Design and development of an unconventional VTOL micro air vehicle: The Cyclocopter

Moble Benedict; Inderjit Chopra

doi:10.1117/12.919482

11 May 2012 Design and development of an unconventional VTOL micro air vehicle: The Cyclocopter

Moble Benedict, Inderjit Chopra

Proceedings Volume 8373, Micro- and Nanotechnology Sensors, Systems, and Applications IV; 83731F (2012) https://doi.org/10.1117/12.919482
Event: SPIE Defense, Security, and Sensing, 2012, Baltimore, Maryland, United States

Abstract

This paper discusses the systematic experimental and vehicle design/development studies conducted at the University of Maryland which culminated in the development of the first flying Cyclocopter in the history. Cyclocopter is a novel Vertical Take-Off and Landing (VTOL) aircraft, which utilizes cycloidalrotors (cyclorotors), a revolutionary horizontal axis propulsion concept, that has many advantages such as higher aerodynamic efficiency, maneuverability and high-speed forward flight capability when compared to a conventional helicopter rotor. The experimental studies included a detailed parametric study to understand the effect of rotor geometry and blade kinematics on cyclorotor hover performance. Based on the experimental results, higher blade pitch angles were found to improve thrust and increase the power loading (thrust per unit power) of the cyclorotor. Asymmetric pitching with higher pitch angle at the top than at the bottom produced better power loading. The chordwise optimum pitching axis location was observed to be around 25-35% of the blade chord. Because of the flow curvature effects, the cycloidal rotor performance was a strong function of the chord/radius ratio. The optimum chord/radius ratios were extremely high, around 0.5-0.8, depending on the blade pitching amplitude. A flow field investigation was also conducted using Particle Image Velocimetry (PIV) to unravel the physics behind thrust production of a cyclorotor. PIV studies indicated evidence of a stall delay as well as possible increases in lift on the blades from the presence of a leading edge vortex. The goal of all these studies was to understand and optimize the performance of a micro-scale cyclorotor so that it could be used in a flying vehicle. An optimized cyclorotor was used to develop a 200 gram cyclocopter capable of autonomous stable hover using an onboard feedback controller.

Citation Download Citation

Moble Benedict and Inderjit Chopra "Design and development of an unconventional VTOL micro air vehicle: The Cyclocopter", Proc. SPIE 8373, Micro- and Nanotechnology Sensors, Systems, and Applications IV, 83731F (11 May 2012); https://doi.org/10.1117/12.919482

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