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