Jet engine noise reduction system

Power plants – Reaction motor – Air passage bypasses combustion chamber

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Details

60271, 181213, 415119, F01N 124, F02K 104

Patent

active

050604716

ABSTRACT:
A noise reduction system for a jet engine including a tubular exhaust shroud affixed to the engine through which engine exhaust gases pass, porous acoustical lining affixed to a substantial portion of the internal circumferential surface of the shroud, a chamber in contact with the acoustical lining outer surface and a controllable source of air pressure affixed to the chamber to control the passage of air through the acoustical lining to thereby vary the acoustical absorption properties of the lining.

REFERENCES:
patent: 3262264 (1966-07-01), Gardiner et al.
patent: 3750402 (1973-08-01), Vdoviak et al.
patent: 4293053 (1981-10-01), Shuttleworth et al.
patent: 4433751 (1984-02-01), Bonneau
C. L. Arctander, C. G. Hodge; R. B. Tate; "Development of Noise-Reduction Concepts for 727 & 737 Airplanes"; Journal Acoustic Society America; vol. 58, No. 1, Jul. 1975.

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