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Fiber-reinforced polymers with integrated shape memory alloy actuation: an innovative actuation method for aerodynamic applications

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Abstract

This contribution focuses on the application potential of active fiber-reinforced polymer (FRP) structures with integrated shape memory alloy (SMA) elements for new aerodynamic functions. The advantages of hybrid SMA FRP structures are highlighted, and promising application concepts are discussed. To illustrate the applicability of the technology, the developed manufacturing, design, and control approaches are presented. Main focus is the development of a new concept for an active aerodynamic airfoil and the realization of a hardware demonstrator. Beginning with the idea of an adaptive airfoil, able to bear an application relevant down force at a relatively high deflection, the design process starts with an evaluation of different actuation concepts. An SMA-powered cantilever is a part of the profile itself. Applying the finite-element method with a suitable model for the active hybrid material, an effective selection of material and design is possible. After manufacturing and assembling of the active hybrid airfoil, a comparison of experimental results and simulation is the first proof of success. Finally, the installation of an integrated hardware setup with power source, control, and the active hybrid structure, demonstrating actuation on demand, verifies the potential and the distinct advantages of the new approach using SMA FRP structures.

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Authors and Affiliations

  1. Institut für Verbundwerkstoffe GmbH, Erwin-Schrödinger-Str. 58, 67663, Kaiserslautern, Germany

    M. Hübler, S. Nissle, M. Gurka & U. Breuer

Authors
  1. M. Hübler
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  2. S. Nissle
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  3. M. Gurka
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  4. U. Breuer
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Correspondence to M. Hübler.

Additional information

This paper is based on a presentation at the German Aerospace Congress, September 22–24, 2015, Rostock, Germany.

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Hübler, M., Nissle, S., Gurka, M. et al. Fiber-reinforced polymers with integrated shape memory alloy actuation: an innovative actuation method for aerodynamic applications. CEAS Aeronaut J 7, 567–576 (2016). https://doi.org/10.1007/s13272-016-0209-0

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  • DOI: https://doi.org/10.1007/s13272-016-0209-0

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