FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to undercarriage module protective panel. Said protective panel is mounted with the help of deformable parts on the support connected with aircraft airframe. Protective panel outer surface comprises composite material. Deformable parts interact with several stringers fitted at the frames. Extent of deformation of deformable parts is adapted to elongation at outer surface fracture to make several deformable parts deformed before fracture of said outer surface.
EFFECT: decreased weight of protective panel and higher impact strength.
14 cl, 4 dwg
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