F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 6/00 (2006.01) F02C 3/02 (2006.01)
Patent
CA 2101287
ABSTRACT OF THE DISCLOSURE Method of operating a gas turbine installation and an application of the method In a gas turbine installation, compressed air is supplied from a compressor to a pressure wave machine. The compressed air is at least partially enriched with fuel. The air which is compressed and enriched with fuel is ignited and burned. The gas resulting from the combustion is supplied to a multi-stage turbine with a low pressure part and a high pressure part. Layers of the compressed air are differently enriched with fuel so that, for example, a layer with a rich fuel/air mixture, a layer with a weak fuel/air mixture and a layer of pure air occur. After combustion, all the layers are expanded to the same temperature and supplied to the multi-stage turbine. (Fig.1))
Asea Brown Boveri Ltd.
Swabey Ogilvy Renault
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