FIELD: machine building.
SUBSTANCE: supersonic compressor rotor contains the rotor disk (48), having top along flow surface (60), bottom along flow surface (62) and radial external surface (58) that has input surface (148), output surface (150) and transient surface (152). The rotor also has blades (46) radially connected to said external surface, at that adjacent blades create pair of blades and are oriented with creation between each pair of adjacent blades of through channel (86), at that said input surface limits the input plane (154) passing between input hole and transient surface, and output surface limits the output plane (156) passing between said output hole and transient surface. The rotor contains at least one supersonic inclined compression section (110) located in the said through channel.
EFFECT: invention simplifies adjustment of the fluid orientation via the through channel of the supersonic compressor.
10 cl, 13 dwg
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