FIELD: transport.
SUBSTANCE: invention relates to methods of producing aircraft component assembly first part and to aircraft structure components. In compliance with first version, proposed method comprises arranging first surface of the first part in the zone of second part second surface, inserting solid shim into the gap between first and second surfaces, retaining solid shim in inserted position and inserting liquid lining via first part into area between first part and solid shim. In compliance with second version, proposed comprises arranging solid shim in the zone of first part first surface, feeding liquid lining in the area between first part and solid shim, and jointing first part with extra part by solid shim. Solid shim is secured on first part first surface by means of liquid lining between solid shim and first part first surface and solid shim arranged adjoining extra part. Aircraft structure component comprises first part with first surface, solid shim secured on first surface, and hardening liquid lining arranged between solid shim and first surface. First part has through channel that extends from first surface. Part of hardening liquid lining is arranged in said channel.
EFFECT: simplified assembly of aircraft structure component two parts.
15 cl, 8 dwg
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Authors
Dates
2011-02-10—Published
2006-12-14—Filed