公开(公告)号：US20150008285A1

公开(公告)日：2015-01-08

申请号：US14491251

申请日：2014-09-19

Applicant: AIRBUS OPERATIONS GMBH

Inventor： M. Ichwan Zuardy ,  Karim Grase ,  Carsten Rowedder ,  Claas DeJong ,  Markus Mueller ,  Mathias Jessrang

IPC: B64C1/10

CPC classification number: B64C1/10

Abstract: A pressure bulkhead of an aircraft with a fuselage shell and a pressure bulkhead disposed therein preferably in the rear region for forming a fuselage-internal pressure region, which pressure bulkhead is attached on the edge in the interior of the fuselage shell, wherein the pressure bulkhead has a lenticular cross-section and a sandwich construction that comprises a foam core sandwiched between two opposing exterior shells.

Abstract translation: 具有机身壳体和压力舱壁的飞机的压力舱壁优选地设置在后部区域中，用于形成机身内部压力区域，该压力舱壁附接在机身壳体内部的边缘上，其中压力舱壁 具有透镜状横截面和夹层结构，其包括夹在两个相对的外壳之间的泡沫芯。