FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to jointing aircraft two fibrous composite parts. Proposed method comprises the following stages: a) making first fibrous composite part 1. Note here that seat surface 2 may be offset from tolerances, b) making tool holder 7 to fit in surface shape 2, c) making second fibrous composite part 3 with the help of tool holder 7. Note here that shape of contact surface 9 of second part 3 matches mainly with seat surface 2. d) It includes also jointing first fibrous composite part 1 and second fibrous composite part 3 in the zone of mount surface 2 and contact surface 9.
EFFECT: simple and reliable joint.
8 cl, 1 dwg
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