公开(公告)号：US20240017813A1

公开(公告)日：2024-01-18

申请号：US18351865

申请日：2023-07-13

申请人： AIRBUS OPERATIONS, S.L.U.

发明人： Israel VILLAFRANCA DÍAZ ,  Rafael DE LA TORRE SAN JOSÉ

IPC分类号： B64C1/10

CPC分类号： B64C1/10

摘要： A section of fuselage for an aircraft including: a pressure bulkhead comprising a dome-shaped structure and at least one coupling structure extending from the edge of the dome-shaped structure, and at least one circumferential structure arranged on a skin of the section of fuselage, wherein the dome-shaped structure is secured to the circumferential structure via a distal portion of the coupling structure, wherein said distal portion is coupled to a foot portion of the circumferential structure, the coupling structure extending obliquely from the foot portion of the circumferential structure, such that the distance between a skin of the section of fuselage and the coupling structure increases from the foot portion to the edge of the dome-shaped structure.