Notch attenuation device

Acoustics – Auditorium

Patent

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Details

181 33HB, 244 1N, B64D 3306

Patent

active

039688534

ABSTRACT:
A method for the attenuation of the noise emitted by a main exhaust nozzle f a jet engine, wherein an auxiliary exhaust nozzle adapted to emit less noise than the main nozzle is associated with said main nozzle and is located to the side of the main nozzle, in the direction in which it is desired to attenuate the noise of the main nozzle.

REFERENCES:
patent: 3033494 (1962-05-01), Tyler et al.
patent: 3174282 (1965-03-01), Harrison
patent: 3706353 (1972-12-01), Ffowces-Williams et al.
patent: 3743185 (1973-07-01), Ffowces-Williams et al.

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