摘要 |
The invention relates to a method for the generative production of a component (1) with an integrated damping element for a turbomachine, in particular a gas turbine, having the following method steps: assembling the component (1) in a generative manner, and introducing a damping material (2) into the component (1) during the method step of the generative assembly of the component (1). The invention further relates to a component (1) with an integrated damping element for a turbomachine, in particular a gas turbine, wherein the component (1) is assembled in a generative manner, and the component (1) has a damping material (2) which is introduced into the component (1) during the generative assembly of the component (1). The invention further relates to a turbomachine, in particular a gas turbine, comprising such a component (1). |
申请人 |
MTU AERO ENGINES GMBH;NEUHAEUSLER, STEFAN;SATZGER, WILHELM;SIKORSKI, SIEGFRIED;DUSEL, KARL-HEINZ;MELZER, HANS-CHRISTIAN;BAYER, ERWIN |
发明人 |
NEUHAEUSLER, STEFAN;SATZGER, WILHELM;SIKORSKI, SIEGFRIED;DUSEL, KARL-HEINZ;MELZER, HANS-CHRISTIAN;BAYER, ERWIN |