公开(公告)号：WO2007103777A2

公开(公告)日：2007-09-13

申请号：PCT/US2007063144

申请日：2007-03-02

Applicant: HONEYWELL INT INC ,  VRBAS GARY D

Inventor： VRBAS GARY D

IPC: F01D17/16 ,  F02B37/013 ,  F02B37/24 ,  F02C3/08 ,  F02C3/09 ,  F02C6/12

CPC classification number: F02C6/12 ,  F01D17/162 ,  F01D17/165 ,  F02B37/004 ,  F02B37/013 ,  F02B37/24 ,  F02C3/085 ,  F04D17/025 ,  F04D25/04 ,  F05D2270/10 ,  Y02T10/144

Abstract: [0043] A turbocharger, having an axial compressor wheel and an axial turbine wheel mounted on a first shaft supported by a housing, and a radial compressor wheel and a radial turbine wheel mounted on a second shaft, the second shaft concentrically extending around the first shaft and being supported by the housing. The housing defines a first duct extending axially from the exducer of the axial compressor to the inducer of the radial compressor, and a second duct extending axially from the exducer of the radial turbine to the inducer of the axial turbine. A plurality of controllable compressor guide vanes extend through the first duct, and a plurality of controllable turbine stator vanes extend through the second duct. The housing is provided with variable diffuser vanes at the exducer of the radial compressor, and with variable turbine vanes at the inducer of the radial turbine. The variable turbine vanes and the turbine stator vanes are controlled to accurately control the rotation rate of the radial and axial turbines. The compressor guide vanes are controiled to minimize surge and maximize choke flow rate.

Abstract translation: 涡轮增压器，其具有安装在由壳体支撑的第一轴上的轴向压缩机叶轮和轴向涡轮机叶轮，以及安装在第二轴上的径向压缩机叶轮和径向涡轮机叶轮，所述第二轴同心地围绕第一轴 并且由壳体支撑。 壳体限定了从轴向压缩机的排放器轴向延伸到径向压缩机的引导器的第一管道，以及从径向涡轮机的排放器轴向延伸到轴向涡轮机的引导器的第二管道。 多个可控制的压缩机导向叶片延伸穿过第一管道，并且多个可控制的涡轮机定子叶片延伸通过第二管道。 壳体在径向压缩机的排放器处设置有可变的扩散器叶片，并且在径向涡轮机的引导器处具有可变涡轮叶片。 控制可变涡轮机叶片和涡轮机定子叶片以精确地控制径向和轴向涡轮机的旋转速率。 压缩机导叶受到控制以最小化浪涌并最大限度地提高扼流流量。