Optimization of Intentional Mistuning Patterns for the Mitigation of the Effects of Random Mistuning

Author:

Han Yun1,Murthy Raghavendra2,Mignolet Marc P.3,Lentz Jeff4

Affiliation:

1. Mem. ASME SEMTE, Faculties of Mechanical and Aerospace Engineering, Arizona State University, Tempe, AZ 85287-6106 e-mail:

2. Mem. ASME SEMTE, Faculties of Mechanical and Aerospace Engineering, Arizona State University, Tempe, AZ 85287-6106 e-mail:

3. Fellow ASME SEMTE, Faculties of Mechanical and Aerospace Engineering, Arizona State University, Tempe, AZ 85287-6106 e-mail:

4. Department 93-34/301-134, Honeywell Aerospace, P.O. Box 52181, Phoenix, AZ 85072-2181 e-mail:

Abstract

This paper focuses on the optimization of intentional mistuning patterns for the reduction of the sensitivity of the forced response of bladed disks to random mistuning. Intentional mistuning is achieved here by using two different blade types (denoted as A and B) around the disk. It is thus desired to find the arrangement of these A and B blades (A/B pattern) that leads to the smallest 99th percentile of the amplitude of blade response in the presence of random mistuning. It is first demonstrated that there usually is a large number of local minima and further that the cost of a function evaluation is high. Accordingly, two novel, dedicated optimization algorithms are formulated and validated to address this specific problem. Both algorithms proceed in a two-step fashion. The first step, which consists of an optimization in a reduced space, leads to a series of good initial guesses. A local search from these initial guesses forms the second step of the methods. A detailed validation effort of this new procedure was next achieved on a single-degree-of-freedom-per-blade model, a reduced order model of a blisk, and that of an impeller considered in an earlier study. In all validation cases, the two novel algorithms were found to converge to the global optimum or very close to it at a small computational cost. Finally, the results of these optimization efforts further demonstrate the value of intentional mistuning to increase the robustness of bladed disks to random mistuning.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference17 articles.

1. Localization Phenomena in Mistuned Assemblies With Cyclic Symmetry—Part I: Free Vibrations;ASME J. Vib., Acoust., Stress, Reliab. Des.,1988

2. Localization Phenomena in Mistuned Assemblies With Cyclic Symmetry—Part II: Forced Vibrations;ASME J. Vib., Acoust., Stress, Reliab. Des.,1988

3. Flutter of Turbofan Rotors With Mistuned Blades;AIAA J.,1984

4. Vibration and Flutter of Mistuned Bladed-Disk Assemblies;J. Propul.,1985

5. Consideration on the Benefits of Intentional Blade Mistuning for the Forced Response of Turbomachinery Rotors,1997

Cited by 37 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3