Integrated flow turbine engine

Power plants – Combustion products used as motive fluid – With dual function turbine

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Details

415 56, F02C 304

Patent

active

040708241

ABSTRACT:
A gas turbine having a rotor serving as both compressor and turbine, and utilizing a plurality of non-rotating arcuate members disposed in spaced relation about the periphery of the rotor. These arcuate members are involved in the directing of the flow of combustion products into proximity of the blading of the turbine, to cause its rotation, and by virtue of their advantageous design, these arcuate members not only help establish a cool air boundary against which the combustion products react and thus minimize heating of the blades, but also form passages for the subsequent exhausting of the combustion products.

REFERENCES:
patent: 2537344 (1951-01-01), Gruss
patent: 2658338 (1953-11-01), Ledoc
patent: 3310940 (1967-03-01), Oetliker

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