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Morphing aircraft with telescopic lifting and control surfaces

机译:使飞机具有伸缩式升力和控制面

摘要

A morphing aircraft includes a lifting body and a telescopic lifting or control surface, such as a wing, coupled to the lifting body. The lifting surface is deployable between extended and retracted positions relative to the lifting body and configured such that, when disposed in the extended position, the flight characteristics of the aircraft correspond to those of a low-speed, high-lift aircraft, and when disposed in the retracted position, the flight characteristics of the air-craft correspond to those of a high-speed, low-lift aircraft, the lifting surface is disposed entirely within the lifting body, and an outboard end surface of the lifting surface blends continuously into an outer mold line surface of the lifting body.
机译:变形飞机包括升力体和与升力体连接的可伸缩升力或控制表面,例如机翼。提升表面相对于提升体可在伸展位置和缩回位置之间展开,并且构造成使得当处于伸展位置时,飞行器的飞行特性对应于低速,高升力飞机的飞行特性,并且当被布置时在缩回位置,飞机的飞行特性与高速,低升力飞机的飞行特性相对应,升力面完全设置在升力体内,升力面的外侧端面连续地融入提升体的外部模具线表面。

著录项

  • 公开/公告号US7789343B2

    专利类型

  • 公开/公告日2010-09-07

    原文格式PDF

  • 申请/专利权人 BRANKO SARH;DAVID J. FILE;

    申请/专利号US20070782456

  • 发明设计人 BRANKO SARH;DAVID J. FILE;

    申请日2007-07-24

  • 分类号B64C3/38;

  • 国家 US

  • 入库时间 2022-08-21 18:48:59

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