Dual pressure turbine

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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60/155

F01D 1/02 (2006.01) F01K 23/06 (2006.01) F02G 5/04 (2006.01)

Patent

CA 1251052

-22- ABSTRACT A DUAL PRESSURE TURBINE A first stage of a dual pressure turbine receives superheated gas and directs the gas at a supersonic velocity against the blades of the rotor. The gas exiting the first stage and superheated gas at a lower preselected temperature are controllably and substantially separately directed to a second stage at substantially the same velocity. The dual pressure turbine effectively utilizes the superheated gases to produce useful work at a high system efficiency.

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