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A general frequency adaptive framework for damped response analysis of wind turbines

机译:风力涡轮机阻尼响应分析的一般频率自适应框架

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Dynamic response analysis of wind turbine towers plays a pivotal role in their analysis, design, stability, performance and safety. Despite extensive research, the quantification of general dynamic response remains challenging due to an inherent lack of the ability to model and incorporate damping from a physical standpoint. This paper develops a frequency adaptive framework for the analysis of the dynamic response of wind turbines under general harmonic forcing with a damped and flexible foundation. The proposed method is founded on an augmented dynamic stiffness formulation based on a Euler-Bernoulli beam-column with elastic end supports along with tip mass and rotary inertia arising from the nacelle of the wind turbine. The dynamic stiffness coefficients are derived from the complex-valued transcendental displacement function which is the exact solution of the governing partial differential equation with appropriate boundary conditions. The closed-form analytical expressions of the dynamic response derived in the paper are exact and valid for higher frequency ranges. The proposed approach avoids the classical modal analysis and consequently the ad-hoc use of the modal damping factors are not necessary. It is shown that the damping in the wind turbine dynamic analysis is completely captured by seven different physically-realistic damping factors. Numerical results shown in the paper quantify the distinctive nature of the impact of the different damping factors. The exact closed-form analytical expressions derived in the paper can be used for benchmarking related experimental and finite element studies and at the initial design/analysis stage.
机译:风力涡轮机塔的动态响应分析在分析,设计,稳定性,性能和安全方面发挥了枢轴作用。尽管研究广泛,但由于固有的模拟能力和从物理立场抑制阻尼的固有缺乏缺乏能力,普遍动态响应的量化仍然具有挑战性。本文开发了一种频率自适应框架,用于分析通用谐波迫使风力涡轮机的动态响应,具有阻尼和柔性基础。所提出的方法是基于具有弹性端支架的欧拉-Bernoulli梁柱的增强动态刚度配方,以及由风力涡轮机的机舱产生的尖端质量和旋转惯性。动态刚度系数源自复值转向位移函数,其是具有适当边界条件的控制局部微分方程的精确解。纸张中导出的动态响应的闭合形式分析表达式精确且有效地用于更高的频率范围。所提出的方法避免了经典的模态分析,因此不需要使用模态阻尼因子的ad-hoc使用。结果表明,风力涡轮机动态分析中的阻尼被七种不同的物理逼真的阻尼因子完全捕获。纸张中显示的数值结果量化了不同阻尼因子的影响的独特性。纸张中得出的确切闭合形式的分析表达式可用于基准测试相关的实验和有限元研究和初始设计/分析阶段。

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