Designing the Ornicopter, a tailless helicopter with active flapping blades

a case study

Journal Article (2016)
Author(s)

J Wan (Shanghai Jiao Tong University)

M.D. Pavel (TU Delft - Control & Simulation)

Copyright
© 2016 J. Wan, M.D. Pavel
DOI related publication
https://doi.org/10.1177/0954410015622228
More Info
expand_more
Publication Year
2016
Language
English
Copyright
© 2016 J. Wan, M.D. Pavel
Issue number
12
Volume number
230
Pages (from-to)
2195-2219
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

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.

Files

License info not available