| 摘要 |
A supersonic compressor (10) includes a fluid inlet (26), a fluid outlet (28), and a fluid conduit extending there between with a supersonic compressor rotor (40) disposed therein. The supersonic compressor rotor includes a first end wall (60) and a plurality of vanes ( 46) coupled thereto. Each pair of the vanes defines a fluid flow channel (80). The fluid flow channel defines a flow channel inlet opening (76) and a flow channel outlet opening (78) and includes a throat portion (124). The supersonic compressor rotor also includes a second end wall (90) and at least one axially translatable fluid control device (172) positioned adjacent to the rotor. The axially translatable fluid control device is configured to obstruct the throat portion and includes at least one axially translatable protrusion (178) insertable into at least a portion of the throat portion. |
