Affiliation:
1. AERMEC Lab, Department of Mechanical and Aerospace Engineering, Politecnico di Torino, Torino 10129, Italy e-mail:
Abstract
This paper furthers recent research by these authors. The starting point is the pre-optimization of solid dampers, which ensures that all dampers bound to “misbehave” are excluded since the early design stage. The authors now enlarge the scope of their investigations to explore those damper configurations selected inside the admissible design area. The purpose of the paper is to present a set of criteria apt to select a damper configuration which not only avoids unwanted situations, but in addition guarantees high performance under different design conditions. The analysis starts with the definition of a set of requirements a high performance damper should meet. In detail, the present investigation seeks to answer the following questions: in the low excitation regime, what is the frequency shift and the stiffening effect each damper can provide? for increasing excitation levels, which damper will start slipping sooner? in the high excitation regime, which damper provides the maximum dissipation? Like pre-optimization, it does not involve nonlinear finite element calculations, and unlike existing optimization procedures, is not linked to a specific set of blades the damper may be coupled to. The numerical prediction of the blade-damper coupled dynamics is here used only for validation purposes. The approach on which this paper rests is fully numerical; however, real contact parameters are taken from extensive experimental investigations made possible by those purposely developed test rigs which are the distinctive mark of the AERMEC Lab of Politecnico di Torino.
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Reference39 articles.
1. Friction Damping of Resonant Stresses in Gas Turbine Engine Airfoils;ASME J. Eng. Power,1980
2. Flutter and Resonant Vibration Characteristics of Engine Blades;ASME J. Eng. Gas Turbines Power,1997
3. Sextro, W., Popp, K., and Wolter, I., 1997, “Improved Reliability of Bladed Disks Due to Friction Dampers,” ASME Paper No. 97-GT-189.10.1115/97-GT-189
4. Characterization of Turbine Blade Friction Dampers;ASME J. Eng. Gas Turbines Power,2005
5. Effects of Damping and Varying Contact Area at Blade-Disk Joints in Forced Response Analysis of Bladed Disk Assemblies;ASME J. Turbomach.,2006
Cited by
4 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