FIELD: engines and pumps.
SUBSTANCE: invention relates to aircraft engineering, namely to noise quieting devices. The proposed device incorporates a casing, a perforated passage wall and rectangular tubular composite-fibrous fillers attached thereto. The previously mentioned tubular fillers fibrous material layers are crossed and arranged in the lateral walls at the angle of 60 to 80 degrees to the said perforated passage wall. The crossed layers of fibrous material are arranged overlapped.
EFFECT: higher reliability of noise quieting device resulted from increased bearing capacity of tubular filler side walls.
2 cl, 2 dwg
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Authors
Dates
2009-02-10—Published
2007-09-10—Filed