发明名称 |
TURBOMACHINE BLADE TIP SHROUD WITH PARALLEL CASING CONFIGURATION |
摘要 |
Embodiments of the present disclosure include a turbomachine having a turbomachine blade and a stationary structural component. The turbomachine blade includes a tip shroud having a leading edge portion where the leading edge portion has a first surface. The stationary structural component is disposed about the turbomachine blade and includes a corresponding portion corresponding to the leading edge portion of the tip shroud, where the corresponding portion has a second surface, where the first surface and the second surface have generally parallel contours.
|
申请公布号 |
US2013272888(A1) |
申请公布日期 |
2013.10.17 |
申请号 |
US201213447134 |
申请日期 |
2012.04.13 |
申请人 |
CHOUHAN ROHIT;PIERRE SYLVAIN;SIDEN GUNNAR LEIF;VIJAYAN SANTHOSH KUMAR;COTRONEO JOSEPH ANTHONY;GENERAL ELECTRIC COMPANY |
发明人 |
CHOUHAN ROHIT;PIERRE SYLVAIN;SIDEN GUNNAR LEIF;VIJAYAN SANTHOSH KUMAR;COTRONEO JOSEPH ANTHONY |
分类号 |
F04D29/38 |
主分类号 |
F04D29/38 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|