Low-cost general aviation fuel control system
    1.
    发明授权
    Low-cost general aviation fuel control system 失效
    低成本通用航空燃油控制系统

    公开(公告)号:US06675570B2

    公开(公告)日:2004-01-13

    申请号:US09882858

    申请日:2001-06-15

    IPC分类号: F02C926

    CPC分类号: F02C9/32 F02C9/30 Y02T50/671

    摘要: A fuel system for providing a desired fuel flow to an engine comprises a metering assembly for providing a variable portion of metered fuel flow to an associated nozzle system. The variable portion corresponds to a variable demand signal received by the metering assembly. A centrifugal pumping assembly is adapted to receive fuel from an associated pumping system. The centrifugal pumping assembly is capable of pressurizing and delivering adequate fuel flow to the metering assembly. A throttling valve is in fluid communication between the metering assembly and the centrifugal pumping assembly to maintain a constant pressure rise across the metering assembly. An electronic engine control provides the variable demand signal to the metering assembly.

    摘要翻译: 用于向发动机提供期望的燃料流的燃料系统包括用于向相关联的喷嘴系统提供计量燃料流的可变部分的计量组件。 可变部分对应于由计量组件接收的可变需求信号。 离心泵送组件适于从相关联的泵送系统接收燃料。 离心泵组件能够对计量组件加压和输送足够的燃料流。 节流阀在计量组件和离心泵组件之间处于流体连通状态,以保持整个计量组件的恒定的压力上升。 电子发动机控制向计量组件提供可变需求信号。