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    • 10. 发明申请
    • TURBINE COMBUSTION CHAMBER PRESSURE ASSISTED CONTROL VALVE
    • 涡轮燃烧室压力辅助控制阀
    • US20170051676A1
    • 2017-02-23
    • US15306985
    • 2014-04-28
    • Moog Inc.
    • David GEIGER
    • F02C7/232F16K17/36
    • F02C7/232F16K3/246F16K17/36
    • A combustion turbine control valve comprising a fuel passage to a combustion chamber, a control valve assembly to meter fuel flow to the combustion chamber, the control valve assembly comprising a metering valve body having a valve seat, a metering valve plug movable relative to the body from an open to a closed position, a chamber separated from the flow passage by the plug, the plug having a first area exposed to the chamber, a second area exposed to the flow passage when in the open position and a third area exposed to the flow passage when in the closed position, the first area being greater than the third area and equal to or less than the second area, a passage connecting the chamber and the upstream side of the flow passage, and an actuator to actuate the body between the closed and open positions.
    • 一种燃烧涡轮机控制阀,包括到燃烧室的燃料通道,控制阀组件,用于计量到燃烧室的燃料流量,该控制阀组件包括具有阀座的计量阀体,相对于阀体可移动的计量阀塞 从打开位置到关闭位置,通过所述塞子与所述流动通道分离的腔室,所述塞子具有暴露于所述腔室的第一区域,当处于所述打开位置时暴露于所述流动通道的第二区域和暴露于所述第二区域的第三区域 当处于关闭位置时,第一区域大于第三区域并且等于或小于第二区域,连接腔室和流动通道的上游侧的通道,以及致动器,用于致动身体 封闭和空头。