FIELD: compressor manufacture. SUBSTANCE: compression in radial peripheral turbine is realized due to centripetal rotation of gas flows around axis of turbomachine in direction opposite relative to its rotation sign and due to formation of cylindrical swirl at its outlet. Compression is realized in elongated narrowing curvilinear ducts with length and width values significantly more than their height values. Outlet cylindrical swirl passes to cone swirl narrowed along axis. EFFECT: enhanced degree of compression, high efficiency. 1 dwg
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Authors
Dates
2000-12-10—Published
2000-05-19—Filed