High efficiency transonic mixed-flow compressor method and apparatus
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United States of America Patent
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Jul 7, 1987
Grant Date -
N/A
app pub date -
May 8, 1985
filing date -
May 8, 1985
priority date (Note) -
Expired
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Abstract
Method and apparatus for compression of elastic fluids such as air in a rotary continuous flow process particularly of interest in the turbomachinery field. Resulting structure has an envelope or outer diameter favorably comparable with axial flow compressors and a static pressure ratio, cost, and resistance to FOD comparable to centrifugal compressors. Jet propulsion engine apparatus incorporating such a compressor is also presented.
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