发明名称 Turbine rotor assembly
摘要 <p>A turbine blade includes an airfoil defined by a convex suction side wall, a concave pressure side wall, a leading edge, a trailing edge, a root, and a tip, the walls and the tip each including an interior surface that defines an interior with the root, the interior including an airfoil cooling circuit for directing airflow through the blade, and a platform supporting the airfoil and having a leading side edge, a trailing side edge, suction side edge, a pressure side edge, an airfoil-facing wall, and a root-facing wall, the platform including a platform cooling circuit having an inlet on the leading side edge and an outlet. The turbine blade may be included in a turbine rotor assembly.</p>
申请公布号 EP2441920(A2) 申请公布日期 2012.04.18
申请号 EP20110184232 申请日期 2011.10.06
申请人 HONEYWELL INTERNATIONAL INC. 发明人 HALFMANN, STEVE;MORRIS, MARK C.
分类号 F01D5/08;F01D5/30 主分类号 F01D5/08
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