High-bandwidth morphing actuator for aeroelastic model control

Fichera, S, Isnardi, I and Mottershead, JE (2019) High-bandwidth morphing actuator for aeroelastic model control. Aerospace, 6 (2).

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Abstract

© 2019 by the authors. The design and testing of a high-bandwidth continuous actuator for aeronautical applications is presented hereinafter. The actuator has a dual goal of controlling both the aeroelastic behaviour and the flight mechanics of the model in which it is installed. In order to achieve these aims, the actuation bandwidth of the active aerofoil, as well as its static camber variation, have to be sufficiently high. The camber morph is achieved by using tailored piezoelectric patches in a sandwich configuration with a linear trailing edge slider to allow the necessary compliance. The morphing actuator is designed for a NACA 0018 aerofoil with a chord of 300mmand a span of 40 mm. Static and dynamic experimental tests are carried out on a prototype, and a camber variation control technique is implemented. It is proved that the actuator bandwidth is up to 25 Hz and the equivalent maximum deflection is ±15 degrees. This solution is shown to be a viable light-weight alternative to the conventional brushless/servo-motor approach currently used in aeroelastic models.

Item Type:	Article
Depositing User:	Symplectic Admin
Date Deposited:	15 Mar 2019 10:26
Last Modified:	19 Jan 2023 00:56
DOI:	10.3390/aerospace6020013
Open Access URL:	https://doi.org/10.3390/aerospace6020013
URI:	https://livrepository.liverpool.ac.uk/id/eprint/3034331