Single shaft gas turbine engine with radial exhaust diffuser

Power plants – Combustion products used as motive fluid – With exhaust treatment

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F02C 710

Patent

active

041776380

ABSTRACT:
A compact single shaft gas turbine engine includes a radial compressor and a radial turbine mounted for rotation about a central axis and an axially inline disk regenerator disposed forward of the turbine. A highly efficient engine configuration minimizes energy loss along an improved gas flow path while permitting the engine to be mounted on a standard 22 inch wide farming tractor frame. Efficiency is further increased by a radial exhaust diffuser disposed between the regenerator and turbine which does not contribute substantially to engine size.

REFERENCES:
patent: 3276515 (1966-10-01), Whitfield

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