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发明授权
US07891192B2 Gas turbine engine combustor assembly having integrated control valves 有权
具有集成控制阀的燃气轮机发动机燃烧器组件

Gas turbine engine combustor assembly having integrated control valves
摘要：
A combustor assembly for a gas turbine engine includes a combustor endcover having at least one fuel circuit and mounted thereto a plurality of pre-mixers and at least one control valve. The at least one control valve is fluidly connected to the at least one fuel circuit and operatively connected to a controller. The controller selectively operates the at least one control valve to deliver fuel through the at least one fuel circuit to the plurality of pre-mixers in order to achieve an enhanced level of operational flexibility by providing individual combustion chamber control.
摘要（中）：

用于燃气涡轮发动机的燃烧器组件包括具有至少一个燃料回路并且安装到其上的多个预混合器和至少一个控制阀的燃烧器端盖。 所述至少一个控制阀流体地连接到所述至少一个燃料回路并可操作地连接到控制器。 控制器选择性地操作至少一个控制阀以将燃料通过至少一个燃料回路输送到多个预混合器，以通过提供单独的燃烧室控制来实现增强的操作灵活性水平。

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