Other

Doosan Heavy Industries & Construction Co., Ltd

Alexander Bograd

Borys Shershnyov

The gas turbine includes a compressor to compress air introduced thereinto, a combustor to mix the compressed air with fuel for combustion, a main turbine having a plurality of turbine blades rotated by an energy produced by combustion gas in the combustor, a heat recovery boiler to produce steam by heat exchange with the combustion gas, and a fluid accelerator supplied with a first fluid compressed in the compressor to compress the first fluid and supply the compressed first fluid to the combustor, where the fluid accelerator includes a first inlet through which the first fluid is introduced, a second inlet through which a second fluid having a higher pressure than the first fluid is introduced, and an outlet through which the first and second fluids are mixed and discharged.

Gas turbine and method of operating the same

Provided is a gas turbine including: a combustor positioned between a compressor and a turbine of a gas turbine; a cooling air discharge unit configured to receive compressed air from the compressor, receive cooling water from a power plant, and discharge cooling air having exchanged heat with the compressed air; and a supply unit configured to supply the cooling air discharged from the cooling air discharge unit to the turbine and the combustor.

Growing community of inventors

Changwon-si, South Korea

Alexander Bograd