发明名称 NOZZLE MOUNTING STRUCTURE FOR EXHAUST TURBINE SUPERCHARGER
摘要 <p><P>PROBLEM TO BE SOLVED: To provide a nozzle mounting structure for an exhaust turbine supercharger that is structurally simple and reduces thermal stress. <P>SOLUTION: In this nozzle mounting structure for the exhaust turbine supercharger, the nozzle for increasing the speed of exhaust gas supplied from a gas inlet casing 23 and leading the exhaust gas to a turbine moving blade for driving a rotor shaft comprises a nozzle outer ring 2, a nozzle inner ring, a nozzle vane 6 sandwiched therebetween, and a flange 8 formed on the nozzle inner ring 4 and extending radially inward, and is fastened to the gas inlet casing 23 and mounted. The nozzle mounting structure includes a nozzle supporting body for supporting the nozzle from a rotor disk side. The nozzle supporting body has a stepped shape on its edge. The flange 8 and the edge of the nozzle supporting body are configured to have a stepped shape, and a heat insulating space is provided between the stepped parts of the flange 8 and the supporting body on the radial direction side. <P>COPYRIGHT: (C)2010,JPO&INPIT</p>
申请公布号 JP2010112283(A) 申请公布日期 2010.05.20
申请号 JP20080286204 申请日期 2008.11.07
申请人 MITSUBISHI HEAVY IND LTD 发明人 HAMAGAMI YOSHIYUKI;ARAKAWA HIROYUKI
分类号 F02B37/24;F01D9/02;F01D9/04 主分类号 F02B37/24
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