Gas turbine starting circuit
    1.
    发明授权
    Gas turbine starting circuit 失效
    气体启动电路

    公开(公告)号:US3858391A

    公开(公告)日:1975-01-07

    申请号:US39178673

    申请日:1973-08-27

    CPC classification number: F02C7/26

    Abstract: A gas turbine power plant includes an electric starter for cranking the engine and an electrical control system, both energized from a storage battery. The control system regulates the operation of the engine and includes a fuel valve solenoid and an atomizing air valve solenoid which are electrically energized. When the engine is started, these devices are energized along with the starter. Because of the heavy current required to operate the starter, the other electromagnetic devices are energized slightly before the starter to allow them to pull in while battery voltage is still at a normal level. The control system is energized by a first relay and amplifier or driver circuit and the starter by a second relay and amplifier or driver circuit. The starter amplifier circuit includes a capacitor which delays its operation for approximately 1/20 second after that of the other amplifier.

    Abstract translation: 燃气轮机发电厂包括用于起动发动机的电动起动器和从蓄电池供电的电气控制系统。 控制系统调节发动机的运行,并且包括通电的燃料阀螺线管和雾化空气阀螺线管。 当发动机起动时,这些装置与起动器一起被通电。 由于操作起动器所需的大电流,其他电磁装置在启动器之前略微通电,以允许它们在电池电压仍处于正常水平时拉入。 控制系统由第一继电器和放大器或驱动电路和起动器由第二继电器和放大器或驱动器电路供电。 起动放大器电路包括一个电容器,其在另一个放大器之后延迟大约1/20秒的操作。

    Gas turbine fuel control
    2.
    发明授权
    Gas turbine fuel control 失效
    燃气轮机燃油控制

    公开(公告)号:US3893291A

    公开(公告)日:1975-07-08

    申请号:US39273973

    申请日:1973-08-29

    CPC classification number: F02C9/32 F05D2270/112

    Abstract: An electrical fuel control system for a gas turbine engine balances a turbine inlet temperature signal against an allowable turbine inlet temperature signal as means for limiting fuel flow to the engine during acceleration. The turbine temperature signal is generated by a thermocouple which has time lag. This signal is compensated for the time lag and for other parameters to improve engine response by a compensating circuit including an operational amplifier. The amplifier has an integrating feedback to compensate for thermocouple lag and it has a differentiating input of a fuel flow signal to provide damping. It has also a feedback of engine acceleration which reduces the temperature compensation to allow for increased fuel flow in anticipation of increased airflow resulting from the acceleration.

    Abstract translation: 用于燃气涡轮发动机的电气燃料控制系统将涡轮入口温度信号与允许的涡轮机入口温度信号平衡,作为在加速期间限制燃料流向发动机的燃料的装置。 涡轮温度信号由具有时间延迟的热电偶产生。 这个信号被补偿了时间滞后和其他参数来改善包括运算放大器在内的补偿电路的发动机响应。 放大器具有积分反馈以补偿热电偶滞后,并且具有燃料流量信号的微分输入以提供阻尼。 它还具有发动机加速度的反馈,这减少了温度补偿以允许在预期由加速度引起的增加的气流的情况下增加燃料流量。

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