FIELD: manufacturing technology.
SUBSTANCE: invention relates to production of fiber-metal composites and relates to aircraft panel made from multilayer composites and method of its production. Interconnected multilayer composites comprise laid first and second metal layers and fibro-reinforced layers of adhesive between adjacent metal layers. Filler is arranged at the transition from the outer surface of the first outer metal layer to the outer surface of the second outer metal layer. Panel additionally contains a plating layer, which contains at least one layer of fibrous material, which extends over the surface of the filler and adjacent areas of the external surface of external metal layers located on opposite sides, and which is glued to areas of the external surface.
EFFECT: invention provides higher efficiency of aircraft panel manufacturing.
25 cl, 11 dwg
| Title | Year | Author | Number |
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| METHOD FOR MANUFACTURE OF MULTILAYER CONSTRUCTION AND PRINTED CIRCUIT BOARD SUBSTRATE BASED ON MULTILAYER CONSTRUCTION | 1995 |
|
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| THIN-LAYER LAMINATES | 2005 |
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| CONDUCTING FACING MATERIAL FOR COMPOSITE STRUCTURES | 2013 |
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| SURFACING FILM FOR COMPOSITE STRUCTURES AND METHOD OF MAKING SAME | 2012 |
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|
RU2725456C1 |
| PERFECTED COMPOSITES | 2009 |
|
RU2496645C2 |
