Jet mixer noise suppressor using acoustic feedback
AssigneeThe United States of America as represented by the Administrator of the National Aeronautics and Space Administration
InventorEdward J. Rice
Life of this patent
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Abstract
The present invention generally relates to providing an improved jet mixer noise suppressor for high speed jets that rapidly mixes high speed air flow with a lower speed air flow, and more particularly, relates to an improved jet mixer noise suppressor that uses feedback of acoustic waves produced by the interaction of sheer flow instability waves with an obstacle downstream of the jet nozzle.
Claims6
A jet mixer noise suppressor, comprising:
- a first nozzle outputting a first air stream generating feedback of a first acoustic wave from downstream of said first nozzle;
- a second nozzle outputting a second air stream, synchronous with said first air stream, generating feedback of a second acoustic wave from downstream of said second nozzle;
- and
- an ejector having an inlet, outlet and shroud, said ejector receiving said first and second air streams from said first and second nozzles through said inlet, receiving entrained air produced from said first and second air streams through said inlet, receiving said first and second acoustic waves fed back from downstream of said first and second nozzles through said outlet, and mixing said first and second air streams and said entrained air responsive to said first and second acoustic waves in said shroud,
- wherein said first and second nozzles are positioned so that said first and second acoustic waves are out of phase with each other.
A method of suppressing noise using a jet mixer noise suppressor, comprising the steps of:
- (a) outputting a first air stream using a first nozzle, generating feedback of a first acoustic wave from downstream of the first nozzle thereby producing a first mixing process;
- (b) outputting a second air stream using a second nozzle, synchronous with the first air stream, generating feedback of a second acoustic wave from downstream of the second nozzle, thereby producing a second mixing process;
- (c) receiving the first and second air streams from the first and second nozzles through an ejector inlet;
- (d) receiving entrained air produced from the first and second air streams through the ejector inlet;
- (e) propagating acoustic waves from the first and second mixing processes downstream of the first and second nozzles through an ejector outlet;
- and
- (f) mixing the first and second air streams and the entrained air responsive to the first and second acoustic waves in an ejector shroud,
- wherein the first and second nozzles are positioned so that the first and second acoustic waves are out of phase with each other.
A method as set forth in claim 7,
- wherein said mixing step (f) generates instability waves which mixes the first and second air streams and the entrained air, and
- wherein the first and second nozzle includes' a bevelled outlet lip propagating the acoustic wave pattern substantially parallel to the bevelled outlet lip.
Dependencies are inferred from the claim text.