Jet engine noise suppressor assembly

Aeronautics and astronautics – Miscellaneous

Patent

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Details

244 73R, 23926517, 602261, B64D 3304

Patent

active

059474122

ABSTRACT:
The present invention relates to a noise supressor assembly for a jet engine comprised of a plurality of conduit assemblies proximate the trailing edges of the wall members which capture a portion of an ambient gaseous stream flowing in an ambient flow for introduction into the hot core gaseous flow to thereby deform the interface between the hot core flow and the fan flow or ambient flow when there is no fan between the fan flow and the ambient flow or between fully or partially mixed core and fan flows and the ambient flow thereby mixing such gaseous streams to thereby reduce velocity of the hot core and fan flows and thus jet noise level.

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patent: 5269139 (1993-12-01), Klees
patent: 5440875 (1995-08-01), Torkelson et al.
patent: 5638675 (1997-06-01), Zysman et al.
patent: 5722233 (1998-03-01), Nikkanen et al.

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