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    • 31. 发明授权
    • Turbine nozzle vane
    • 涡轮喷嘴叶片
    • US06491493B1
    • 2002-12-10
    • US09719398
    • 2001-02-01
    • Hiroyoshi WatanabeHideomi Harada
    • Hiroyoshi WatanabeHideomi Harada
    • F01D514
    • F01D5/145
    • A turbine nozzle comprises an array of nozzle blades (1) U disposed circumferentially in an annular passage (4) defined between inner and outer rings of a diaphragm and fixed to the inner and outer rings of the turbine diaphragm. The flow passage is defined between a pressure surface (F) and a suction surface (B) of adjacent ones of the nozzle blades, and a cross section of the flow passage includes predetermined ranges extending along a blade height (h) from the inner and outer diameter surfaces (hub and tip end walls) and defined by a curved line, and another range defined by a substantially straight line.
    • 涡轮喷嘴包括在隔膜的内环和外环之间限定的环形通道(4)周向设置的一组喷嘴叶片(1),并固定到涡轮隔膜的内环和外环。 流动通道限定在相邻喷嘴叶片的压力表面(F)和吸力表面(B)之间,并且流动通道的横截面包括沿着从内部的叶片高度(h)延伸的预定范围, 外径表面(轮毂和尖端端壁)并由曲线限定,另一范围由基本上直线限定。