发明名称 MULTISTAGE COMPRESSOR WITH IMPROVED MAP WIDTH PERFORMANCE
摘要 A compressor typically for use in a turbocharger comprises a downstream radial compressor impeller wheel, an upstream axial compressor impeller wheel and an intermediate stator. The compressor housing has an inlet with inner and outer walls that define between them an MWE gas flow passage. An upstream opening defined by the flow passage provides communication between said passage and the intake and at least one first slot downstream of the upstream opening provides communication between the passage and the inner surface of the inner wall. The stator comprises a plurality of fixed vanes and is disposed in the inner wall of the inlet between the radial and axial impeller wheels. The position of the slot can be at one of several positions along the gas flow passage, hi other embodiments there are second and third slots and the flow passage is divided into two parts. All the arrangements are designed to improve the compressor map width.
申请公布号 US2013189094(A1) 申请公布日期 2013.07.25
申请号 US201313788064 申请日期 2013.03.07
申请人 CUMMINS TURBO TECHNOLOGIES LIMITED;CUMMINS TURBO TECHNOLOGIES LIMITED 发明人 NIKPOUR BAHRAM
分类号 F04D29/42 主分类号 F04D29/42
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