AFTERBURNER MIXER OF BYPASS OF BYPASS TURBO-JET ENGINE

摘要

FIELD: aircraft engines. SUBSTANCE: mixer of afterburner of bypass turbo-jet engine has corrugations forming alternating channels of internal and external ducts. Trailing edges of corrugations are inclined to longitudinal axis of mixer at different angles; angle of inclination of each subsequent edge of corrugation differs from previous one by 4 to 90 deg. EFFECT: enhanced stability to vibratory combustion. 3 dwge