Jet engine with noise energy dissipation

Power plants – Internal combustion engine with treatment or handling of... – Material from exhaust structure fed to engine intake

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Details

23926519, 181213, F02K 100, B63H 1110, F01N 300

Patent

active

042200024

ABSTRACT:
Means to damp the transmission of gas vibration aft of the tailpipe from the high velocity exhaust gas to the relatively slow moving airstream surrounding the said tailpipe of a jet engine wherein a metallic fringe, due to the low resonant characteristics of slack fine wire, acts as a vibration damper when externally affixed and surrounding the terminus of the said tailpipe, with an additional vibration impediment comprising a miniature airfoil surrounding the said terminus while functioning as an air-pressure reducer wherein a low air-pressure area is interposed between the said exhaust gas and the said airstream.

REFERENCES:
patent: 2882991 (1959-04-01), Killian
patent: 2959917 (1960-11-01), McGehee
patent: 2984972 (1961-05-01), Davidson
patent: 3041218 (1962-06-01), Layton
patent: 3153319 (1964-10-01), Young et al.
patent: 3568792 (1971-03-01), Urquhart
patent: 3572464 (1971-03-01), MacDonald

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