SHORTED ROTATING DIODE PROTECTION FOR SYNCHRONOUS MACHINES

    公开(公告)号:US20200007057A1

    公开(公告)日:2020-01-02

    申请号:US16566062

    申请日:2019-09-10

    Abstract: An assembly according to an embodiment of the present disclosure includes, among other things, a synchronous machine including a rotating portion and a stationary portion, the rotating portion including at least one rotating diode coupled to a field winding, and the stationary portion including a stator winding and an exciter winding. A control unit includes a first gate and a second gate. The exciter winding is connected in series to the first gate and the second gate during a first operating mode to energize the exciter winding. The exciter winding is electrically connected in series to a first gate but is electrically disconnected from the second gate in a second, different operating mode to electrically disconnect the exciter winding from an exciter energy source. A method of operating a synchronous machine is also disclosed.

    Shorted rotating diode protection for synchronous machines

    公开(公告)号:US10469011B2

    公开(公告)日:2019-11-05

    申请号:US15675090

    申请日:2017-08-11

    Abstract: An assembly according to an embodiment of the present disclosure includes, among other things, a synchronous machine including a rotating portion and a stationary portion, the rotating portion including at least one rotating diode coupled to a field winding, and the stationary portion including a stator winding and an exciter winding. A control unit includes a first gate and a second gate. The exciter winding is connected in series to the first gate and the second gate during a first operating mode to energize the exciter winding. The exciter winding is electrically connected in series to a first gate but is electrically disconnected from the second gate in a second, different operating mode to electrically disconnect the exciter winding from an exciter energy source. A method of operating a synchronous machine is also disclosed.

    Wound field generator overvoltage prevention

    公开(公告)号:US10326394B2

    公开(公告)日:2019-06-18

    申请号:US15792475

    申请日:2017-10-24

    Abstract: An aircraft main power generation system includes a rotor shaft, a main power generator a permanent magnet, an exciter, an aircraft power bus, and a generator control unit. The generator control unit is configured to provide a control current to the exciter in response to a speed of the main power generator reaching a threshold speed and electrically couple the main power generator to the aircraft power bus in response to the speed of the main power generator reaching a minimum operating speed, the threshold speed being lower than the minimum operating speed; or provide a control current to the exciter in response to the speed of the main power generator reaching a predetermined speed and electrically coupling the main power generator to the aircraft power bus in response to a time period elapsing after the speed of the main power generator has reached the predetermined speed.

    WOUND FIELD GENERATOR OVERVOLTAGE PREVENTION
    15.
    发明申请

    公开(公告)号:US20190123669A1

    公开(公告)日:2019-04-25

    申请号:US15792475

    申请日:2017-10-24

    Abstract: An aircraft main power generation system includes a rotor shaft, a main power generator a permanent magnet, an exciter, an aircraft power bus, and a generator control unit. The generator control unit is configured to provide a control current to the exciter in response to a speed of the main power generator reaching a threshold speed and electrically couple the main power generator to the aircraft power bus in response to the speed of the main power generator reaching a minimum operating speed, the threshold speed being lower than the minimum operating speed; or provide a control current to the exciter in response to the speed of the main power generator reaching a predetermined speed and electrically coupling the main power generator to the aircraft power bus in response to a time period elapsing after the speed of the main power generator has reached the predetermined speed.

    OVERVOLTAGE LIMITER IN AN AIRCRAFT ELECTRICAL POWER GENERATION SYSTEM
    16.
    发明申请
    OVERVOLTAGE LIMITER IN AN AIRCRAFT ELECTRICAL POWER GENERATION SYSTEM 审中-公开
    飞机电力发电系统中的过压限制

    公开(公告)号:US20150137786A1

    公开(公告)日:2015-05-21

    申请号:US14606293

    申请日:2015-01-27

    Abstract: A method of limiting a generator voltage in an overvoltage condition includes the steps of determining an amount of overvoltage of a generator output voltage exceeding a specified voltage and calculating a reference threshold voltage based upon the duration of overvoltage. A switch is modulated according to a voltage error between the output voltage and the reference threshold voltage. The current flow within the generator is interrupted based upon the voltage error to limit the output voltage to a desired voltage.

    Abstract translation: 限制发电机电压处于过电压状态的方法包括以下步骤:确定发电机输出电压超过规定电压的过电压量,并根据过电压的持续时间计算参考阈值电压。 根据输出电压和参考阈值电压之间的电压误差来调制开关。 基于电压误差,发电机内的电流中断,以将输出电压限制到所需的电压。

    Arc fault induced differential protection isolation

    公开(公告)号:US11641101B2

    公开(公告)日:2023-05-02

    申请号:US17221481

    申请日:2021-04-02

    Abstract: A method includes detecting an initial fault in a system and opening a contactor to isolate a load bus from the system for a window of time. During the window of time, the method includes detecting whether current flows from a generator of the system. If current flows from the generator of the system during the window of time, the method includes isolating the load bus from the generator. If current does not flow from the generator to the system during the window of time, the method includes isolating the load bus from all sources including the generator.

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