| 发明名称 |
TURBINE ENGINE WITH A TURBO-COMPRESSOR |
| 摘要 |
A turbine engine is provided that includes a turbo-compressor, a combustor section, a flow path and a recuperator. The turbo-compressor includes a compressor section and a turbine section. The combustor section includes a combustor and a plenum adjacent the combustor. The flow path extends through the compressor section, the combustor section and the turbine section. The recuperator is configured with the flowpath between the combustor section and the turbine section. An inlet duct to the recuperator is fluidly coupled with the flow path upstream of the plenum. An outlet duct from the recuperator is fluidly coupled with the plenum. |
| 申请公布号 |
US2016237894(A1) |
申请公布日期 |
2016.08.18 |
| 申请号 |
US201514622523 |
申请日期 |
2015.02.13 |
| 申请人 |
United Technologies Corporation |
发明人 |
Kupratis Daniel B.;Sheridan William G. |
| 分类号 |
F02C3/34;F02K3/115;F02C3/14 |
主分类号 |
F02C3/34 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A turbine engine, comprising:
a turbo-compressor including a compressor section and a turbine section; a combustor section including a combustor and a plenum adjacent the combustor; a flow path extending through the compressor section, the combustor section and the turbine section; and a recuperator configured with the flowpath between the combustor section and the turbine section, wherein an inlet duct to the recuperator is fluidly coupled with the flow path upstream of the plenum, and an outlet duct from the recuperator is fluidly coupled with the plenum. |
| 地址 |
Hartford CT US |
