An Experimental Investigation on the Dynamic Response Variability of a Turbine Blade With Midspan Dampers

Author:

Ferhatoglu Erhan1,Botto Daniele1,Zucca Stefano1

Affiliation:

1. Department of Mechanical and Aerospace Engineering, Politecnico di Torino , Italy Corso Duca degli Abruzzi 24, Torino 10129, Italy

Abstract

Abstract This paper addresses two main subjects. First, a novel test setup is described to experimentally study the nonlinear dynamic behavior of a turbine blade coupled with two midspan dampers (MSDs). To this end, a representative turbine blade and midspan friction dampers are originally designed, and they are assembled to a special test rig which has been previously developed at Politecnico di Torino. Second, the variability of the dynamic response is intensively investigated with a purposely defined loading/unloading strategy. To better understand the inherent kinematics of the blade–damper interaction, contact forces are measured through the novel design of the experimental campaign. It is shown that multiple responses, which are obtained in different tests while keeping all user-controlled inputs nominally same, are due to nonunique contact forces that provide different static force equilibria on the damper. This outcome is further supported by the qualitative illustration of hysteresis cycles. This study contributes to the understanding of the response repeatability linked to the nonuniqueness of friction forces.

Publisher

ASME International

Subject

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

Reference22 articles.

1. High Cycle Fatigue in Aircraft Gas Turbines—An Industry Prospective;Int. J. Fract.,1996

2. Flutter and Resonant Vibration Characteristics of Engine Blades;ASME J. Eng. Gas Turbines Power,1997

3. Asymmetrical Underplatform Dampers in Gas Turbine Bladings: Theory and Application,2004

4. Forced Response Prediction of Constrained and Unconstrained Structures Coupled Through Frictional Contacts;ASME J. Eng. Gas Turbines Power,2009

5. Forced Response Analysis of Integrally Bladed Disks With Friction Ring Dampers;J. Vib. Acoust.,2010

Cited by 3 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