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    Power control for induction motors using variable frequency AC power
    1.
    发明申请
    Power control for induction motors using variable frequency AC power 有权
    使用变频交流电源的感应电动机的功率控制

    公开(公告)号：US20080074076A1

    公开(公告)日：2008-03-27

    申请号：US11527067

    申请日：2006-09-26

    申请人： Robert E. Fisher ,  John T. Paterson

    发明人： Robert E. Fisher ,  John T. Paterson

    IPC分类号： H02P27/04

    CPC分类号： H02P27/04

    摘要： An autonomous controller allows an AC induction motor to operate over a broad range of AC power supply frequencies by reducing the amount of current supplied to the motor at lower frequencies. The controller detects the frequency of the power supply and switches the supply current on and off during each AC cycle to limit the RMS current to a value that is related to the detected frequency. Alternatively, the controller switches capacitive reactance into the power supply circuit which reduces the current supplied to the motor at lower AC frequencies.

    摘要翻译： 自主控制器允许AC感应电动机通过减少在较低频率下提供给电动机的电流量，在宽范围的交流电源频率上工作。 控制器检测电源的频率，并在每个AC循环期间打开和关闭电源电流，以将RMS电流限制为与检测到的频率相关的值。 或者，控制器将电容电抗器切换到电源电路中，这降低了在较低AC频率下提供给电动机的电流。

    Power control for induction motors using variable frequency AC power
    2.
    发明授权
    Power control for induction motors using variable frequency AC power 有权
    使用变频交流电源的感应电动机的功率控制

    公开(公告)号：US07696715B2

    公开(公告)日：2010-04-13

    申请号：US11527067

    申请日：2006-09-26

    申请人： Robert E. Fisher ,  John T. Paterson

    发明人： Robert E. Fisher ,  John T. Paterson

    IPC分类号： H02P27/04

    CPC分类号： H02P27/04

    摘要： An autonomous controller allows an AC induction motor to operate over a broad range of AC power supply frequencies by reducing the amount of current supplied to the motor at lower frequencies. The controller detects the frequency of the power supply and switches the supply current on and off during each AC cycle to limit the RMS current to a value that is related to the detected frequency. Alternatively, the controller switches capacitive reactance into the power supply circuit which reduces the current supplied to the motor at lower AC frequencies.

    摘要翻译： 自主控制器允许AC感应电动机通过减少在较低频率下提供给电动机的电流量，在宽范围的交流电源频率上工作。 控制器检测电源的频率，并在每个AC循环期间打开和关闭电源电流，以将RMS电流限制为与检测到的频率相关的值。 或者，控制器将电容电抗器切换到电源电路中，这降低了在较低AC频率下提供给电动机的电流。

    Power Control For Induction Motors Using Variable Frequency AC Power
    3.
    发明申请
    Power Control For Induction Motors Using Variable Frequency AC Power 有权
    使用变频交流电源的感应电动机功率控制

    公开(公告)号：US20100148719A1

    公开(公告)日：2010-06-17

    申请号：US12706053

    申请日：2010-02-16

    申请人： Robert E. Fisher ,  John T. Paterson

    发明人： Robert E. Fisher ,  John T. Paterson

    IPC分类号： H02P27/00

    CPC分类号： H02P27/04

    摘要： An autonomous controller allows an AC induction motor to operate over a broad range of AC power supply frequencies by reducing the amount of current supplied to the motor at lower frequencies. The controller detects the frequency of the power supply and switches the supply current on and off during each AC cycle to limit the RMS current to a value that is related to the detected frequency. Alternatively, the controller switches capacitive reactance into the power supply circuit which reduces the current supplied to the motor at lower AC frequencies.

    摘要翻译： 自主控制器允许AC感应电动机通过减少在较低频率下提供给电动机的电流量，在宽范围的交流电源频率上工作。 控制器检测电源的频率，并在每个AC循环期间打开和关闭电源电流，以将RMS电流限制为与检测到的频率相关的值。 或者，控制器将电容电抗器切换到电源电路中，这降低了在较低AC频率下提供给电动机的电流。

    Power control for induction motors using variable frequency AC power
    4.
    发明授权
    Power control for induction motors using variable frequency AC power 有权
    使用变频交流电源的感应电动机的功率控制

    公开(公告)号：US08421398B2

    公开(公告)日：2013-04-16

    申请号：US12706053

    申请日：2010-02-16

    申请人： Robert E. Fisher ,  John T. Paterson

    发明人： Robert E. Fisher ,  John T. Paterson

    IPC分类号： H02P27/00

    CPC分类号： H02P27/04

    摘要： An autonomous controller allows an AC induction motor to operate over a broad range of AC power supply frequencies by reducing the amount of current supplied to the motor at lower frequencies. The controller detects the frequency of the power supply and switches the supply current on and off during each AC cycle to limit the RMS current to a value that is related to the detected frequency. Alternatively, the controller switches capacitive reactance into the power supply circuit which reduces the current supplied to the motor at lower AC frequencies.

    摘要翻译： 自主控制器允许AC感应电动机通过减少在较低频率下提供给电动机的电流量，在宽范围的交流电源频率上工作。 控制器检测电源的频率，并在每个AC循环期间打开和关闭电源电流，以将RMS电流限制为与检测到的频率相关的值。 或者，控制器将电容电抗器切换到电源电路中，这降低了在较低AC频率下提供给电动机的电流。

    ELECTRICAL SYSTEMS ARCHITECTURE FOR AN AIRCRAFT, AND RELATED OPERATING METHODS
    6.
    发明申请
    ELECTRICAL SYSTEMS ARCHITECTURE FOR AN AIRCRAFT, AND RELATED OPERATING METHODS 有权
    用于飞机的电气系统结构及相关操作方法

    公开(公告)号：US20090127855A1

    公开(公告)日：2009-05-21

    申请号：US11944199

    申请日：2007-11-21

    申请人： Mark S. Shander ,  Richard A. Cote ,  Michael L. Drake ,  Howard Carter, III ,  John T. Peters ,  Casey Y.K. Ng ,  Michael S. Hoag ,  John T. Paterson

    发明人： Mark S. Shander ,  Richard A. Cote ,  Michael L. Drake ,  Howard Carter, III ,  John T. Peters ,  Casey Y.K. Ng ,  Michael S. Hoag ,  John T. Paterson

    IPC分类号： H02P9/42 ,  F04B17/03

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

    摘要： An electrical architecture for an aircraft is provided. The electrical architecture is particularly suitable for relatively small, compact, and lightweight aircraft. In one embodiment, the electrical architecture includes an electrical generator component coupled to the aircraft engine, and an air compression system coupled to the electrical generator component. The electrical generator component is configured to receive mechanical power from the engine and to generate a constant frequency AC electrical power from the engine mechanical power, and the air compression system is configured to receive the constant frequency AC power as an input and, in response thereto, produce a pressurized air output having variable characteristics (for example, a variable flow rate or a variable air pressure).

    摘要翻译： 提供飞机的电气结构。 电气结构特别适用于相对较小，紧凑且重量轻的飞机。 在一个实施例中，电气结构包括耦合到飞行器发动机的发电机部件和耦合到发电机部件的空气压缩系统。 发电机部件被配置为从发动机接收机械动力并且从发动机机械动力产生恒定频率的交流电力，并且空气压缩系统被配置为接收作为输入的恒定频率AC电力，并且响应于此 产生具有可变特性（例如，可变流量或可变空气压力）的加压空气输出。

    Independent power generation in aircraft
    8.
    发明授权
    Independent power generation in aircraft 有权
    飞机独立发电

    公开(公告)号：US08657227B1

    公开(公告)日：2014-02-25

    申请号：US12558177

    申请日：2009-09-11

    申请人： Andrew J. Bayliss ,  John T. Paterson ,  Kevin Retz

    发明人： Andrew J. Bayliss ,  John T. Paterson ,  Kevin Retz

    IPC分类号： B64D41/00

    CPC分类号： B64D41/00 ,  B64D13/00 ,  B64D13/06 ,  B64D37/04 ,  B64D37/20 ,  B64D41/007 ,  B64D2013/0603 ,  B64D2013/0644 ,  B64D2041/002 ,  B64D2041/005 ,  B64D2221/00 ,  H02J4/00 ,  H02J2001/004 ,  Y02T50/44 ,  Y02T50/56 ,  Y02T90/36

    摘要： Systems and methods of independent power generation are disclosed. A particular system includes an aircraft having at least one engine and a plurality of independent power units. Each power unit of the plurality of independent power units generates electricity independently of the at least one engine. The plurality of independent power units include at least a first independent power unit that generates first electricity having a first set of electrical characteristics and a second independent power unit that generates second electricity having a second set of electrical characteristics concurrently with the first power unit generating the first electricity. The first set of electrical characteristics is different than the second set of electrical characteristics.

    摘要翻译： 公开了独立发电的系统和方法。 特定系统包括具有至少一个发动机和多个独立动力单元的飞行器。 所述多个独立动力单元中的每个动力单元独立于所述至少一个发动机发电。 所述多个独立动力单元至少包括产生具有第一组电特性的第一电的第一独立功率单元和第二独立功率单元，所述第二独立功率单元产生与所述第一功率单元同时产生第二组电特性的第二电， 第一电 第一组电气特性与第二组电气特性不同。

    Method and application for vehicle power system isolation
    9.
    发明授权
    Method and application for vehicle power system isolation 有权
    车辆电力系统隔离的方法与应用

    公开(公告)号：US08836160B1

    公开(公告)日：2014-09-16

    申请号：US12892871

    申请日：2010-09-28

    申请人： John T. Paterson ,  Donald B. Lee ,  Terrance L. Thomas ,  Richard W. Berman ,  George Liang

    发明人： John T. Paterson ,  Donald B. Lee ,  Terrance L. Thomas ,  Richard W. Berman ,  George Liang

    IPC分类号： H01F3/00

    CPC分类号： H01F27/343 ,  H01F27/02 ,  H01F27/06 ,  H01F27/24 ,  H01F27/29 ,  H01F27/32

    摘要： Presented is a system and method for providing electrical isolation in vehicle power systems. The method comprises placing linear optimized isolation transformers in structures of a vehicle at positions that minimize the propagation of energy spikes into internal electronic systems, for example in the wing root of an aircraft where electrical cables from a generator associated with an engine enter the fuselage. The system includes a linear optimized isolation transformer with a core that has primary side winding isolated from a secondary side winding by an isolation dielectric. The isolation dielectric maintains a high value isolation independent of pressure differences due to operation at different altitudes. In embodiments, linear optimized isolation transformers for each phase of a power distribution system couple power from a generator through a structure of a vehicle thereby increasing electrical isolation of electrical components inside the structure from electrical surges originating outside the structure.

    摘要翻译： 提出了一种在车辆动力系统中提供电气隔离的系统和方法。 该方法包括将车辆结构中的线性优化隔离变压器放置在最小化能量尖峰传播到内部电子系统的位置处，例如在飞机的翼根中，其中来自与发动机相关联的发电机的电缆进入机身。 该系统包括具有芯的线性优化隔离变压器，其具有通过隔离电介质从次级侧绕组隔离的初级侧绕组。 隔离电介质保持高值隔离，独立于由于在不同高度的操作引起的压力差异。 在实施例中，用于配电系统的每个相的线性优化隔离变压器通过车辆的结构耦合来自发电机的功率，从而增加了结构内的电气部件与从结构外部产生的电涌的电隔离。

    Electrical systems architecture for an aircraft, and related operating methods
    10.
    发明授权
    Electrical systems architecture for an aircraft, and related operating methods 有权
    飞机电气系统架构及相关操作方法

    公开(公告)号：US07687927B2

    公开(公告)日：2010-03-30

    申请号：US11944199

    申请日：2007-11-21

    申请人： Mark S. Shander ,  Richard A. Cote ,  Michael L. Drake ,  Howard Carter, III ,  John T. Peters ,  Casey Y. K. Ng ,  Michael S. Hoag ,  John T. Paterson

    发明人： Mark S. Shander ,  Richard A. Cote ,  Michael L. Drake ,  Howard Carter, III ,  John T. Peters ,  Casey Y. K. Ng ,  Michael S. Hoag ,  John T. Paterson

    IPC分类号： H02K7/00

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

    摘要： An electrical architecture for an aircraft is provided. The electrical architecture is particularly suitable for relatively small, compact, and lightweight aircraft. In one embodiment, the electrical architecture includes an electrical generator component coupled to the aircraft engine, and an air compression system coupled to the electrical generator component. The electrical generator component is configured to receive mechanical power from the engine and to generate a constant frequency AC electrical power from the engine mechanical power, and the air compression system is configured to receive the constant frequency AC power as an input and, in response thereto, produce a pressurized air output having variable characteristics (for example, a variable flow rate or a variable air pressure).

    摘要翻译： 提供飞机的电气结构。 电气结构特别适用于相对较小，紧凑且重量轻的飞机。 在一个实施例中，电气结构包括耦合到飞行器发动机的发电机部件和耦合到发电机部件的空气压缩系统。 发电机部件被配置为从发动机接收机械动力并且从发动机机械动力产生恒定频率的交流电力，并且空气压缩系统被配置为接收作为输入的恒定频率AC电力，并且响应于此 产生具有可变特性（例如，可变流量或可变空气压力）的加压空气输出。