Abstract: An engine consisting of an open Brayton cycle gas turbine mechanically as well as thermodynamically integrated with a closed cycle Rankine turbine engine is disclosed. The engine heat exchangers, including Rankine vapor generator, regenerator and condenser, are of annular configuration and are concentric with the axis of rotation of the turbomachinery components. A cooling fan is mounted coaxially with the condenser for improved cooling effectiveness. The engine components also are balanced around the gearbox for improved installation and use.

Abstract: A method and apparatus for improving the efficiency of a compressor of a gas turbine engine is disclosed. The inlet gas entering the compressor is stratified into two portions of different temperatures. The higher temperature gas is introduced adjacent the outer tips of the compressor blades to reduce the relative Mach number of the flow at that area.