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