Blisk With Small Geometry Mistuning and Blend Repair: As-Measured Finite Element Model and Experimental Verification

Author:

Zhou Biao1,Zhao Jingchao1,Ye Nan2,Berruti Teresa M.3

Affiliation:

1. College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics , Nanjing 210016, China

2. College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics , Nanjing 210016, China

3. Dipartimento di Ingegneria Meccanica e Aerospaziale, Politecnico di Torino , Torino 10129, Italy

Abstract

Abstract This paper presents an “As-Measured Model” (AMM) of a blended blisk, built upon the measurement of the true geometry of the blisk by the three-dimensional optical scanning technology. This high-fidelity model aims to account for the variances of blade frequencies and mode shapes within the real blisk in the presence of both the blend repair and inherent geometry mistuning due to manufacturing, etc. An improved mesh updating strategy is proposed to adapt a seed blisk finite element model (FEM) to the measured geometry. The resultant AMM is therefore able to accurately represent the measured blade-to-blade geometry variances. The classical blade detuning test (BDT) in combination with a novel “correction” procedure is employed to experimentally evaluate the “blade-alone” frequency mistuning pattern in the real blisk. Experimental verification of the AMM demonstrates that it is able to not only capture the blade-alone frequency and mode shape variations due to both the blend and intrinsic blade geometry variances, but also to reproduce the global dynamics of the blended blisk with acceptable accuracy.

Funder

European Commission

National Natural Science Foundation of China

Publisher

ASME International

Subject

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

Reference27 articles.

1. Recent Progress in Turbine Blade and Compressor Blisk Regeneration;Procedia CIRP,2014

2. Influence of Geometric Imperfections on Aerodynamic and Aeroelastic Behavior of a Compressor Blisk,2017

3. Blended Fan Blade Effects on Aerodynamic Forces,2019

4. Blended Fan Blade Effects on Unsteady Aerodynamics,2020

5. Consequences of Borescope Blending Repairs on Modern High Pressure Compressor Blisk Aeroelasticity;ASME J. Turbomach.,2019

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