TY - GEN
T1 - On the pressure losses due to the tip clearance of centrifugal blowers
AU - Ishida, M.
AU - Senoo, Y.
N1 - Publisher Copyright:
© Copyright 1980 by ASME.
PY - 1980
Y1 - 1980
N2 - The pressure distribution along the shroud is measured for three types of centrifugal impeller at seven different values of tip clearance each. The change of input power due to a change of tip clearance is related to the effective blockage at the impeller tip. Since the change of input power is little for the test cases, the variation of local pressure gradient along the shroud is mostly attributed to the change of local pressure loss. The local pressure loss is related to the local tip clearance ratio and to the local pressure gradient based on the decleration of relative velocity in the impeller. Since the local pressure gradient is largest near the throat of impeller is used as the representative value. The tip clearance loss is related to the clearance ratio and the pressure rise based on the deceleration of relative velocity in the impeller. A good correlation is observed in all cases at various flow rate.
AB - The pressure distribution along the shroud is measured for three types of centrifugal impeller at seven different values of tip clearance each. The change of input power due to a change of tip clearance is related to the effective blockage at the impeller tip. Since the change of input power is little for the test cases, the variation of local pressure gradient along the shroud is mostly attributed to the change of local pressure loss. The local pressure loss is related to the local tip clearance ratio and to the local pressure gradient based on the decleration of relative velocity in the impeller. Since the local pressure gradient is largest near the throat of impeller is used as the representative value. The tip clearance loss is related to the clearance ratio and the pressure rise based on the deceleration of relative velocity in the impeller. A good correlation is observed in all cases at various flow rate.
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U2 - 10.1115/80GT139
DO - 10.1115/80GT139
M3 - Conference contribution
AN - SCOPUS:84953931515
T3 - Proceedings of the ASME Turbo Expo
BT - General
PB - American Society of Mechanical Engineers (ASME)
T2 - ASME 1980 International Gas Turbine Conference and Products Show, GT 1980
Y2 - 10 March 1980 through 13 March 1980
ER -