发明名称 TURBOMACHINE BLADE HAVING A TUNING ELEMENT
摘要 The invention relates to a turbomachine blade (1) with a tuning element (2; 2'; 20) which is provided for impact contact with the blade, with a tuning element guide (3; 3'), in particular a cavity, by which an individual tuning element (2; 2') is movably guided; and/or with a resilient support structure (10) for oscillating storage of the tuning element (20), and wherein the tuning element guide (3; 3') or support structure (10) is fastened to a blade root (1.10), in particular a blade neck (1.12) of the blade.
申请公布号 WO2012095067(A1) 申请公布日期 2012.07.19
申请号 WO2011DE01991 申请日期 2011.11.16
申请人 MTU AERO ENGINES GMBH;HARTUNG, ANDREAS;BORUFKA, HANS PETER;RETZE, ULRICH;STIEHLER, FRANK;KRAUS, JUERGEN;PERNLEITNER, MARTIN 发明人 HARTUNG, ANDREAS;BORUFKA, HANS PETER;RETZE, ULRICH;STIEHLER, FRANK;KRAUS, JUERGEN;PERNLEITNER, MARTIN
分类号 F01D5/16 主分类号 F01D5/16
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