Improvements of Inlet Structure and Sweep-Angle of Guide Vane Inside a Centrifugal Compressor at Large Pre-Swirl[J]. 2017, 51(11): 1-6+50.
DOI:
Improvements of Inlet Structure and Sweep-Angle of Guide Vane Inside a Centrifugal Compressor at Large Pre-Swirl[J]. 2017, 51(11): 1-6+50.DOI: 10.7652/xjtuxb201711001.
Improvements of Inlet Structure and Sweep-Angle of Guide Vane Inside a Centrifugal Compressor at Large Pre-Swirl
the flow loss induced by the inlet guide vane(IGV)usually degrades the economy of the regulation scheme. Aiming at reducing flow loss at large pre-swirl
the sweep angle at the leading edge of the IGV is changed in forward direction relative to the shroud line. The traditional shape of the shroud of the inlet pipe connecting with the IGV is modified to the cone. The secondary flow initiated within the improved design overcomes the considerable hub flow separation caused by the centrifugal force at the high pre-swirl. The situation of the entropy increase is heightened at the impeller inlet. The new structure efficiently improves the polytropic efficiency and the total pressure ratio of the centrifugal compressor within a wide operation range for the pre-swirl of +60 and -60 degrees. The improvements are enhanced with the increasing flow rate. While the left margin in the operation range remains constant
the right margin obviously widens.
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