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    • 3. 发明专利
    • Turbine housing
    • JP5260258B2
    • 2013-08-14
    • JP2008324722
    • 2008-12-19
    • 三菱重工業株式会社
    • 大剛 渡辺巧 時吉幹 惠比寿
    • F02B39/00
    • PROBLEM TO BE SOLVED: To provide a turbine housing inhibiting occurrence and progress of a crack in a tongue portion without limiting an amount of exhaust gas flowing in the turbine housing. SOLUTION: The turbine housing is provided with an exhaust gas flow path of a circumferential shape in the inside and has the tongue portion separating the exhaust gas flowing into the exhaust gas flow path from the exhaust gas flowed and swirled in the exhaust gas flow path, and a slit is formed in a central area of the tongue portion in a thickness direction perpendicular to the exhaust gas flow and in a direction almost parallel to the exhaust gas flow. The slit is formed over the entire surface in a transverse direction of the tongue portion almost parallel to the exhaust gas flow and has a depth in which thermal stress occurring in the deepest portion ranges from 1/2 to 1/3 of thermal stress occurring in the surface of the tongue portion. COPYRIGHT: (C)2010,JPO&INPIT