DEVICE FOR GAS-TURBINE ENGINE OF AIRCRAFT FOR OPERATION AT MODES OF START-LANDING CYCLE

摘要

A device for gas-turbine engine of aircraft for operation at modes of start-landing cycle has condenser of combustion products connected by cooling side at inlet to atmosphere, and at outlet - to compressor, and at heating - to heat exchange unit and tank for collection of condensed moisture connected at inlet to condenser and at outlet - to fuel tank. Tank for fuel mixing with water is connected to fuel tank, tank with water and heat exchange unit heating surfaces of which through branch pipe are connected to turbine. To condenser fuel-water mix is supplied, this is discharged through piston compressor connected through crank mechanism to brake system of aircraft and connected at inlet to heat exchange unit, and at outlet - to reactor connected at inlet to piston compressor, and at outlet - to tank for keeping converted fuel.