| 摘要 |
PURPOSE:To attempt reduction of heat loss by supplying drain in exhaust gas to an exhaust heat recovering device and an intermediate air cooler, and after that, by supplying it to a combustor. CONSTITUTION:An exhaust heat recovering device 12 and an exhaust gas condenser 14 are provided in an exhaust system of a gas turbine 10. The recovered drain is supplied to the exhaust gas recovering device 12 and an intermediate air cooler 3, and after that, supplied to a combustor 6 through a spray line 8. Heat loss from exhaust gas can thus be reduced.
|
