FIELD: process engineering.
SUBSTANCE: invention relates to aircraft and space engineering, namely, to canting elements of aircraft engine sound absorbing three-layer panels Proposed panel comprises cellular filler arranged between top and bottom skins. Canting element comprises inner layer adjoining said cellular filler and jointed therewith to outer layer canting three-layer and jointed with inner layer via foamed glue composition. Inner layer is jointed with cellular filler by glue film. Canting element inner layer width is smaller than cellular filler height.
EFFECT: lower labour input.
3 dwg
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