| 摘要 |
Aircraft comprising at least one door (14, 16 P1) for passengers to board the aircraft, characterized in that it comprises at least one interconnection device (20; 40; 50; 60; 70) connecting an aircraft internal structure component (24) and a skin of the fuselage (22) of the aircraft, the interconnection device being positioned near the internal periphery of the door in a region (Z1) subject to external knocks and comprising at least one region that is weakened in terms of compression (26c; 42a; 42b; 62b; 62c; 62d; 72b; 74b) so as to absorb the knocks experienced by the external face of the skin of the fuselage, the device also being configured to withstand tensile forces applies to the internal face of the skin of the fuselage by the internal pressure inside the aircraft. |
