GAS TURBINE ENGINE FUEL COMBUSTION SYSTEM

摘要

FIELD: engines and pumps.SUBSTANCE: proposed system comprises at least one resonator arranged at fuel combustion system wall confining channel of hot and pressurised combustion gaseous products flow. Resonator volume is confined by walls, one adjoining fuel combustion system wall or being composed thereof. Resonator has narrow connection slot open towards fluid flow channel and at least one cooling fluid feed hole open towards coolant source. Only one narrow connection slot of resonator is located in the way of fluid flow.EFFECT: high-efficiency fuel combustion system.16 cl, 7 dwg