发明名称 Turbine blade for a flow engine with profiled trailing edge, blade and integrally bladed rotor
摘要 The present invention relates to an airfoil for a fluid flow machine (100), having a suction side (5), a pressure side (7) and an airfoil trailing edge (200). The airfoil (100), at least in portions thereof, has a profile (9) in the region of the airfoil trailing edge (200), which profile extends over the suction side (5) and the pressure side (7) of the airfoil trailing edge (200). The present invention also relates to a blade and an integrally bladed rotor.
申请公布号 EP2789798(A3) 申请公布日期 2015.01.21
申请号 EP20140162553 申请日期 2014.03.31
申请人 MTU AERO ENGINES AG 发明人 RAMM, GÜNTER;LANG, CHRISTINE
分类号 F01D5/14;F04D29/38 主分类号 F01D5/14
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