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Rapidly convertible hybrid aircraft and manufacturing method

机译:可快速转换的混合动力飞机及其制造方法

摘要

A hybrid fixed wing aircraft converts into a roadworthy vehicle in a matter of seconds therefore operating efficiently in both air and ground transportation systems. The single piece wing is mounted on a skewed pivot that is on the lower portion of the fuselage and is operated by a pushbutton operating system. The aircraft includes telescopic twin boom tail design that when extended allows good pitch stability and damping. The aircraft's wing area may be increased with additional telescopic wing tip segments. This allows an increase in aspect ratio, hence improving efficiency at high loads. This feature also creates a reduction in induced drag at cruise speed by simply retracting the tips in flight. The vehicle has a unique synchronized control system that switches from flight to ground mode without input from the operator, thereby providing a natural interface for the operator.
机译:混合式固定翼飞机只需几秒钟即可转换为可行驶的车辆,因此可以在空中和地面运输系统中高效运行。单件机翼安装在机身下部的偏心枢轴上,并由按钮操作系统进行操作。该飞机采用伸缩式双动臂尾翼设计,伸出后可实现良好的俯仰稳定性和阻尼。飞机的机翼面积可能会增加其他伸缩式机翼尖端部分。这允许增加纵横比,从而提高高负载下的效率。通过简单地缩回飞行中的尖端,此功能还可以降低巡航速度下的感应阻力。该车辆具有独特的同步控制系统,无需驾驶员的输入即可从飞行模式切换到地面模式,从而为驾驶员提供自然的界面。

著录项

  • 公开/公告号US8371520B2

    专利类型

  • 公开/公告日2013-02-12

    原文格式PDF

  • 申请/专利权人 WILLIAM CRAIG EASTER;

    申请/专利号US20100846882

  • 发明设计人 WILLIAM CRAIG EASTER;

    申请日2010-07-30

  • 分类号B64C37;B64C27/24;B64C3/56;B64C9/34;

  • 国家 US

  • 入库时间 2022-08-21 16:46:01

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