FIELD: transport.
SUBSTANCE: invention relates to aircraft door frame, aircraft fuselage and aircraft with such door frame. Proposed door frame comprises door carcass wherein door is mounted. Said carcass comprises outer frame 60, inner frame 50 and rib 40 arranged between inner and outer frames. Rib 40 is made up of accordion-shape rigid bracing from composite material and consisting of set of inserts 70, V-shaped (70a) and inverted V-shaped (70b).
EFFECT: reduced weight.
10 cl, 7 dwg
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