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    • 17. 发明申请
    • Gas turbine engine
    • 燃气轮机
    • US20060196191A1
    • 2006-09-07
    • US11072539
    • 2005-03-07
    • William Green
    • William Green
    • F02C7/266
    • F02C3/055F02C7/266
    • A gas turbine engine uses a carburetor or a fuel injector and spark ignition devices to fuel and fire it. A gear pump compresses the air/fuel mixture into a compressor discharge passage connected to ignition holes. The spark ignition devices thread into the ignition holes and ignite the combustible mixture which is pumped up through the ignition holes into horizontal combustion passages that flow the burning gas in between the turbine rotors on their downstream side. The gas pressure forces the turbine rotors in each pair of turbines to accelerate in opposite directions. The turbine rotors are located on the compressor drive shafts and drive the counter rotating compressor rotors. The combustion gas flows through the top sides of the turbines and flows out the sides of the housing through exhaust ports. Another embodiment uses a fuel injector and the combustion gas is pumped into the upstream side of the turbines.
    • 燃气涡轮发动机使用化油器或燃料喷射器和火花点火装置来燃料和燃烧。 齿轮泵将空气/燃料混合物压缩成连接到点火孔的压缩机排出通道。 火花点火装置螺纹连接到点火孔中,并将通过点火孔泵送的可燃混合物点燃到水平燃烧通道,使燃烧气体在其下游侧的涡轮转子之间流动。 气体压力迫使每对涡轮机中的涡轮转子在相反方向上加速。 涡轮转子位于压缩机驱动轴上并驱动反向旋转的压缩机转子。 燃烧气体流过涡轮机的顶侧,并通过排气口流出壳体的侧面。 另一实施例使用燃料喷射器并且燃烧气体被泵送到涡轮机的上游侧。