发明名称 |
Turbomachine Blade Assembly |
摘要 |
Embodiments of the present disclosure include a system comprising a turbomachine blade assembly having a blade portion, a shank portion, and a mounting portion, wherein the blade portion, the shank portion, and the mounting portion comprise a first plurality of plies extending from a tip of the airfoil to a base of the dovetail. |
申请公布号 |
US2014301850(A1) |
申请公布日期 |
2014.10.09 |
申请号 |
US201313856303 |
申请日期 |
2013.04.03 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
Garcia Crespo Andres Jose |
分类号 |
F01D11/00;F01D5/30;F01D5/28 |
主分类号 |
F01D11/00 |
代理机构 |
|
代理人 |
|
主权项 |
1. A system, comprising:
a turbomachine blade assembly, comprising:
a blade portion;a shank portion; anda mounting portion,wherein the blade portion, the shank portion, and the mounting portion comprise a first plurality of plies extending from a tip of the blade portion to a base of the mounting portion. |
地址 |
Schenectady NY US |