| 摘要 |
A gas turbine engine includes a first stage compressor, an intercooler in fluid communication with the first stage compressor, and a second stage compressor in fluid communication with the intercooler. The engine also includes a combustor in fluid communication with the second stage compressor and a turbine in fluid communication with the combustor. The intercooler cools an air inflow from the first stage compressor and the recuperator heats the airflow traveling from the second stage compressor to the turbine exhaust. The intercooler and recuperator are arranged radially outward of the combustor. |
