Apparatus for ignition and reignition for a gas turbine
    1.
    发明授权
    Apparatus for ignition and reignition for a gas turbine 失效
    燃气轮机点火和重燃点装置

    公开(公告)号:US4414804A

    公开(公告)日:1983-11-15

    申请号:US334220

    申请日:1981-12-24

    Abstract: A spark ignition system for a gas turbine electronically controls the cycle of charge and discharge of a spark generator of the capacitive type. There is a function generator (5) which derives a reference voltage as a function of the speed of the turbine and possibly of other parameters. A charge control (6) for the capacitive cell (9) and a spark frequency control (7) are controlled by the reference voltage. Reignition in the case of flame extinction is controlled by an opto-electronic arrangement (11, 12, 13) which drives a reignition circuit (14), when flame extinction is detected. The reignition circuit produces a voltage which is superimposed on and over-rides the speed reference voltage to activate the system to produce ignition at a start condition.The system can be used for ignition of a gas turbine, especially a turbo-compressor.

    Abstract translation: 用于燃气轮机的火花点火系统电子地控制电容式火花发生器的充放电循环。 有一个函数发生器(5),它将参考电压作为涡轮速度和其他参数的函数。 用于电容单元(9)的电荷控制(6)和火花频率控制(7)由参考电压控制。 在火焰熄灭的情况下,当检测到火焰熄灭时,通过驱动重新点火电路(14)的光电子装置(11,12,13)来控制重燃。 重新点火电路产生叠加在速度参考电压上并超越速度参考电压的电压,以激活系统以在起动条件下产生点火。 该系统可用于燃气轮机,特别是涡轮压缩机的点火。

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