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PRESSURE FUSELAGE OF AN AIRCRAFT WITH A FUSELAGE SHELL AND A PRESSURE BULKHEAD DISPOSED THEREIN

机译:带有机身壳的飞机的压力机身及其上布置的压力块头

摘要

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.
机译:具有机身壳体和设置在其中的压力隔板的飞机的压力隔板,优选地在后部区域中用于形成机身内部压力区域,该压力隔板附接在机身壳体内部的边缘上,其中,压力隔板具有双凸透镜的横截面和夹心结构,该结构包括夹在两个相对的外壳之间的泡沫芯。

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