发明名称 Variable geometry turbine
摘要 A turbine wheel mounted within a housing rotating about a turbine axis; a gas flow control passage upstream of the turbine wheel between a radial first surface of a movable wall member and a facing wall of the housing, the movable wall member comprising second and third surfaces opposing the first surface. The movable wall member moves in an axial direction to vary the size of the gas flow control passage. A first gas region of the turbine, being upstream of the gas flow control passage, includes a portion of the gas flow control passage; a second gas region of the turbine downstream of the gas flow control passage containing the turbine wheel; and a third gas region of the turbine downstream of the turbine wheel. The first gas region comprises the first and second surfaces, and the second gas region or third gas region comprises the third surface.
申请公布号 US8992165(B2) 申请公布日期 2015.03.31
申请号 US201113238869 申请日期 2011.09.21
申请人 Cummins Turbo Technologies Limited 发明人 Luck David Andrew;Garrett Stephen Edward;Vijayakumar Arun Tamil Selvan
分类号 F01D17/14;F02B37/18;F02B37/24 主分类号 F01D17/14
代理机构 Krieg DeVault LLP 代理人 Krieg DeVault LLP
主权项 1. A variable geometry turbine comprising: a turbine wheel mounted within a housing for rotation about a turbine axis; and flow control passage upstream of said turbine wheel, the gas flow control passage being defined at least in part between a radial first surface of a movable wall member and a facing wall of the housing, the movable wall member also comprising second and third surfaces which oppose the first surface, the movable wall member being movable in an axial direction so as to vary the size of the gas flow control passage; there being a first gas region of the turbine, a portion of which is upstream of the gas flow control passage, the first gas region including at least a portion of the gas flow control passage; a second gas region of the turbine downstream of the gas flow control passage which contains the turbine wheel; and a third gas region of the turbine downstream of the turbine wheel; wherein the first gas region comprises the first and second surfaces, and the second gas region or third gas region comprises the third surface.
地址 Huddersfield GB