| 发明名称 |
BLADE, SHROUD AND TURBOMACHINE |
| 摘要 |
The invention relates to a blade for a turbomachine a shroud for such a blade, and a turbomachine having at least one such blade. The blade comprises a shroud which is positioned on the blade tip side of the blade and is stiffened in the region of its surface by means of a stiffening structure having at least one longitudinal stiffening element such as a rib. The height of the longitudinal stiffening element varies in the circumferential direction. |
| 申请公布号 |
US2016237829(A1) |
申请公布日期 |
2016.08.18 |
| 申请号 |
US201615008742 |
申请日期 |
2016.01.28 |
| 申请人 |
MTU Aero Engines AG |
发明人 |
KOZDRAS Marcin;SKURA Krzysztof;LEBIEDOWICZ Piotr;SZPONAR Marek |
| 分类号 |
F01D5/22;F04D29/08;F04D29/38;F01D5/14 |
主分类号 |
F01D5/22 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A blade for a turbomachine, wherein the blade comprises a shroud which is positioned on a blade tip side of the blade and is stiffened in a region of its surface by a stiffening structure comprising at least one rib, and wherein a height of the rib varies in circumferential direction. |
| 地址 |
Munich DE |
