| 摘要 |
A method enables a gas turbine engine positioned within a module to be operated. The engine includes an inlet and an exhaust, and the module includes an inlet area, an exhaust area, and an engine area extending therebetween and housing the engine. The exhaust area includes an exhaust duct and an outlet. The engine is operated such that inlet air is routed through the module inlet and into the engine inlet, wherein exhaust gases are discharged through the module exhaust duct and substantially perpendicularly from the gas turbine engine. The exhaust gases are discharged from the module outlet in a direction that is at least ninety degrees offset from exhaust gases flowing within the exhaust duct. Cooling fluid is discharged from the module engine area through a cooling system exhaust, such that the discharged fluid flows through the cooling system exhaust and around the module exhaust area.
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