Towards a digital twin realization of the blade system design study wind turbine blade

被引:10
作者
Baldassarre, Alessandro [1 ]
Ceruti, Alessandro [2 ]
Valyou, Daniel N. [3 ]
Marzocca, Pier [4 ]
机构
[1] Clarkson Univ, Dept Mech & Aeronaut Engn MAE, 8 Clarkson Ave, Potsdam, NY 13699 USA
[2] Univ Bologna, Dept Ind Engn DIN, Viale Risorgimento 2, I-40136 Bologna, Italy
[3] Clarkson Univ, Sch Engn, 8 Clarkson Ave, Potsdam, NY 13699 USA
[4] RMIT Univ, Sch Engn Aerosp Engn & Aviat, Bundoora, Vic 3083, Australia
关键词
wind turbine; digital twin; finite element method; composite materials; modeling and simulation; design; PERFORMANCE; SIMULATION;
D O I
10.12989/was.2019.28.5.271
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
This paper describes the application of a novel virtual prototyping methodology to wind turbine blade design. Numeric modelling data and experimental data about turbine blade geometry and structural/dynamical behaviour are combined to obtain an affordable digital twin model useful in reducing the undesirable uncertainties during the entire turbine lifecycle. Moreover, this model can be used to track and predict blade structural changes, due for example to structural damage, and to assess its remaining life. A new interactive and recursive process is proposed. It includes CAD geometry generation and finite element analyses, combined with experimental data gathered from the structural testing of a new generation wind turbine blade. The goal of the research is to show how the unique features of a complex wind turbine blade are considered in the virtual model updating process, fully exploiting the computational capabilities available to the designer in modern engineering. A composite Sandia National Laboratories Blade System Design Study (BSDS) turbine blade is used to exemplify the proposed process. Static, modal and fatigue experimental testing are conducted at Clarkson University Blade Test Facility. A digital model was created and updated to conform to all the information available from experimental testing. When an updated virtual digital model is available the performance of the blade during operation can be assessed with higher confidence.
引用
收藏
页码:271 / 284
页数:14
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