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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Designing the Ornicopter, a tailless helicopter with active flapping blades: a case study
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Designing the Ornicopter, a tailless helicopter with active flapping blades: a case study

机译:设计Ornicopter,这是一款具有主动襟翼的无尾直升机:案例研究

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摘要

The Ornicopter concept is a single-rotor, tailless configuration. By actively flapping its blades, the Ornicopter rotor can propel itself to rotate, and hence does not need a tail rotor. In previous research, the Ornicopter concept has been compared with the Bo-105 conventional helicopter from various aspects, while the Ornicopter has the same design parameters as the Bo-105. Comparisons show that the Ornicopter has one major drawback, namely a small flight envelope. To improve the Ornicopter performance and understand how the Ornicopter should be designed, in this paper, the Ornicopter design is unfrozen and optimized for the flight envelope. The optimization result shows that with a proper design, the Ornicopter performance can be improved dramatically. A similar flight envelope as the Bo-105 can be achieved for the Ornicopter. However, the Ornicopter requires higher power than the Bo-105 due to the inherent characteristics of this concept.
机译:Ornicopter概念是单旋翼无尾翼配置。通过主动拍打其叶片,Ornicopter旋翼可以推动自身旋转,因此不需要尾旋翼。在先前的研究中,Ornicopter概念已从各个方面与Bo-105常规直升机进行了比较,而Ornicopter具有与Bo-105相同的设计参数。比较表明,直升机具有一个主要缺点,即较小的飞行包线。为了提高Ornicopter的性能并了解应如何设计Ornicopter,本文对Ornicopter的设计进行了冻结并针对飞行包线进行了优化。优化结果表明,通过适当的设计,可以显着提高Ornicopter的性能。直升机可以达到与Bo-105类似的飞行包线。但是,由于这种概念的固有特性,Ornicopter需要比Bo-105更高的功率。

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