Mistuning sensitivity and optimization for bladed disks using high-fidelity models

被引:22
作者
Tan, Yuanqiu [1 ]
Zang, Chaoping [1 ]
Petrov, E. P. [2 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Jiangsu, Peoples R China
[2] Univ Sussex, Brighton BN1 9QT, E Sussex, England
基金
中国国家自然科学基金;
关键词
Rotordynamics; Mistuned bladed disk; Forced response; Sensitivity; FORCED RESPONSE; VIBRATION; LOCALIZATION; MINIMIZATION; ALGORITHM;
D O I
10.1016/j.ymssp.2019.02.002
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
An effective method is developed for efficient calculations of the sensitivity of the maximum forced response levels for mistuned bladed disks with respect to blade frequency mistuning. The expressions for 1st and 2nd order sensitivity coefficients are derived in an analytical form which provides high accuracy and computational efficiency. Then, the optimization methods are used for searching the best and worst mistuning patterns of bladed disks. Two major types of the mistuning optimization problems are considered: (i) a continuous optimization problem when the blade mistuning can take any values from a prescribed range and (ii) a combinatorial optimization problem, when the set of mistuned blades is given and the optimization can be achieved by blade re-arrangement in a disk. For the first type of the optimization problem a set of sensitivity-based optimization algorithms is applied and for the second type a variant of a genetic algorithm is developed. The analysis of mistuning sensitivity coefficients and results of optimization searching are shown on an example of a realistic turbine bladed disk. (C) 2019 Published by Elsevier Ltd.
引用
收藏
页码:502 / 523
页数:22
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