Regenerative gas turbine cycle

Power plants – Combustion products used as motive fluid

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60 3953, F02C 700

Patent

active

045370230

ABSTRACT:
In a regenerative gas turbine cycle in which heat recovery is carried out by a mixture of air/steam which is obtained by contact between water and a part of or the whole of compressed air, said compressed air being compressed by a compressor for compressing gas using air or air based gas as a combustion supporting/working medium gas; the improvement comprising: the mixture of air/steam and liquid phase cooled water being obtained through the contact between the compressed air and heated water which is used as heat recovering medium; said cooled water being used as heat recovering medium not only for heat recovery of turbine exhaust gas but also, for

REFERENCES:
patent: 2115338 (1938-04-01), Lysholm
patent: 2186706 (1940-01-01), Martinka
patent: 2602289 (1952-07-01), Anxionnaz et al.
patent: 3379009 (1968-04-01), Sharp et al.
patent: 3877218 (1975-04-01), Nebgen
patent: 4418527 (1983-12-01), Schlom et al.
Zucrow, M. J., Aircraft and Missile Propulsion, New York, Wiley & Sons, 1958, pp. 24, 26.

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