FIELD: chemistry.
SUBSTANCE: invention refers to laminate composites used in aviation and machine industry and concerns a method for glass laminate aluminium reinforced epoxy junction. The method involves placing at least two metal layers each of which consists of separate edge-jointed sheets and glass reinforced plastics in between. Each of the sheet joints of the adjoining metal layers is half-size displaced in relation to each other. At least two layers of prepreg with differently oriented fibres are placed between the metal layers.
EFFECT: invention provides higher uniformity of strength characteristics throughout the related product.
3 cl, 2 dwg, 2 ex
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Authors
Dates
2015-12-10—Published
2014-09-10—Filed