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    Electronic load control unit (ELCU) used as bus tie breaker in electrical power distribution systems
    1.
    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。

    Multi-functional LRM performing SSPC and ELCU functions
    4.
    发明授权
    Multi-functional LRM performing SSPC and ELCU functions 有权
    多功能LRM执行SSPC和ELCU功能

    公开(公告)号：US07732939B2

    公开(公告)日：2010-06-08

    申请号：US11873091

    申请日：2007-10-16

    申请人： Randy J. Fuller ,  Zhenning Z. Liu ,  Milind Ghanekar ,  Ted J. Gayowsky

    发明人： Randy J. Fuller ,  Zhenning Z. Liu ,  Milind Ghanekar ,  Ted J. Gayowsky

    IPC分类号： B60L1/00 ,  B60L3/00 ,  H02G3/00

    CPC分类号： B64D47/00 ,  B64D2221/00 ,  Y10T307/305 ,  Y10T307/615

    摘要： On an aircraft, primary power distribution control and secondary power distribution control may be performed with a single line replaceable module (LRM) having an integrated architecture. The LRM may be provided with trip engines that are based on digital signal processors (DSP's). The DSP's may be programmed to allow the trip engines to perform either ELCU functions or SSPC functions. Use of the single LRM precludes a need for complex circuitry that might otherwise be required to coordinate prior-art independent ELCU and SSPC controls.

    摘要翻译： 在飞机上，可以用具有集成架构的单线可更换模块（LRM）来执行主配电控制和二次配电控制。 LRM可以提供基于数字信号处理器（DSP）的跳闸引擎。 DSP的编程可以允许跳闸引擎执行ELCU功能或SSPC功能。 使用单个LRM排除了需要可能需要协调现有独立ELCU和SSPC控制的复杂电路。

    A METHOD OF PROVIDING A SECONDARY MEANS OF OVERLOAD PROTECTION AND LEAKAGE CURRENT PROTECTION IN APPLICATIONS USING SOLID STATE POWER CONTROLLERS
    5.
    发明申请
    A METHOD OF PROVIDING A SECONDARY MEANS OF OVERLOAD PROTECTION AND LEAKAGE CURRENT PROTECTION IN APPLICATIONS USING SOLID STATE POWER CONTROLLERS 失效
    在使用固态功率控制器的应用中提供过载保护和泄漏电流保护的次要方法的方法

    公开(公告)号：US20090021874A1

    公开(公告)日：2009-01-22

    申请号：US11780386

    申请日：2007-07-19

    申请人： Rocco Divito ,  Zhenning Z. Liu ,  Randy J. Fuller ,  That Nguyen

    发明人： Rocco Divito ,  Zhenning Z. Liu ,  Randy J. Fuller ,  That Nguyen

    IPC分类号： H02H3/08 ,  H01H77/00

    CPC分类号： H02H3/023 ,  H02H3/08 ,  Y10T307/944

    摘要： The present invention provides an overload protection circuit having a first switch connected at a first side to a source of electrical power and at a second side to a load, the switch having on and off modes and a second switch connected between the first switch second side and ground, the second switch having on and off modes. A control module generates at least one signal controlling the first switch mode and the second switch mode wherein the signal turns the second switch to the off mode when turning the first switch to the on mode and the signal turning the second switch to an on mode when turning the first switch to the off mode. Both over current and leakage protection are thereby achieved.

    摘要翻译： 本发明提供了一种过载保护电路，其具有在第一侧连接到电源的第一开关和在负载的第二侧，所述开关具有开和关模式，以及第二开关，其连接在第一开关第二侧 并接地，第二开关具有开和关模式。 控制模块产生控制第一开关模式和第二开关模式的至少一个信号，其中当将第一开关转到导通模式时，该信号将第二开关转到关断模式，并且当第二开关处于接通模式时信号将第二开关转到导通模式 将第一个开关转到关闭模式。 从而实现过电流和漏电保护。

    Power line communication based aircraft power distribution system with real time wiring integrity monitoring capability
    6.
    发明授权
    Power line communication based aircraft power distribution system with real time wiring integrity monitoring capability 有权
    基于电力线通信的飞机配电系统具有实时布线完整性监控能力

    公开(公告)号：US07868621B2

    公开(公告)日：2011-01-11

    申请号：US12041941

    申请日：2008-03-04

    申请人： Zhenning Liu ,  Randy J. Fuller ,  Wenjiang Yu ,  Yang Ye ,  Guangjun G. Liu

    发明人： Zhenning Liu ,  Randy J. Fuller ,  Wenjiang Yu ,  Yang Ye ,  Guangjun G. Liu

    IPC分类号： G01R31/08 ,  G01R31/02

    CPC分类号： G01R31/008 ,  G01R31/025 ,  G01R31/086 ,  G01R31/11 ,  H04B3/546 ,  H04B2203/5445 ,  H04B2203/5458 ,  H04B2203/5495

    摘要： A power line communication-based aircraft power distribution system may allow for both power line communication (PLC) technology and spread spectrum time domain reflectometry (SSTDR) technology to be utilized in aircraft power distribution systems to achieve key maintenance functions. Unlike conventional power distribution systems, which may, for example, use only SSTDR for fault detection, the present invention includes a hardware platform that may allow both the PLC and the SSTDR to be utilized in aircraft power distribution systems to achieve key maintenance functions, such as real time wire fault location, and cost and weight savings. Further, unlike conventional power distribution systems, which may only detect and locate damage in feeder conductor wire sections before the power is applied to the load, the power distribution system of the present invention may permit real time wire fault location.

    摘要翻译： 基于电力线通信的飞机配电系统可以允许在飞机配电系统中利用电力线通信（PLC）技术和扩频时域反射计（SSTDR）技术来实现关键维护功能。 与常规配电系统不同，传统配电系统可能例如仅使用SSTDR进行故障检测，本发明包括硬件平台，其可以允许PLC和SSTDR在飞机配电系统中使用以实现关键维护功能，例如 作为实时线路故障定位，并节省成本和重量。 此外，与在功率施加到负载之前只能检测和定位馈线导线部分中的损坏的常规配电系统不同，本发明的配电系统可以允许实时线路故障定位。

    Method and apparatus of capacitor divider based offline AC-DC converter
    7.
    发明授权
    Method and apparatus of capacitor divider based offline AC-DC converter 有权
    基于电容分压器的离线AC-DC转换器的方法和装置

    公开(公告)号：US07808219B2

    公开(公告)日：2010-10-05

    申请号：US11945035

    申请日：2007-11-26

    申请人： Yang Ye ,  Wenjiang Yu ,  Yuanli Kathy Kang ,  Zhenning Z. Liu ,  Randy J. Fuller

    发明人： Yang Ye ,  Wenjiang Yu ,  Yuanli Kathy Kang ,  Zhenning Z. Liu ,  Randy J. Fuller

    IPC分类号： G05F1/613 ,  H02M7/00

    CPC分类号： H02M7/2176 ,  H02M2001/007

    摘要： An AC/DC power converter has, as its first stage, a capacitor divider and rectifier and, as the second stage, a switch mode power supply. This configuration may be suitable for low power low voltage aerospace applications. The benefits of the circuit may include small reactive component size; near sinusoidal input current, low EMI emissions resulting from low inrush current; intrinsic current limiting that may eliminate the need for short circuit protection; and low overall component count.

    摘要翻译： 作为其第一级的AC / DC功率转换器具有电容器分压器和整流器，并且作为第二级，具有开关模式电源。 这种配置可能适用于低功率低压航空航天应用。 电路的优点可能包括小的无功元件尺寸; 接近正弦输入电流，由低浪涌电流导致的低EMI辐射; 本征电流限制可以消除短路保护的需要; 并且总体组件数量较少。

    Intelligent aircraft secondary power distribution system that facilitates condition based maintenance
    8.
    发明授权
    Intelligent aircraft secondary power distribution system that facilitates condition based maintenance 失效
    智能飞机二次配电系统，便于基于条件的维护

    公开(公告)号：US07634329B2

    公开(公告)日：2009-12-15

    申请号：US11682190

    申请日：2007-03-05

    申请人： Zhenning Z. Liu ,  Wenjiang Yu ,  Yang Ye ,  Rocco DiVito ,  Randy J. Fuller ,  Guangjun G. Liu

    发明人： Zhenning Z. Liu ,  Wenjiang Yu ,  Yang Ye ,  Rocco DiVito ,  Randy J. Fuller ,  Guangjun G. Liu

    IPC分类号： G05D17/00 ,  G06F1/28

    CPC分类号： H02J13/0096 ,  B64D2221/00 ,  G05B23/0213 ,  G05B23/0283 ,  H02J1/14 ,  H02J3/02 ,  H02J3/14 ,  H02J4/00 ,  H02J13/0062 ,  H02J13/0075 ,  Y02T50/54

    摘要： An electrical power distribution system comprises a solid state power controller in communication with an aircraft system main data bus via a gateway module and a condition based maintenance module in communication with the solid state power controller via a communication network distinct from the main data bus. A method of load/feeder health assessment for an electrical power distribution system includes applying a controlled excitation to a load; sampling information from the load/feeder system for the load; characterizing a normal behavior of the load/feeder system for the load; determining if the load characteristics are within the normal behavior profile for the load; and shutting down power to the load if load characteristics are not within the profile when immediate action is indicated or generating a health message for the load when immediate action is not required.

    摘要翻译： 电力分配系统包括经由网关模块和基于条件的维护模块与飞行器系统主数据总线通信的固态功率控制器，其经由与主数据总线不同的通信网络与固态功率控制器通信。 一种用于配电系统的负载/馈线健康评估方法包括对负载施加受控激励; 来自负载/馈线系统的负载采样信息; 描述负载/馈线系统对负载的正常行为; 确定负载特性是否在负载的正常行为曲线内; 如果在立即采取行动时指示负载特性不在配置文件内，或在不需要立即采取行动时为负载生成健康信息，则关闭负载电源。

    Method of providing a secondary means of overload protection and leakage current protection in applications using solid state power controllers
    9.
    发明授权
    Method of providing a secondary means of overload protection and leakage current protection in applications using solid state power controllers 失效
    在使用固态功率控制器的应用中提供过载保护和漏电流保护的二次装置的方法

    公开(公告)号：US07586725B2

    公开(公告)日：2009-09-08

    申请号：US11780386

    申请日：2007-07-19

    申请人： Rocco DiVito ,  Zhenning Z. Liu ,  Randy J. Fuller ,  That Nguyen

    发明人： Rocco DiVito ,  Zhenning Z. Liu ,  Randy J. Fuller ,  That Nguyen

    IPC分类号： H02H3/08 ,  H02H9/02 ,  H02H5/04

    CPC分类号： H02H3/023 ,  H02H3/08 ,  Y10T307/944

    摘要： The present invention provides an overload protection circuit having a first switch connected at a first side to a source of electrical power and at a second side to a load, the switch having on and off modes and a second switch connected between the first switch second side and ground, the second switch having on and off modes. A control module generates at least one signal controlling the first switch mode and the second switch mode wherein the signal turns the second switch to the off mode when turning the first switch to the on mode and the signal turning the second switch to an on mode when turning the first switch to the off mode. Both over current and leakage protection are thereby achieved.

    摘要翻译： 本发明提供了一种过载保护电路，其具有在第一侧连接到电源的第一开关和在负载的第二侧，所述开关具有开和关模式，以及第二开关，其连接在第一开关第二侧 并接地，第二开关具有开和关模式。 控制模块产生控制第一开关模式和第二开关模式的至少一个信号，其中当将第一开关转到导通模式时，该信号将第二开关转到关断模式，并且当第二开关处于接通模式时信号将第二开关转到导通模式 将第一个开关转到关闭模式。 从而实现过电流和漏电保护。

    INTEGRATED ELECTRICAL POWER DISTRIBUTION SYSTEM USING COMMON BUILDING BLOCKS
    10.
    发明申请
    INTEGRATED ELECTRICAL POWER DISTRIBUTION SYSTEM USING COMMON BUILDING BLOCKS 有权
    使用通用建筑块的集成电力分配系统

    公开(公告)号：US20080234838A1

    公开(公告)日：2008-09-25

    申请号：US12018670

    申请日：2008-01-23

    申请人： Milind Ghanekar ,  Randy J. Fuller ,  Zhenning Z. Liu ,  Ted J. Gayowsky

    发明人： Milind Ghanekar ,  Randy J. Fuller ,  Zhenning Z. Liu ,  Ted J. Gayowsky

    IPC分类号： G05B11/01 ,  G06F17/00 ,  G05B15/02

    CPC分类号： H02J4/00 ,  B64D2221/00 ,  Y02T50/54

    摘要： An electrical power distribution system includes a data bus, separate from the main aircraft data bus, internal to the aircraft electrical power distribution system and an electric power control unit (EPCU) in communication with the internal data bus. Primary and emergency power distribution subsystems include line replaceable modules (LRM) connected in the aircraft electrical power distribution system as electrical load control units (ELCU), each having a common supervisory control interface in communication with the internal data bus, while a secondary power distribution subsystem includes LRMs connected in the aircraft electrical power distribution system as solid state power control (SSPC) units, each having the common supervisory control interface in communication with the internal data bus. The common supervisory control interfaces all execute a common supervisory control logic for receiving commutation commands from the EPCU and providing status back to the EPCU.

    摘要翻译： 电力分配系统包括与主飞机数据总线分离的数据总线，与飞机配电系统内部以及与内部数据总线通信的电力控制单元（EPCU）。 主要和应急配电子系统包括连接在飞机配电系统中的线路可更换模块（LRM）作为电力负载控制单元（ELCU），每个电气负载控制单元具有与内部数据总线通信的通用监控控制接口，而二次配电 子系统包括作为固态功率控制（SSPC）单元连接在飞机配电系统中的LRM，每个单元具有与内部数据总线通信的通用监控控制接口。 通用的监控控制接口都执行一个通用的监控控制逻辑，用于从EPCU接收换向指令，并向EPCU提供状态。