Gas turbine arrangement

Details Gas turbine arrangement Gas turbine arrangement

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 3/02 (2006.01) F02C 3/10 (2006.01) F02C 3/14 (2006.01) F02C 6/02 (2006.01)

Patent

CA 2049852

90/071 ABSTRACT OF THE DISCLOSURE 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. (Fig. 1)

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