Tailored Twist Morphing Achieved using Graded Bend-twist Metamaterials

H Gu (University of Bristol), J Taghipour, AD Shaw (Swansea University), MR Amoozgar (University of Nottingham), J Zhang (Beihang University, China), C Wang (Nanjing University of Aeronautics and Astronautics, China) & MI Friswell (Swansea University)

Composite Structures, Vol. 300, 15 November 2022, paper 116151

This work develops a morphing concept that utilises a metamaterial as the passive morphing device for helicopter blades. The metamaterials are created with bend-twist coupling, which enable the blade twist under prescribed bending loads. Finite element analysis (FEA) is performed to investigate the influence of the unit cell configurations on the coupling properties of the metamaterials. The numerical models are then validated experimentally through a set of bending tests conducted with additively manufactured prototypes. Finally, the validated model is used to design a graded metamaterial, where the cell aspect ratio gradually changes along the blade span, providing unique bend-twist coupling and allowing for tailored twist to be obtained. The results suggest the graded metamaterials are capable of introducing optimised nonlinear twists to the blade during different flight conditions including both hover and forward flight.

Paper Availability

This material has been published in the Composite Structures, Vol. 300, 15 November 2022, paper 116151. This article is published with open access.


Link to paper using doi: 10.1016/j.compstruct.2022.116151

Composite Structures

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