METHOD OF CONTINUOUS OPERATION GAS TURBINE PLANT ACTION Russian patent published in 2016 - IPC F02C3/20 B82Y30/00 

FIELD: devices for fuel combustion.

SUBSTANCE: invention can be used in stationary gas turbine units in fuel combustion chamber. Method of continuous action gas turbine unit operation consists of air compression supplied to compressor, compressed air and fuel supply into first combustion chamber, fuel combustion in first combustion chamber, expansion of combustion products formed in first turbine, use of at least part of mechanical energy generated by first turbine for compressor drive, subsequent supply of expanded fuel combustion products and fuel into second combustion chamber and expansion of combustion products formed in second turbine for generation of mechanical energy. Fuel supplied to second combustion chamber is not oxidized aluminium nanoparticles, which radius is not more than 25 nm. At second turbine output formation of corona discharge for combustion products processing is provided. Processed combustion products are directed to electrostatic filter for formed corundum particles separation, which is additional product produced by gas-turbine plant, and directed at least part of combustion products, passed through electrostatic filter, to first combustion chamber, where they are used as additional fuel. For protection against oxidation supply of aluminium nanoparticles to second combustion chamber is performed in nitrogen medium.

EFFECT: technical result consists in improvement of plant efficiency.

1 cl, 2 dwg