FIELD: instrument making.
SUBSTANCE: invention relates to mechanical component assembly (1) for aircraft containing part (3) containing connected end; recess intended for fitting part (3), wherein said cavity (2) has wall with composite material with organic matrix; fixing composite material (4) containing a thermoplastic or thermosetting material with content of filler from 0 to 70 wt% and forming a mechanical and/or physical-chemical bond between said part (3) and socket (2) with a wall made from composite material with an organic matrix.
EFFECT: achieving reduced weight, reduced production costs, simple and less costly repair, production of finished parts without any reworking after moulding.
15 cl, 2 dwg
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