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发明公开
CN102562620A 超音速压缩机及其组装方法 无效 - 驳回

超音速压缩机及其组装方法
摘要：
本发明涉及超音速压缩机及其组装方法。一种超音速压缩机(10)包括流体入口(26)、流体出口(28)、在它们之间延伸的流体管道(32)，以及设置在流体管道内的超音速压缩机转子(40)。转子包括包含在径向内表面(56)和径向外表面(58)之间延伸的基本圆柱形本体(50)的转子盘(48)，以及联接到本体上的、从转子盘沿径向向外延伸的多个导叶(46)，相邻的导叶形成一对。转子盘进一步包括在转子盘周围延伸的套罩(200)。套罩联接到该多个导叶中的各个的至少一部分上。径向外表面、相邻的导叶对和套罩定向成使得流体流通道(80)限定在它们之间。转子盘还包括定位在流体流通道内的多个相邻的超音速压缩坡道(98)。
摘要（英）：

The invention relates to a supersonic compressor and method of assembling same. The supersonic compressor (10) includes a fluid inlet (26), a fluid outlet (28), a fluid conduit (32) extending therebetween, a supersonic compressor rotor (40) disposed within the fluid conduit. The rotor includes a rotor disk (48) that includes a substantially cylindrical body (50) extending between a radially inner (56) and outer surface (58), and a plurality of vanes (46) coupled to the body that extend radially outward from the rotor disk, adjacent vanes forming a pair. The rotor disk further includes a shroud (200) extending about the rotor disk. The shroud is coupled to at least a portion of each of the plurality of vanes. The radially outer surface, the pair of adjacent vanes, and the shroud are oriented such that a fluid flow channel (80) is defined therebetween. The rotor disk also includes a plurality of adjacent supersonic compression ramps (98) positioned within the fluid flow channel.

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