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FLYING WING TYPE AIRCRAFT

机译:飞翼式飞机

摘要

FIELD: aviation. ;SUBSTANCE: aircraft of the aerodynamic design of the flying wing contains a wing of a thick profile designed for flight, having longitudinal and transverse axes, forming a configuration for flying at a subsonic speed and a configuration for flying at a hypersonic speed, engines and controls. The wing is made with the ability to fly at a subsonic speed in the direction of the transverse axis of the wing and with the ability to fly at a hypersonic speed in the direction of the longitudinal axis of the wing. The wing is made with the possibility of reducing the relative thickness of the profile and radii of curvature of the edges of the wing, lengthening the wing, increasing the sweep along the leading edges and narrowing the wing.;EFFECT: invention is aimed at expanding the arsenal of technical means. ;8 cl, 4 dwg
机译:领域:航空。 ;物质:飞行器的飞行器的飞行器含有厚型型设计,该机翼设计用于飞行,具有纵向和横向轴,形成用于以亚音速飞行的配置和以超声波速度,发动机飞行的配置控制。通过在机翼的横向轴线的方向上以亚音速飞行的能力,并且能够在机翼的纵向轴线的方向上以超声速度飞行的能力。通过减少翼形边缘的曲线的相对厚度和轴的边缘的曲率的相对厚度的可能性,延长翼,沿着前边缘的扫描增加并使机翼变窄。;效果:发明旨在扩展技术手段的阿森纳。 ; 8 cl,4 dwg

著录项

  • 公开/公告号RU2744692C2

    专利类型

  • 公开/公告日2021-03-15

    原文格式PDF

  • 申请/专利权人

    申请/专利号RU20190121142

  • 发明设计人 RESHETNIKOV MIKHAIL IVANOVICH (RU);

    申请日2019-07-05

  • 分类号B64C39/10;

  • 国家 RU

  • 入库时间 2022-08-24 17:42:13

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