| 发明名称 |
GAS TURBINE EXHAUST DIFFUSER |
| 摘要 |
A gas turbine exhaust diffuser includes a frustoconical portion that defines an interior surface and an axial centerline. In particular embodiments, the interior surface may have a slope greater than 6 degrees, 10 degrees, or 20 degrees with respect to the axial centerline to define an axial cross-sectional area of at least 200 square feet, 240 square feet, or 260 square feet. In other particular embodiments, the interior surface may have an axial length of less than 25 feet or less than 10 feet. A helical turbulator on the interior surface of the frustoconical portion may reduce flow separation between exhaust gases and the interior surface to enhance recovery of potential energy from the exhaust gases. |
| 申请公布号 |
US2014298771(A1) |
申请公布日期 |
2014.10.09 |
| 申请号 |
US201313855907 |
申请日期 |
2013.04.03 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
Zhang Hua;Byrd Douglas Scott;Merchant Laxmikant;Ponyavin Valery Ivanovich |
| 分类号 |
F01D25/30 |
主分类号 |
F01D25/30 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine exhaust diffuser, comprising:
a. a frustoconical portion that defines an interior surface and an axial centerline; b. a helical turbulator on the interior surface of the frustoconical portion; and c. wherein the interior surface has a slope greater than 6 degrees with respect to the axial centerline. |
| 地址 |
Schenectady NY US |
