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

• DOI: 10.1007/s00158-020-02518-2
• Publication Date: 2020-03-05T10:03:00Z
• Authors: A. E. Albanesi; I. Peralta; F. Bre; B. A. Storti; V. D. Fachinotti
• Keywords: 0203 mechanical engineering; https://purl.org/becyt/ford/2.5; GENETIC ALGORTIHMS; https://purl.org/becyt/ford/2.3; WIND TURBINE BLADES; COMPOSITE MATERIAL LAYOUT; 02 engineering and technology; https://purl.org/becyt/ford/2; 7. Clean energy; INVERSE FINITE ELEMENT METHOD; TOPOLOGY OPTIMIZATION

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.