风力涡轮机叶片翼梁帽

By designing a tapered end section of the intermediate pultruded layer sandwiched between the pultruded layers of the sub-laminated layers in the spar cap of the wind turbine blade, the problem of load asymmetry in the tapered section is solved, achieving uniform load distribution and avoiding stress concentration, thereby improving the stiffness and service life of the structure.

CN122422653APending Publication Date: 2026-07-17VESTAS WIND SYSTEMS AS
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
VESTAS WIND SYSTEMS AS
Filing Date
2024-12-17
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

The existing wind turbine blade spars caps bear asymmetrical high loads at the interface between the pultruded end of the tapered section and the adjacent pultruded section that extends further, resulting in load imbalance and stress concentration.

Method used

A wing cap structure is designed in which the tapered end section of the middle pultruded layer is sandwiched between multiple pultruded layers of the first and second sub-laminated layers. Through the non-uniform configuration of the tapered end section and the layup of the sandwiched pultruded layers, the load is evenly distributed and stress concentration is avoided.

Benefits of technology

This design achieves uniform load distribution at the tapered end of the wing spars, avoiding stress concentration, improving the symmetry and stiffness uniformity of the structure, and enhancing the service life and load-bearing capacity of the blades.

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Abstract

在本发明的第一方面,提供了一种风力涡轮机叶片翼梁帽。翼梁帽具有上翼梁帽表面、下翼梁帽表面以及限定在上翼梁帽表面与下翼梁帽表面之间的翼梁帽厚度。翼梁帽具有中间部分和渐缩端部部分,在整个中间部分中翼梁帽厚度基本恒定,在渐缩端部部分中翼梁帽厚度朝向翼梁帽的端部减小。翼梁帽包括布置在叠层中的多个拉挤层。每个拉挤层具有上拉挤层表面、下拉挤层表面以及限定在相应的上拉挤层表面与下拉挤层表面之间的层厚度。叠层包括第一子叠层和第二子叠层,第一子叠层包括多个拉挤层,第二子叠层包括多个拉挤层。叠层还包括中间拉挤层,中间拉挤层包括渐缩端部区段,在该渐缩端部区段中中间拉挤层的层厚度朝向翼梁帽的端部减小。渐缩端部区段位于翼梁帽的渐缩端部部分中。中间拉挤层被夹设在第一子叠层与第二子叠层之间,使得在翼梁帽的渐缩端部部分中,中间拉挤层的渐缩端部区段被夹设在第一子叠层的多个拉挤层与第二子叠层的多个拉挤层之间。
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