ELCU receives signals corresponding to the flow of current between the second PDP and the first PDP. The first, second and third ELCUs protect the electrical power distribution system from a variety of fault conditions.

    摘要翻译： 本发明提供了一种配电系统，其包括连接到第一电源的第一主配电板（PDP）和连接到第二电源的第二PDP。 第二PDP通过导体连接到第一PDP。 第一ELCU接收与通过第一PDP的电流相对应的信号到负载。 接收与第一PDP和第二PDP之间的电流相对应的信号的第二ELCU和第三ELCU接收与第二PDP和第一PDP之间的电流相对应的信号。 第一，第二和第三ELCU保护配电系统免受各种故障条件的影响。

    Aerospace electrical power DC subsystem configuration using multi-functional DC/DC converter
    4.
    发明授权
    Aerospace electrical power DC subsystem configuration using multi-functional DC/DC converter 失效
    航空电力直流子系统配置采用多功能DC / DC转换器

    公开(公告)号：US07701082B2

    公开(公告)日：2010-04-20

    申请号：US11589196

    申请日：2006-10-30

    申请人： David Lazarovich ,  Srinivasa R. Dangeti ,  Ileana Rusan

    发明人： David Lazarovich ,  Srinivasa R. Dangeti ,  Ileana Rusan

    IPC分类号： H02J3/02 ,  H02J3/38 ,  H02J5/00 ,  B64D41/00

    CPC分类号： H02J7/34 ,  H02J5/00 ,  H02J7/02 ,  Y02T50/54 ,  Y10T307/313 ,  Y10T307/328 ,  Y10T307/336 ,  Y10T307/367 ,  Y10T307/511 ,  Y10T307/516

    摘要： An apparatus for regulating voltage and aerospace electrical power systems are implemented. A multi-functional apparatus for regulating voltage, according to one embodiment, comprises: a DC to DC converter (315), wherein the DC to DC converter (315) is controlled to operate in a first direction to receive a DC voltage from a first bus (329) and to output a first regulated DC voltage adjusted to charge a battery (307), wherein the first bus (329) receives power from a second bus (201), and is controlled to operate in a second direction to receive a battery DC voltage from the battery (307) and to output a second regulated DC voltage to the first bus (329) to power a load (231) independently or in combination with the second bus (201).

    摘要翻译： 实现用于调节电压和航空航天电力系统的装置。 根据一个实施例的用于调节电压的多功能设备包括：DC-DC转换器（315），其中DC-DC转换器（315）被控制为在第一方向上操作以从第一方向接收DC电压 总线（329）并输出调节为对电池（307）充电的第一调节DC电压，其中第一总线（329）从第二总线（201）接收电力，并且被控制为在第二方向上操作以接收 从电池（307）提供电池直流电压，并向第一总线（329）输出第二调节的直流电压，以独立地或与第二总线（201）组合来为负载（231）供电。