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    • 70. 发明申请
    • Centrifuge turbine
    • 离心机
    • US20170067343A1
    • 2017-03-09
    • US14756450
    • 2015-09-04
    • Steven L. Maugh
    • Steven L. Maugh
    • F01D1/32F01D5/04
    • F01D1/32F01D5/043F01D5/048F02C3/165
    • A centrifuge type turbine. The turbine has a circular hollow rotor having a centrally located air and fuel inlet and an outer periphery. A stationary exhaust shroud surrounds the outer periphery of the rotor. The rotor has at least two spiral shaped swirl channels located therein extending from the air and fuel inlet to an outlet located at its outer periphery. The swirl channels are formed by stationary spiral walls. The air and fuel inlet has a plurality of stationary curved blades located therein and adapted to rotate with the rotor and to swirl and admix fuel and air introduced thereinto. An ignition source located in the exhaust shroud ignites the air/fuel mixture. A plurality of stationary push point members are located within the exhaust shroud.
    • 离心式涡轮机。 涡轮机具有圆形中空转子,其具有位于中心的空气和燃料入口以及外周边。 固定排气罩围绕转子的外周。 转子具有位于其中的至少两个螺旋形旋转通道,其从空气和燃料入口延伸到位于其外周边处的出口。 涡流通道由固定螺旋壁形成。 空气和燃料入口具有多个固定的弯曲刀片,其位于其中并且适于与转子一起旋转并且旋转并混合引入其中的燃料和空气。 位于排气罩中的点火源点燃空气/燃料混合物。 多个固定推动部件位于排气罩内。