发明名称 Axial turbine for exhaust gas turbochargers
摘要 In an axial turbine for exhaust gas turbochargers, the inner wall of the rotationally symmetrical exhaust gas deflection duct is designed as a deflection collar rigidly connected to the turbocharger shaft and rotating with it. The outer diameter of the deflection collar is greater than the diameter of the turbine disc and, at maximum, equal to the outer diameter of the turbine rotor. An element for contactless sealing of the exhaust gas deflection duct is provided between the rotating deflection collar and the casing. The element for contactless sealing of the deflection duct preferably consists of two labyrinth seals located on a cylindrical surface opening inwards, the sealing air being supplied radially from within between the labyrinth seals by means of a sealing air duct.
申请公布号 US4648790(A) 申请公布日期 1987.03.10
申请号 US19840623199 申请日期 1984.06.21
申请人 BBC BROWN, BOVERI & COMPANY, LIMITED 发明人 HOERLER, HANSULRICH
分类号 F02B39/00;F01D5/00;F01D5/02;F01D5/04;F01D5/08;F01D11/02;F02B37/00;F02C6/12;(IPC1-7):F01D9/02 主分类号 F02B39/00
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