Passive load alleviation bi-stable morphing concept
Source abstract
Abstract
In wind turbines, large loads caused by fluid structure interaction leading to fatigue failure and added robustness to withstand high bending stresses on the root of blades constitute important design bottlenecks. Implementation of morphing offers a potential solution for such challenges in wind turbine blades. In this letter, a passive load alleviating bi-stable morphing concept is proposed. A bi-stable specimen designed to have different stiffness and dynamic response characteristics on each stable state is devised as a compliant structure. Passive alleviation mechanisms require no active components to achieve the load alleviation objective, resulting in lighter and simpler designs in comparison to actively morphed solutions.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Vibration and Dynamic Analysis · Acoustic Wave Phenomena Research · Fluid Dynamics and Vibration Analysis
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Technische Universität Darmstadt 1 System Reliability and Machine Acoustics, Dynamics and Vibrations Group, , LOEWE-Zentrum AdRIA, Darmstadt, 64289 Germany
Swansea University 2 College of Engineering, , Singleton Park, Swansea, SA2 8PP UK
References (9)
Show source-provided references
1. Upwind: Design limits and solutions for very large wind turbines
2. Morphing skins
3. A morphing wind turbine blade control surface
4. B. Lambie, Aeroelastic Investigation of a Wind Turbine Airfoil with Self-Adaptive Camber, PhD thesis, Technische Universität Darmstadt, 2011.
5. Some observations on the cured shapes of thin unsymmetric laminates10.1177/002199838101500207 ↗
6. F. Mattioni, Thermally induced multi-stable composites for morphing aircraft applications, PhD thesis, University of Bristol, 2009.10.1117/12.776226 ↗
7. Dynamic control for morphing of bi-stable composites
8. Experimental investigation of bistable winglets to enhance wing lift10.2514/1.39614 ↗
9. Aeroelastic study of bistable composite airfoils10.2514/1.44287 ↗