Turbomachinery and method of manufacturing the same
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United States of America Patent
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-
May 16, 2000
Grant Date -
N/A
app pub date -
Oct 23, 1997
filing date -
Dec 7, 1995
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
An impeller in a turbomachinery has blades designed such that reduced static pressure difference .DELTA.Cp between the hub and the shroud on the suction surface of the blade shows a remarkably decreasing tendency near the impeller exit as it approaches the impeller exit between the impeller inlet and the impeller exit.
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