| 摘要 |
A supersonic compressor rotor. The supersonic compressor rotor includes a substantially cylindrical disk body (56) that includes an upstream surface (68), a downstream surface (70), and a radially outer surface (66) that extends generally axially between the upstream surface (68) and the downstream surface. The disk body defines a centerline axis (62). A plurality of vanes (54) are coupled to the radially outer surface. Adjacent vanes form a pair and are oriented such that a flow channel (88) is defined between each pair of adjacent vanes. The flow channel extends generally axially between an inlet opening (90) and an outlet opening (92). At least one supersonic compression ramp (112) is positioned within the flow channel. The supersonic compression ramp is selectively positionable at a first position (156), at a second position (158), and at any position therebetween. |
