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    • 8. 发明申请
    • Methods and apparatus for operating gas turbine engine systems
    • 运行燃气涡轮发动机系统的方法和装置
    • US20070113560A1
    • 2007-05-24
    • US11284491
    • 2005-11-22
    • Charles SteberMassoud ParisayRavindra AnnigeriWilly ZiminskyJohn Henderson
    • Charles SteberMassoud ParisayRavindra AnnigeriWilly ZiminskyJohn Henderson
    • F02C9/28
    • F23N5/003F23N2021/10F23N2041/20F23R3/00Y02T50/677
    • Methods and systems for operating a gas turbine engine system include an electrical generator configured to provide electrical energy to a load, a gas turbine engine including at least one combustor that includes a plurality of fuel injection points configured to inject a fuel into the combustor at a plurality of different locations wherein the combustor configured to combust the fuel and the gas turbine engine is rotatably coupled to the generator through a shaft. The gas turbine engine system includes a control system including a plurality of sensors positioned about the gas turbine engine system and configured to measure at least one parameter associated with the sensor, a processor programmed to receive a signal indicative of a heating value of the fuel, and automatically control a fuel split between the fuel injection points on the combustor using the determined heating value.
    • 用于操作燃气涡轮发动机系统的方法和系统包括被配置为向负载提供电能的发电机,包括至少一个燃烧器的燃气涡轮发动机,该至少一个燃烧器包括多个燃料喷射点,燃料喷射点被配置成在 多个不同的位置,其中构造成燃烧燃料和燃气涡轮发动机的燃烧器通过轴可旋转地联接到发电机。 所述燃气涡轮发动机系统包括控制系统,所述控制系统包括围绕所述燃气涡轮发动机系统定位的多个传感器,所述多个传感器被配置为测量与所述传感器相关联的至少一个参数,被编程为接收指示所述燃料的热值的信号的处理器 并使用所确定的热值自动控制燃烧器上的燃料喷射点之间的燃料分配。