A Novel Design of a Torsional Shape Memory Alloy Actuator for Active Rudder

Author:

Lima Felipe S.1,Souto Cícero R.2ORCID,Oliveira Andersson G.1,Silvestre Alysson D.3,Alves Railson M. N.1ORCID,Santos Sebastião E. S.4,Gomez Ricardo S.4,Brito Glauco R. F.5ORCID,Bezerra André L. D.5,Santana Diogenes S. M.5,Lima Antonio G. B.4ORCID

Affiliation:

1. Department of Mechanical Engineering, Federal University of Paraíba, João Pessoa 58051-900, Brazil

2. Department of Electrical Engineering, Federal University of Paraíba, João Pessoa 58051-900, Brazil

3. Department of Mechatronics, Federal Institute of Education, Science and Technology of Pernambuco, Caruaru 55040-120, Brazil

4. Department of Mechanical Engineering, Federal University of Campina Grande, Campina Grande 58429-900, Brazil

5. Postgraduate Program in Process Engineering, Federal University of Campina Grande, Campina Grande 58429-900, Brazil

Abstract

SMA actuators are a group of lightweight actuators that offer advantages over conventional technology and allow for simple and compact solutions to the increasing demand for electrical actuation. In particular, an increasing number of SMA torsional actuator applications have been published recently due to their ability to supply rotational motion under load, resulting in advantages such as module simplification and the reduction of overall product weight. This paper presents the conceptual design, operating principle, experimental characterization and working performance of torsional actuators applicable in active rudder in aeronautics. The proposed application comprises a pair of SMA torsion springs, which bi-directionally actuate the actuator by Joule heating and natural cooling. The experimental results confirm the functionality of the torsion springs actuated device and show the rotation angle of the developed active rudder was about 30° at a heating current of 5 A. After the design and experiment, one of their chief drawbacks is their relatively slow operating speed in rudder positioning, but this can be improved by control strategy and small modifications to the actuator mechanism described in this work.

Funder

CNPq

Publisher

MDPI AG

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