Door surrounding arrangement for aircraft fuselage structure, has door surrounding structure integrally or partially integrally designed and including connecting surface, which is connectable with support surface of fuselage skin

摘要

The arrangement has reinforcement elements e.g. stringers (6) and bulkheads (8), associated to a fuselage skin (4), and a door surrounding structure (10a) integrally or partially integrally designed and including a connecting surface (16) facing toward a fuselage skin. The connecting surface is connectable with a support surface (18) of the fuselage skin. The door surrounding structure exhibits a door surrounding frame (20) dividingly provided in a circumferential direction of a fuselage structure, which is connectable in a region of a center section (14) of a door cutout (12).