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Folding pressure bulkhead for aircraft, and aircraft provided with such a pressure bulkhead

机译:飞机的折叠式压力舱壁以及具有这种压力舱壁的飞机

摘要

the invention relates to a pressure bulkhead for an aircraft (3), having a first side intended to be subjected to a relatively high pressure and a second side intended to be subjected to a relatively low pressure, the pressure bulkhead with pockets in connection to the rigid structure of the aircraft, the partition (3) is formed of a flexible material.for folding when not assembly to the rigid structure of the aircraft.according to the invention, the flexible material is a shape memory material, which, when the connecting areas are attached to the rigid structure of the aircraft, the maintenance of the partition (3) into a position of use,essentially the same when the pressure in the first and second side are balanced, and when the pressure applied to the first surface is greater than the pressure on the second side to a value less than one, and three bars.
机译:用于飞机(3)的压力舱壁技术领域本发明涉及一种用于飞机(3)的压力舱壁,该压力舱壁的第一侧旨在承受相对较高的压力,第二侧旨在承受相对较低的压力,该压力舱壁具有与容器连接的凹穴。隔板(3)是飞机的刚性结构,隔板(3)由柔性材料制成。用于在未组装到飞机的刚性结构时折叠。根据本发明,柔性材料是形状记忆材料,当连接时将区域固定在飞机的刚性结构上,将隔板(3)的维护位置保持在使用位置,当第一侧和第二侧的压力达到平衡且施加到第一表面的压力为大于第二侧的压力,使其小于一和三巴。

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