AFTERBURNER MIXER OF BYPASS OF BYPASS TURBO-JET ENGINE Russian patent published in 1998 - IPC

Abstract RU 2117805 C1

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 dwg

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RU 2 117 805 C1

Authors

Andreev A.V.

Chepkin V.M.

Dates

1998-08-20—Published

1995-02-15—Filed