An optimization method based on the evolutionary and topology approaches to reduce the mass of composite wind turbine blades

被引:34
作者
Albanesi, A. E. [1 ]
Peralta, I. [1 ]
Bre, F. [1 ]
Storti, B. A. [1 ]
Fachinotti, V. D. [1 ]
机构
[1] UNL, CONICET, CIMEC Ctr Invest Metodos Computac, Santa Fe, Argentina
关键词
Genetic algortihms; Topology optimization; Inverse finite element method; Composite material layout; Wind turbine blades; STRUCTURAL OPTIMIZATION; LAMINATED COMPOSITES; GENETIC ALGORITHM; DESIGN;
D O I
10.1007/s00158-020-02518-2
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
The design of large and lightweight wind turbines is a current challenge in the wind energy industry. In this context, this work aims to present a novel methodology to reduce the mass of composite wind turbine blades by combining evolutionary and topology optimization schemes in a staggered mode. First, the optimal laminate layout in the outer shell skin of the blade is determined by using genetic algorithms and by assuming that the shear webs are fully dense. Considering this optimized shell skin, the material is removed from the shear webs by using topology optimization. In both cases, the blade is assumed to be subjected to an extreme load scenario, with constraints on the tip displacement, the stresses, the natural vibration frequencies, and buckling phenomena. As an extra feature, the methodology integrates the inverse finite element method to recover the aerodynamically efficient shape of the blade when it is working in normal load scenario as well as to increase the tower clearance safety margin under the extreme load scenario. To illustrate the performance of the methodology, the design of a 28.5-m composite blade is presented. Results show mass savings of up to 23% and a significant increase of the tower clearance safety margin. Furthermore, it is observed that after the classical genetic optimization of the shell skin, there is still margin to achieve additional mass savings via topology optimization of the shear webs without compromising the structural response of the blade.
引用
收藏
页码:619 / 643
页数:25
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