Duct-Winged Inertial Bicopter: Theory, Design and Testing

G. Gress
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Abstract

This paper describes and reports on the status of an electric vertical take-off and landing (eVTOL) aircraft type being developed at Athena Aero Corp that began life as a concept entry in the Boeing-sponsored GoFly Challenge initiated in Sept. 2017. Known as a duct-winged inertial bicopter, the concept was intended to satisfy the Challenge’s basic requirements of giving the pilot an unobstructed forward view within a 90-degree cone and of being able to: 1.take off and land (essentially) vertically, 2.transport a 200 lb. person six times around two pylons a half-mile apart at a speed of at least 30kts, and 3.stay aloft for 20 minutes with a 10-minute fuel/energy reserve, all in a single flight. Additionally, the aircraft could be no larger than 8.5 ft. in any direction and had to be quieter than 85 dB at 50 ft. on take-off.
导管翼惯性双旋翼:理论、设计与试验
本文描述并报告了雅典娜航空公司(Athena Aero Corp)正在开发的电动垂直起降(eVTOL)飞机的现状,该飞机于2017年9月作为波音赞助的GoFly挑战赛的概念项目开始使用。这个概念被称为导管翼惯性直升机,旨在满足挑战赛的基本要求,即在90度锥体内为飞行员提供无阻碍的前视图,并能够:起飞和降落(基本上)垂直,2。运送一个200磅重的人,以至少30公里的速度绕两个半英里的桥塔运输六次;在空中停留20分钟,并有10分钟的燃料/能量储备,所有这些都是在一次飞行中完成的。此外,飞机在任何方向上都不能超过8.5英尺,起飞时在50英尺处的噪音必须低于85分贝。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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