| 发明名称 | Turbomachine geared architecture support assembly | ||
| 摘要 | An example turbomachine geared architecture support assembly includes a subpart having a more compliant portion and a less compliant portion. The less compliant portion includes a stop that limits axial movement of a geared architecture within a turbomachine. | ||
| 申请公布号 | US9017010(B2) | 申请公布日期 | 2015.04.28 |
| 申请号 | US201213362389 | 申请日期 | 2012.01.31 |
| 申请人 | United Technologies Corporation | 发明人 | Otto John R. |
| 分类号 | F16H57/08;F02C7/20;F01D21/04;F01D25/16;F02C3/107;F02C7/36 | 主分类号 | F16H57/08 |
| 代理机构 | Carlson, Gaskey & Olds, P.C. | 代理人 | Carlson, Gaskey & Olds, P.C. |
| 主权项 | 1. A turbomachine geared architecture support assembly, comprising: a support having a more compliant portion and a less compliant portion, wherein the less compliant portion includes a stop that limits axial movement of a geared architecture within a turbomachine, the stop configured to be spaced from a rigid member during normal operation of a turbomachine that includes the geared architecture, the stop further configured to contact the rigid member during abnormal operation of the turbomachine to limit the axial movement. | ||
| 地址 | Hartford CT US | ||