AIR COOLING APPARUSTUS FOR GAS TURBINE

摘要

PURPOSE: An intake cooling apparatus for a gas turbine is provided to cold air which passes through an evaporator of an adsorption refrigerator by installing the adsorption refrigerator in an air compressor of a gas turbine. CONSTITUTION: An intake cooling apparatus for a gas turbine comprises an air cooling unit(110), a cold air generation unit(120), and a drive unit(130). The air cooling unit is installed on the inlet of a gas turbine(1) and colds the air inhaled to the gas turbine. The cold air generation unit is connected to the air cooling unit and transfers the cold air to the air cooling unit. The drive unit is connected to the cold air generation unit and operates the cold air generation unit. The drive unit operates the cold air generation unit using the solar energy.