发明名称 |
Integrated Flex Support and Front Center Body |
摘要 |
A gas turbine engine is provided. The gas turbine engine may include a geared architecture, a central body support and a bearing package. The geared architecture may interconnect a spool and a fan rotatable about an axis. The central body support may provide an annular wall for a core flow path and an integral flex support inwardly extending therefrom. The integral flex support may couple the geared architecture to the central body support. The bearing package may include a bearing support removably coupled to the integral flex support. |
申请公布号 |
US2016003105(A1) |
申请公布日期 |
2016.01.07 |
申请号 |
US201414765680 |
申请日期 |
2014.03.14 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Cigal Brian P.;Davis Todd A. |
分类号 |
F01D25/28;F01D25/04;F01D25/18;F01D25/16 |
主分类号 |
F01D25/28 |
代理机构 |
|
代理人 |
|
主权项 |
1. A gas turbine engine, comprising:
a geared architecture interconnecting a spool and a fan rotatable about an axis; a central body support providing an annular wall for a core flow path and an integral flex support inwardly extending therefrom, the integral flex support coupling the geared architecture to the central body support; and a bearing package having a bearing support removably coupled to the integral flex support. |
地址 |
Hartford CT US |