首页> 外国专利> AIRCRAFT WITH SUPER HIGH ASPECT RATIO BASED ON SELF-UNFOLDING FOLDING WING TECHNOLOGY

AIRCRAFT WITH SUPER HIGH ASPECT RATIO BASED ON SELF-UNFOLDING FOLDING WING TECHNOLOGY

机译:基于自折叠折翼技术的超高纵横比飞机

摘要

Disclosed is an aircraft with a super high aspect ratio based on self-unfolding folding wing technology, the aircraft including: an aircraft body; a fixed wing; and a movable wing assembly including a first movable wing and a second movable wing. When the aircraft takes off, the first movable wing and the second movable wing are in a folded position. The first movable wing and the second movable wing are deflected and moved to an unfolded position or a folded position by the aerodynamic force and moment generated by the deflection of aerodynamic control surfaces and the differential thrust and moment generated by a distributed propulsion system.
机译:公开了一种基于自展开折叠翼技术的超高长宽比的飞机,该飞机包括:机身;固定翼动翼组件包括第一动翼和第二动翼。当飞机起飞时,第一可动翼和第二可动翼处于折叠位置。第一活动翼和第二活动翼通过由气动控制面的偏转产生的气动力和力矩以及由分布式推进系统产生的差推力和力矩而偏转并移动到展开位置或折叠位置。

著录项

  • 公开/公告号US2020269967A1

    专利类型

  • 公开/公告日2020-08-27

    原文格式PDF

  • 申请/专利权人 TSINGHUA UNIVERSITY;

    申请/专利号US201716492126

  • 发明设计人 HAIXIN CHEN;XIAOPENG ZHOU;

    申请日2017-07-13

  • 分类号B64C3/54;B64C39/08;B64C3/32;B64C9;B64C13/40;B64C13/50;

  • 国家 US

  • 入库时间 2022-08-21 11:23:36

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