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Space-efficient stowable, automatically operated, compressible aircraft wing

机译:节省空间的可收起,自动操作的可压缩飞机机翼

摘要

Automated combination of closely-knit telescopic wing surface shells or accordion-like wing surface skin and / or ribs, on the one hand, with an unsegmented wing spar or wing spars, on the other hand, said components can be stowed in a space-efficient manner predominantly within the top view of an aircraft fuselage, said spar or spars are predominantly parallel from a stowed position can be pivoted towards the fuselage to an operational position ready for flight, predominantly transversely to the fuselage, and said closely combined surfaces and ribs can be extended and are combined with said spar in such a way that they together form an aerodynamic wing.
机译:一方面,紧密编织的可伸缩机翼表面壳体或类似手风琴的机翼表面蒙皮和/或肋骨与不分段的翼梁或翼梁自动组合,另一方面,可以将这些组件存放在以下空间中:主要在飞机机身的顶视图内的有效方式,所述翼梁或翼梁主要从收起位置平行,可以朝向机身枢转到准备飞行的操作位置,主要横向于机身,并且所述紧密结合的表面和肋骨所述翼梁可以被延伸并与所述翼梁组合,使得它们一起形成空气动力学翼。

著录项

  • 公开/公告号DE112018006890T5

    专利类型

  • 公开/公告日2020-10-01

    原文格式PDF

  • 申请/专利权人 FLECK FUTURE CONCEPTS GMBH;

    申请/专利号DE20181106890T

  • 发明设计人 JOHN BROWN;

    申请日2018-01-18

  • 分类号B64C3/56;

  • 国家 DE

  • 入库时间 2022-08-21 11:01:33

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