Gas turbine arrangement

Power plants – Combustion products used as motive fluid

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60 3945, F02C 0303

Patent

active

052823547

ABSTRACT:
This gas turbine arrangement has a gas turbine which can be divided into a high-pressure part and a basic part and has a compressor (1) and at least one energy exchanger (7). In addition, it has a combustion-chamber arrangement and a separate combustion chamber (18) connected upstream of the energy exchanger (7). The intention is to provide a gas turbine arrangement in which an increased efficiency is achieved by simple means and which can be regulated more simply. This is achieved by providing at least two combustion chambers (9, 10) for the combustion-chamber arrangement. The first (9) of the combustion chambers cooperates with the high-pressure part of the gas turbine arrangement. The second (10) of the combustion chambers cooperates, via the interposed energy exchanger (7) having the upstream combustion chamber (18), with the basic part.

REFERENCES:
patent: 2461186 (1949-02-01), Seippel
patent: 2738123 (1956-03-01), Hassmann
patent: 3398525 (1968-08-01), Jenny
patent: 4679393 (1987-07-01), Hellat et al.
patent: 4719746 (1988-01-01), Keller
International Search Report No. 90/071 EP, May 1991.

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