发明名称 ROTORS WITH MODULUS MISTUNED AIRFOILS
摘要 A rotor assembly for a gas turbine engine includes a rotor defining an outer periphery; and a plurality of blades attached to the outer periphery. The plurality of blades includes a material property different than the other of the plurality of blades to provide mistuning of the rotor.
申请公布号 WO2014197119(A3) 申请公布日期 2015.03.19
申请号 WO2014US33407 申请日期 2014.04.09
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 GRELOTTI, ROBERT A.;MORRIS, ROBERT J.
分类号 F01D5/00;F01D5/02;F01D5/14;F01D5/30 主分类号 F01D5/00
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