HIGH combustion annular chamber with the temperature in the combustion zone 1700ºS

摘要

Combustion chamber of a gas turbine installation ring type with bunk front device and 76 of the vortex burner is required parameters of volume of the flame tube, the diffuser length, the length of the combustion zone, the length of the gas plenum and the corresponding angle of inclination to the chamber axis to the motor axis, which provide the combustion temperature of air-fuel mixture of at least 1700 ° C in the combustion zone.