发明名称 AXIAL FLOW TURBINE OF EXHAUST GAS TURBO SUPERCHARGER
摘要 PROBLEM TO BE SOLVED: To save a cost and an assembling time by constituting a bursting protecting ring arranged on the radial direction outer side of a rotary impeller as a wall constitution part extending to a radial direction, which is integrated with the gas inlet side wall of a gas outlet casing, and connecting to the gas inlet casing through the extending member of an axial direction. SOLUTION: The wall 5 of the gas inlet side of a gas outlet casing 2 comprises the extending member 6 of an axial direction connected to a gas inlet casing 1, a gas outlet pipe piece 7 extending to a radial direction, and a bursting protecting ring 8, and the extending member 6 and the gas outlet pipe piece 7 are connected to each other through the ring 8. A turbine disk plate 10 held by an axis 9 is arranged in a turbine casing 3, and it is restricted by a cover ring 12 as a defuser fixed to the ring 8 through a flange 13 outward. The ring 8 is formed having the length 17 of an axial direction or the height 18 of a radial direction larger than the width or the height of an impeller 11.
申请公布号 JPH1047011(A) 申请公布日期 1998.02.17
申请号 JP19970116816 申请日期 1997.05.07
申请人 ASEA BROWN BOVERI AG 发明人 BAETTIG JOSEF;RICANEK RUDOLF
分类号 F02B39/00;F01D21/04;F01D25/24;F02B39/16;F02C3/04;F02C7/00;F02C7/05;F16P7/00;(IPC1-7):F01D25/24 主分类号 F02B39/00
代理机构 代理人
主权项
地址
您可能感兴趣的专利