关于风力轮机截面的中心位置对的影响的实验研究
Qi Zheng1,2,3, Zhiying Gao1,2,3, Baozhong Zhao1,2,3
1Key Laboratory of Wind Energy and Solar Energy Utilization Technology of Ministry of Education, Inner Mongolia University of Technology, Hohhot, 010051, China.
Heliyon
|September 19, 2024
概括
大型风力轮机叶片可能会造成飞损伤. 向前移动心脏状元器件可以提高稳定性,而调度运动是抑制飞的关键. 这项研究提供了关于预防运营故障的见解.
科学领域:
- 航空弹性 航空弹性
- 机械工程 机械工程
- 航空航天工程 航空航天工程
背景情况:
- 大型风力轮机面积比较高,容易在运行过程中因动而造成不可逆转的损坏.
- 了解动力学对于确保风力轮机叶片的结构完整性和寿命至关重要.
研究的目的:
- 为了研究中心位置对风力轮机叶片段的飞边界的影响.
- 分析导致翼的主要因素,并确定有效的抑制策略.
主要方法:
- 建造一个两度自由度 (俯冲和俯冲) 飞测试台.
- 用于动态信号处理的时间和频域分析方法.
- 系统地改变中心点位置,以评估它们对特征的影响.
主要成果:
- 中心位置向前转移,特别是靠近前沿,显著提高了气弹性稳定性.
- 波动主要是由于净减缓的减少以及自然频率的合和合引起的.
- 距离运动是两个自由度系统中占主导地位的模式,随着质量中心远离扭转轴的移动,移位更大.
结论:
- 优化心心位置对于改善风力轮机叶片的飞边界和整体气弹性稳定性至关重要.
- 压制的努力应优先解决由于其主导影响的球位运动.
- 为减轻大型风力轮机中的飞,建议进一步研究以动为重点的控制策略.
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