发明名称 Damping element for reducing the vibration of an airfoil
摘要 An airfoil (10) is provided with a tip (12) having an opening (14) to a center channel (24). A damping element (16) is inserted within the opening of the center channel, to reduce an induced vibration of the airfoil. The mass of the damping element, a spring constant of the damping element within the center channel, and/or a mounting location (58) of the damping element within the center channel may be adjustably varied, to shift a resonance frequency of the airfoil outside a natural operating frequency of the airfoil.
申请公布号 US8579593(B2) 申请公布日期 2013.11.12
申请号 US20090613957 申请日期 2009.11.06
申请人 CAMPBELL CHRISTIAN X.;MARRA JOHN J.;SIEMENS ENERGY, INC. 发明人 CAMPBELL CHRISTIAN X.;MARRA JOHN J.
分类号 F01D5/14;F01D5/16;F01D5/18 主分类号 F01D5/14
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