Abstract
Rotation is one of the critical motion forms in morphing wings. A rotation-locking joint can significantly improve aircraft stability and adaptability across different environments. However, designing a joint that combines stepless locking, high compact, energy efficiency and lightweight remains a considerable challenge. This paper proposes a novel flexible active locking mechanism for rotational motion. Comprising a piezoelectric actuator, a flexible lever mechanism, and a flexible bridge mechanism, it allows locking at any position. A nonlinear model of the mechanism is developed using the compliance matrix method to predict its amplified displacement output in response to input forces. The model’s accuracy is validated through Finite Element Analysis (FEA). Finally, a locking force experiment further demonstrates the feasibility of the locking mechanism. This compact locking system holds significant potential for aerospace application.
| Original language | English |
|---|---|
| Title of host publication | Proceedings of the 2nd Aerospace Frontiers Conference, AFC 2025 - Volume V |
| Publisher | Springer Science and Business Media Deutschland GmbH |
| Pages | 372-386 |
| Number of pages | 15 |
| ISBN (Print) | 9789819529971 |
| DOIs | |
| State | Published - 2026 |
| Event | 2nd Aerospace Frontiers Conference, AFC 2025 - Beijing, China Duration: 11 Apr 2025 → 14 Apr 2025 |
Publication series
| Name | Lecture Notes in Mechanical Engineering |
|---|---|
| ISSN (Print) | 2195-4356 |
| ISSN (Electronic) | 2195-4364 |
Conference
| Conference | 2nd Aerospace Frontiers Conference, AFC 2025 |
|---|---|
| Country/Territory | China |
| City | Beijing |
| Period | 11/04/25 → 14/04/25 |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 7 Affordable and Clean Energy
Keywords
- Compliant mechanism
- Locking force
- Morphing skeleton
- Nonlinear model
- Stepless lockable joint
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