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    Generator for gas turbine engine having DC bus fault short circuit control using a battery
    2.
    发明授权
    Generator for gas turbine engine having DC bus fault short circuit control using a battery 有权
    用于燃气轮机发电机，具有使用电池的直流总线故障短路控制

    公开(公告)号：US07876542B2

    公开(公告)日：2011-01-25

    申请号：US11839823

    申请日：2007-08-16

    申请人： Gregory I. Rozman ,  Kevin Dooley ,  Vijay K. Maddali

    发明人： Gregory I. Rozman ,  Kevin Dooley ,  Vijay K. Maddali

    IPC分类号： B64D31/00

    CPC分类号： B64D33/00 ,  B64D2221/00 ,  H02J9/06

    摘要： An aircraft electrical system comprises a generator to be driven as part of a gas turbine engine. The generator supplies electrical power to a plurality of accessories associated with the gas turbine engine, and to an aircraft DC bus in parallel to the supply to the accessories. A battery supplies voltage to a control circuit for the generator through a selectively opened and closed switch. A control detects a short circuit on the aircraft DC bus. The battery switch allows power from the battery to flow to provide control voltage for the generator when the control detects a short circuit on the aircraft DC bus.

    摘要翻译： 飞机电气系统包括作为燃气涡轮发动机的一部分驱动的发电机。 发电机对与燃气涡轮发动机相关联的多个附件以及平行于附件供应的飞机DC总线供电。 电池通过选择性地打开和关闭的开关向发电机的控制电路提供电压。 控制器检测飞机直流总线上的短路。 当控制器检测到飞机直流总线上的短路时，电池开关允许来自电池的电力流动以提供发电机的控制电压。

    MOTOR DRIVE ARCHITECTURE FOR HIGH FREQUENCY AC BUS
    3.
    发明申请
    MOTOR DRIVE ARCHITECTURE FOR HIGH FREQUENCY AC BUS 失效
    高频交流总线的电机驱动架构

    公开(公告)号：US20090151362A1

    公开(公告)日：2009-06-18

    申请号：US11955616

    申请日：2007-12-13

    申请人： Gregory I. Rozman ,  Kevin Dooley

    发明人： Gregory I. Rozman ,  Kevin Dooley

    IPC分类号： F02C7/32 ,  H02P27/08 ,  H02M5/40

    CPC分类号： H02P5/46 ,  H02P25/024

    摘要： A motor drive for an electric motor receives high frequency AC current, and delivers this current through a converter which is operable to change the current delivered downstream to an inverter and an electric motor.

    摘要翻译： 用于电动机的电动机驱动器接收高频交流电流，并且通过转换器传送该电流，该转换器可操作以将向下游传递的电流改变为逆变器和电动机。

    ENGINE HAVING POWER BUS FAULT SHORT CIRCUIT CONTROL WITH A DISCONNECTION SWITCH
    5.
    发明申请
    ENGINE HAVING POWER BUS FAULT SHORT CIRCUIT CONTROL WITH A DISCONNECTION SWITCH 有权
    具有断开开关的发动机具有电源总线故障短路电路控制

    公开(公告)号：US20090045292A1

    公开(公告)日：2009-02-19

    申请号：US11839763

    申请日：2007-08-16

    申请人： Vijay K. Maddali ,  Gregory I. Rozman ,  Kevin Dooley

    发明人： Vijay K. Maddali ,  Gregory I. Rozman ,  Kevin Dooley

    IPC分类号： B64D31/00

    CPC分类号： H02J4/00

    摘要： An aircraft electrical system comprises a generator to be driven as part of a gas turbine engine. The generator supplies electrical power to a plurality of accessories associated with the gas turbine engine, and to an aircraft power bus in parallel to the supply to the accessories. A control detects a short circuit on the aircraft power bus. When a short circuit is detected on the aircraft power bus, a switch is driven open to disconnect the aircraft power bus from the generator. In this manner, the power will continue to be delivered to the plurality of accessories. In a separate feature, a control voltage is provided by an auxiliary permanent magnet generator to a voltage regulator for the main generator.

    摘要翻译： 飞机电气系统包括作为燃气涡轮发动机的一部分驱动的发电机。 发电机将电力供应到与燃气涡轮发动机相关联的多个附件，并且与提供给附件的飞机电源总线并联。 控制器检测飞机电源总线上的短路。 当在飞机电源总线上检测到短路时，开关被驱动打开以将飞机电源总线与发电机断开。 以这种方式，电力将继续被传送到多个附件。 在单独的特征中，辅助永久磁铁发电机提供控制电压到主发电机的电压调节器。

    Motor drive architecture for high frequency AC bus
    6.
    发明授权
    Motor drive architecture for high frequency AC bus 失效
    高频交流总线的电机驱动架构

    公开(公告)号：US07710058B2

    公开(公告)日：2010-05-04

    申请号：US11955616

    申请日：2007-12-13

    申请人： Gregory I. Rozman ,  Kevin Dooley

    发明人： Gregory I. Rozman ,  Kevin Dooley

    IPC分类号： H02P27/08 ,  H02M5/40 ,  F02C7/32

    CPC分类号： H02P5/46 ,  H02P25/024

    摘要： A motor drive for an electric motor receives high frequency AC current, and delivers this current through a converter which is operable to change the current delivered downstream to an inverter and an electric motor.

    摘要翻译： 用于电动机的电动机驱动器接收高频交流电流，并且通过转换器传送该电流，该转换器可操作以将向下游传递的电流改变为逆变器和电动机。

    GENERATOR FOR GAS TURBINE ENGINE HAVING DC BUS FAULT SHORT CIRCUIT CONTROL USING A BATTERY
    7.
    发明申请
    GENERATOR FOR GAS TURBINE ENGINE HAVING DC BUS FAULT SHORT CIRCUIT CONTROL USING A BATTERY 有权
    使用电池进行直流母线故障短路控制的气体发动机发电机

    公开(公告)号：US20090045293A1

    公开(公告)日：2009-02-19

    申请号：US11839823

    申请日：2007-08-16

    申请人： Gregory I. Rozman ,  Kevin Dooley ,  Vijay K. Maddali

    发明人： Gregory I. Rozman ,  Kevin Dooley ,  Vijay K. Maddali

    IPC分类号： B64D31/00

    CPC分类号： B64D33/00 ,  B64D2221/00 ,  H02J9/06

    摘要： An aircraft electrical system comprises a generator to be driven as part of a gas turbine engine. The generator supplies electrical power to a plurality of accessories associated with the gas turbine engine, and to an aircraft DC bus in parallel to the supply to the accessories. A battery supplies voltage to a control circuit for the generator through a selectively opened and closed switch. A control detects a short circuit on the aircraft DC bus. The battery switch allows power from the battery to flow to provide control voltage for the generator when the control detects a short circuit on the aircraft DC bus.

    摘要翻译： 飞机电气系统包括作为燃气涡轮发动机的一部分驱动的发电机。 发电机对与燃气涡轮发动机相关联的多个附件以及平行于附件供应的飞机DC总线供电。 电池通过选择性地打开和关闭的开关向发电机的控制电路提供电压。 控制器检测飞机直流总线上的短路。 当控制器检测到飞机直流总线上的短路时，电池开关允许来自电池的电力流动以提供发电机的控制电压。

    Generating system with a regulated permanent magnet machine
    8.
    发明申请
    Generating system with a regulated permanent magnet machine 有权

    公开(公告)号：US20090009146A1

    公开(公告)日：2009-01-08

    申请号：US11825583

    申请日：2007-07-06

    申请人： Gregory I. Rozman ,  Kevin Dooley

    发明人： Gregory I. Rozman ,  Kevin Dooley

    IPC分类号： H02P9/02 ,  H02H7/06 ,  H02M7/217

    CPC分类号： H02P9/10 ,  H02P29/027

    摘要： An electromechanical power transfer system that transfers power between a prime mover and a direct current (DC) electrical power system, comprises: a permanent magnet machine (PMM) that has a permanent magnet (PM) rotor coupled to the prime mover, a stator with a multiphase alternating current (AC) winding coupled to an AC bus and a control coil with a winding that has a configuration to generate a magnetic field with flux that varies the reactance of the stator winding with the application of control coil current; a position sensing system for generating a rotor position signal that is representative of the angular position of the PM rotor; a control coil current sensor for generating a control coil current signal that is representative of the level of electrical current in the control coil; an electrical potential sensor for generating a DC bus potential signal that is representative of the level of DC potential on the DC bus; an electrical current sensor for generating a DC bus current signal that is representative of the level of DC current that the active rectifier supplies to the electrical load by way of the DC bus; an output power estimator that compares the DC bus potential signal with the DC bus current signal to generate an output power signal; a differentiator that receives the output power signal to generate a respective rate of output power signal; a summer that adds the rate of output power signal with the DC bus potential signal to generate a DC potential feedback signal; and a selectable main active/passive rectifier system for converting multiphase AC power developed by the stator to DC power supplied to the electrical load by way of a DC bus; a control coil current regulator system to regulate the control coil current; wherein the control coil current regulator system generates a level of the control coil current that regulates current in the stator to a desired level in response to a control coil current feedback loop that comprises the control coil current signal and a DC bus potential feedback loop that comprises the DC potential feedback signal and in a generating mode the main active rectifier system maintains a constant potential on the DC bus regardless of sudden changes in electrical load on the DC bus in response to the DC bus potential feedback loop and the rotor position feedback loop; and wherein both the control coil current regulator system and the main active rectifier system switch from an active regulating mode to a protection non-regulating mode upon detection of a fault in the DC bus.

    Electric motor control with buck boost converter
    10.
    发明授权
    Electric motor control with buck boost converter 有权
    带升压转换器的电机控制

    公开(公告)号：US08217616B2

    公开(公告)日：2012-07-10

    申请号：US11934170

    申请日：2007-11-02

    申请人： Gregory I. Rozman ,  Kevin Dooley

    发明人： Gregory I. Rozman ,  Kevin Dooley

    IPC分类号： H02P27/00

    CPC分类号： H02K11/0094 ,  H02K9/06 ,  H02M2001/008 ,  H02P25/024 ,  H02P25/22 ,  H02P27/06 ,  H02P2201/07

    摘要： A power supply for an electric motor includes a converter that can increase and decrease a voltage supplied into an inverter and then into the stator windings of the motor. As a separate feature, the inverter includes a control coil which is positioned within a motor housing such that it may be cooled by a thermal management system for the motor.

    摘要翻译： 用于电动机的电源包括能够增加和减少提供给逆变器的电压，然后进入电动机的定子绕组的转换器。 作为单独的特征，逆变器包括控制线圈，该控制线圈定位在电动机壳体内，使得其可以由用于电动机的热管理系统来冷却。