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Reliability analysis of turbine blades based on fuzzy response surface method

机译:基于模糊响应面法的涡轮叶片可靠性分析

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摘要

To improve the precision of reliability analysis on turbine blades, the fuzzy response surface method of reliability analysis is proposed by considering the fuzziness of the input variables and the vagueness of the limit state variables. Initially, the fuzzy basic variables were converted into equivalent random variables according to the method of equivalent transformation. Additionally, the mathematic model of the fuzzy response surface for structural reliability analysis was established, based on the quadratic polynomial response surface function. The mean value and variance of the blade stress and radial deformation were obtained by using the Monte-Carlo method based on generous linkage sampling to the model. Finally, the probability of failure and fuzzy random reliability index were calculated based on the probability integral method. Results indicate that the reliability probability of the blade is 97.665%, when the allowable stress and deformation are 390 MPa and 0.195 mm, respectively. It is demonstrated that with an increase of the fuzzy coefficient, the blade reliability index decreases; thus, the random reliability of the blade is slightly higher than the fuzzy reliability.
机译:为了提高涡轮叶片可靠性分析的精度,在考虑输入变量的模糊性和极限状态变量的模糊性的基础上,提出了可靠性分析的模糊响应面法。最初,根据等效变换的方法将模糊基本变量转换为等效随机变量。此外,基于二次多项式响应面函数,建立了用于结构可靠度分析的模糊响应面数学模型。在模型的慷慨链接采样的基础上,使用蒙特卡洛方法获得了叶片应力和径向变形的平均值和方差。最后,基于概率积分法计算了失效概率和模糊随机可靠性指标。结果表明,当许用应力和变形分别为390 MPa和0.195 mm时,叶片的可靠性概率为97.665%。结果表明,随着模糊系数的增加,叶片的可靠性指标降低。因此,叶片的随机可靠性略高于模糊可靠性。

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