Vortex mixers for reducing the noise emitted by jet engines

Power plants – Reaction motor – Air passage bypasses combustion chamber

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181219, F02K 302

Patent

active

042177561

ABSTRACT:
Apparatus for internally mixing fan exhaust with primary exhaust forward of the nozzle exit plane of a turbofan engine having an outer engine cowling, a splitter wall structure and a tail plug disposed in mid engine upstream of the nozzle exit plane is provided by a plurality of struts disposed radially between the engine tail plug and the outer engine cowling upstream of the nozzle exit plane and a plurality of vortex generating means disposed on the struts for generating vorticies across the entire engine exhaust area.

REFERENCES:
patent: 2443250 (1948-06-01), Johnson
patent: 2880574 (1959-04-01), Howald
patent: 2935847 (1960-05-01), Markowski
patent: 3100627 (1963-08-01), Wilde
patent: 3647020 (1972-03-01), MacDonald
patent: 3655009 (1972-04-01), Hilbig
patent: 3737005 (1973-06-01), Tontini
patent: 3776363 (1973-12-01), Kuethe

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