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AIRCRAFT WINGS WITH REDUCED WINGSPAN

机译:飞机翅膀减少翅膀牌

摘要

An aircraft wing device having one or more numbered wing sets, each wing set further comprising: one or more internal wings, one or more external wings and a transition unit. The internal wings are used to structurally connect the wing set with the main aircraft body, and the external wings are capable of being positionally adjusted and maneuvered by way of vertical, horizontal, or angular movement. The device not only reduces the wingspan of the traditionally used aircraft wings, but also provides better stability and reduces the takeoff time. The wing sets may be positionally staggered on the aircraft body, height wise for aerodynamics efficiency and lift efficiency.
机译:具有一个或多个编号翼组的飞机翼装置,每个机翼设置还包括:一个或多个内部翼,一个或多个外部翼和过渡单元。 内部翼用于在结构上将翼组与主飞机主体连接,外部翼能够通过垂直,水平或角运动来定位和操纵。 该装置不仅减少了传统使用的飞机翼的翅膀,而且还提供更好的稳定性并减少起飞时间。 机翼组可以在飞机体上定位交错,高度明智的空气动力学效率和提升效率。

著录项

  • 公开/公告号US2021253248A1

    专利类型

  • 公开/公告日2021-08-19

    原文格式PDF

  • 申请/专利权人 SAMIR HANNA SAFAR;

    申请/专利号US202117169364

  • 发明设计人 SAMIR HANNA SAFAR;

    申请日2021-02-05

  • 分类号B64C39/08;B64C3/38;B64D27/18;B64C3/32;

  • 国家 US

  • 入库时间 2022-08-24 20:41:53

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