松装叶片燕尾型叶根干摩擦力模型及振动响应分析

徐自力 1; 上官博 2; 吴其林 3; 周显丁 3; 曹守洪 3

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松装叶片燕尾型叶根干摩擦力模型及振动响应分析

更新时间：2025-07-09

- 松装叶片燕尾型叶根干摩擦力模型及振动响应分析
- Dry Friction Force Model and Dynamic Response Analysis of Blades with Loosely Assembled Dovetail Attachment
- 西安交通大学学报 2009年43卷第7期页码：1-5+68
- 作者机构：
  
  西安交通大学强度与振动教育部重点实验室,西安,710049
- 作者简介：
- 基金信息：
  
  : 2008-09-25. 作者简介: 徐自力(1967-),男,副教授. 基金项目: 国家高技术研究发展计划资助项目(2007AA04Z1A1);国家自然科学基金资助项目(50675169);陕西省自然科学基础研究计划资助项目(2005E220)
- DOI：
  中图分类号： TK263.3;V231.92
- 网络首发：2009-07-10，
  
  纸质出版：2009
- 稿件说明：
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徐自力 1, 上官博 2, 吴其林 3, 等. 松装叶片燕尾型叶根干摩擦力模型及振动响应分析[J]. 西安交通大学学报, 2009,43(7):1-5+68.

Dry Friction Force Model and Dynamic Response Analysis of Blades with Loosely Assembled Dovetail Attachment[J]. 2009, 43(7): 1-5+68.
徐自力 1, 上官博 2, 吴其林 3, 等. 松装叶片燕尾型叶根干摩擦力模型及振动响应分析[J]. 西安交通大学学报, 2009,43(7):1-5+68. DOI：

Dry Friction Force Model and Dynamic Response Analysis of Blades with Loosely Assembled Dovetail Attachment[J]. 2009, 43(7): 1-5+68. DOI：

摘要

建立了叶片燕尾型叶根与轮缘接触面干摩擦力宏滑移迟滞模型

推导出了干摩擦力的数学表达式.采用一阶谐波平衡法和集中质量弹簧模型对燕尾型叶根叶片系统进行了强迫振动响应分析.计算结果表明:随着离心力增大

燕尾型叶根的等效刚度单调地增大

存在一个渐近值; 等效阻尼先增后减

存在最大值; 叶片系统的共振频率随离心力增大而增大

存在最优的离心力使叶片系统阻尼效果最佳.所提出的干摩擦力模型可应用于燕尾型叶根叶片振动响应分析.

Abstract

A macroslip model to determine the dry friction force on the contact interface between the blade dovetail attachment and the disk dovetail groove is presented

and then the mathematical expression of the dry friction force is obtained. The dynamic response of blades with loosely assembled dovetail attachment is analyzed using the lumped mass and spring model via the one-term harmonic balance method. The results show that the equivalent stiffness of loosely assembled dovetail attachment increases with the blade centrifugal force and then reaches a maximum value gradually. The equivalent damping increases at the beginning and then decreases with the increase of blade centrifugal force

and thus there exists a maximum value. The resonance frequency of the blade system rises with the blade centrifugal force and there exists an optimal centrifugal force at which the optimal effect of the dry friction damping can be achieved for the blade system.

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references

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YANG B D, MENQ C H. Characterization of contact kinematics and application to the design of wedge dampers in turbomachinery blading: Part 1 [J]. ASME Journal of Engineering for Gas Turbines and Power, 1998,120(2):410-417.

PETROV P E, EWINS D J. Advanced modeling of underplatform friction dampers for analysis of bladed disk vibration[J]. ASME Journal of Turbomachinery, 2007,129(1):143-150.

CHEN J J, MENQ C H. Prediction of periodic response of blades having 3D nonlinear shroud constraints[J]. ASME Journal of Engineering for Gas Turbines and Power, 2001,123(4):901-909.

任勇生, 朱德懋. 具有干摩擦阻尼叶片组振动理论与实验研究[J]. 航空学报,1994,15(11):1306-1314.

REN Yongsheng, ZHU Demao. The theoretical analysis and experimental investigation of vibration on blades with dry friction damping [J]. Acta Aeronautica Et Astrorautica Sinica, 1994,15(11):1306-1314.

徐自力,李辛毅,袁奇,等.用改进的摩擦模型计算带阻尼结构叶片的响应[J].西安交通大学学报,1998,32(1):42-44.

XU Zili, LI Xinyi, YUAN Qi, et al. Analysis of response of blades with friction damping interconnector using a new friction model [J]. Journal of Xi'an Jiaotong University, 1998, 32(1):42-44.

GRINFFIN J H. Friction damping of resonant stress in gas turbine engine airfoil[J]. ASME Journal of Engineering for Power, 1980,102(2):329-333.

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