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 |