发明名称 |
Blade assembly for turbomachine |
摘要 |
The surface of the blade (1) or a wall (2) in the region of corner flow is provided with at least one auxiliary blade extending from the surface of the blade and/or wall into the flow, set against the flow at this point. In the wake of the auxiliary blade, an eddy is formed whose rotation direction is directed to induce a velocity on the associated blade surface from the blade center to the transition region between wall and blade. |
申请公布号 |
EP0976928(A2) |
申请公布日期 |
2000.02.02 |
申请号 |
EP19990114975 |
申请日期 |
1999.07.30 |
申请人 |
DLR DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V. |
发明人 |
BECHERT, DIETRICH, DR.-ING. |
分类号 |
F01D5/14;F04D29/18;F04D29/30;F04D29/32;F04D29/54;F04D29/68 |
主分类号 |
F01D5/14 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|