| 发明名称 | Gas turbine engine with attached nosecone | ||
| 摘要 | A gas turbine engine includes a compressor section and a nosecone assembly. The compressor section includes an inlet guide vane assembly including an inner shroud, an outer shroud, and an inlet guide vane extending from the inner shroud to the outer shroud. The nosecone assembly is attached to the inner shroud. | ||
| 申请公布号 | US9540939(B2) | 申请公布日期 | 2017.01.10 |
| 申请号 | US201314141055 | 申请日期 | 2013.12.26 |
| 申请人 | United Technologies Corporation | 发明人 | Maliniak David;Monahan Daniel J.;Little Jonathan D.;Mayachari Veerachari J.;Dumavath Rakesh Sharma N.;Jayasingh Arun Kumar;Walker Herbert L. |
| 分类号 | F02C7/04;F01D9/04;F01D25/24 | 主分类号 | F02C7/04 |
| 代理机构 | Kinney & Lange, P.A. | 代理人 | Kinney & Lange, P.A. |
| 主权项 | 1. A gas turbine engine comprising: a compressor section comprising: an inlet guide vane assembly comprising: an inner shroud;an outer shroud; andan inlet guide vane extending from the inner shroud to the outer shroud; and a nosecone assembly attached to the inner shroud, wherein the nosecone assembly comprises: a nosecone; anda nosecone support ring connected to an aft end of the nosecone, wherein a first set of bolts extend substantially radially to connect the nosecone to the nosecone support ring, and wherein a second set of bolts extend substantially axially to connect the nosecone support ring to the inner shroud. | ||
| 地址 | Farmington CT US | ||