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Integration of the passive energy balancing based actuation system into a camber morphing design

C. Wang, Y. Zhao Orcid Logo, K. Huang, Jiaying Zhang Orcid Logo, Alexander Shaw Orcid Logo, H. Gu Orcid Logo, M. Amoozgar Orcid Logo, Michael Friswell, B.K.S. Woods Orcid Logo

Aerospace Science and Technology, Volume: 155, Issue: 2

Swansea University Authors: Jiaying Zhang Orcid Logo, Alexander Shaw Orcid Logo, Michael Friswell

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DOI (Published version): 10.1016/j.ast.2024.109641

Abstract

A spiral pulley mechanism can be used to passively balance the energy between the morphing structure and actuation system. Applying the energy balancing concept has the potential to improve the performance of the actuation system by reducing the external energy consumption. In the current study, the...

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Published in: Aerospace Science and Technology
ISSN: 1270-9638 1626-3219
Published: Elsevier BV 2024
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URI: https://cronfa.swan.ac.uk/Record/cronfa67989
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spelling v2 67989 2024-10-15 Integration of the passive energy balancing based actuation system into a camber morphing design 12b61893c794b14f11cf0a84cb947d0e 0000-0001-7308-5090 Jiaying Zhang Jiaying Zhang true false 10cb5f545bc146fba9a542a1d85f2dea 0000-0002-7521-827X Alexander Shaw Alexander Shaw true false 5894777b8f9c6e64bde3568d68078d40 Michael Friswell Michael Friswell true false 2024-10-15 A spiral pulley mechanism can be used to passively balance the energy between the morphing structure and actuation system. Applying the energy balancing concept has the potential to improve the performance of the actuation system by reducing the external energy consumption. In the current study, the integration workflow for the passive energy balancing device is established and is adopted in a variable camber morphing wing. The design variables of the passive energy balancing system are optimised and the effects of the different parameters are discussed together with the adaptability of the passive energy balancing device when the load stiffness changes. An integrated demonstrator was also built to validate the mechanism by measuring the currents in the process of morphing actuation. Journal Article Aerospace Science and Technology 155 2 Elsevier BV 1270-9638 1626-3219 Passive energy balancing, morphing wing, energy efficiency, tuned stiffness 1 12 2024 2024-12-01 10.1016/j.ast.2024.109641 COLLEGE NANME COLLEGE CODE Swansea University Not Required This project has received funding from the European Union‘s Horizon 2020 research and innovation program under grant agreement No 723491. The first two authors would like to acknowledge the funding from National Natural Science Foundation of China (Grant No 52305262) and the Starting Grant of Nanjing University of Aeronautics and Astronautics (Grant No YQR22056). The third and fourth author would like to acknowledge the funding from National Natural Science Foundation of China (Grant No 12102017, 92271104) and Beijing Natural Science Foundation (Grant No 1232014). 2024-10-15T12:57:24.4736006 2024-10-15T12:39:08.6987097 Faculty of Science and Engineering School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering C. Wang 1 Y. Zhao 0009-0002-9175-5590 2 K. Huang 3 Jiaying Zhang 0000-0001-7308-5090 4 Alexander Shaw 0000-0002-7521-827X 5 H. Gu 0000-0001-9562-5326 6 M. Amoozgar 0000-0003-1670-9762 7 Michael Friswell 8 B.K.S. Woods 0000-0002-8151-3195 9
title Integration of the passive energy balancing based actuation system into a camber morphing design
spellingShingle Integration of the passive energy balancing based actuation system into a camber morphing design
Jiaying Zhang
Alexander Shaw
Michael Friswell
title_short Integration of the passive energy balancing based actuation system into a camber morphing design
title_full Integration of the passive energy balancing based actuation system into a camber morphing design
title_fullStr Integration of the passive energy balancing based actuation system into a camber morphing design
title_full_unstemmed Integration of the passive energy balancing based actuation system into a camber morphing design
title_sort Integration of the passive energy balancing based actuation system into a camber morphing design
author_id_str_mv 12b61893c794b14f11cf0a84cb947d0e
10cb5f545bc146fba9a542a1d85f2dea
5894777b8f9c6e64bde3568d68078d40
author_id_fullname_str_mv 12b61893c794b14f11cf0a84cb947d0e_***_Jiaying Zhang
10cb5f545bc146fba9a542a1d85f2dea_***_Alexander Shaw
5894777b8f9c6e64bde3568d68078d40_***_Michael Friswell
author Jiaying Zhang
Alexander Shaw
Michael Friswell
author2 C. Wang
Y. Zhao
K. Huang
Jiaying Zhang
Alexander Shaw
H. Gu
M. Amoozgar
Michael Friswell
B.K.S. Woods
format Journal article
container_title Aerospace Science and Technology
container_volume 155
container_issue 2
publishDate 2024
institution Swansea University
issn 1270-9638
1626-3219
doi_str_mv 10.1016/j.ast.2024.109641
publisher Elsevier BV
college_str Faculty of Science and Engineering
hierarchytype
hierarchy_top_id facultyofscienceandengineering
hierarchy_top_title Faculty of Science and Engineering
hierarchy_parent_id facultyofscienceandengineering
hierarchy_parent_title Faculty of Science and Engineering
department_str School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering
document_store_str 0
active_str 0
description A spiral pulley mechanism can be used to passively balance the energy between the morphing structure and actuation system. Applying the energy balancing concept has the potential to improve the performance of the actuation system by reducing the external energy consumption. In the current study, the integration workflow for the passive energy balancing device is established and is adopted in a variable camber morphing wing. The design variables of the passive energy balancing system are optimised and the effects of the different parameters are discussed together with the adaptability of the passive energy balancing device when the load stiffness changes. An integrated demonstrator was also built to validate the mechanism by measuring the currents in the process of morphing actuation.
published_date 2024-12-01T12:57:22Z
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score 11.0351515

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