航空发动机中的干摩擦阻尼器及其设计技术研究进展

李琳; 刘久周; 李超

doi:10.13224/j.cnki.jasp.2016.10.001

航空发动机中的干摩擦阻尼器及其设计技术研究进展

doi: 10.13224/j.cnki.jasp.2016.10.001

李琳^1,2,
刘久周^1,2,
李超^1,2

1. 北京航空航天大学能源与动力工程学院, 北京 100191;
2. 先进航空发动机协同创新中心, 北京 100191

详细信息

作者简介:
李琳(1956-),女,河北唐山人,教授、博士生导师,博士,主要从事航空发动机叶盘结构振动、流固耦合动力学分析等研究.

中图分类号: V231
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- 文章访问数: 1185
- HTML浏览量: 6
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- 被引次数: 0
出版历程
- 收稿日期: 2015-01-31
- 刊出日期: 2016-10-28

Review of the dry friction dampers in aero-engine and their design technologies

LI Lin^1,2,
LIU Jiu-zhou^1,2,
LI Chao^1,2

1. School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
2. Collaborative Innovation Center for Advanced Aero-Engine, Beijing 100191, China

摘要

摘要: 总结了航空发动机中的典型干摩擦阻尼器的结构形式及其工作原理，并给出了干摩擦模型以及接触运动模型的简化方法以及不同简化模型的优缺点和适用范围.分析了干摩擦阻尼系统响应分析的各种方法的特点，重点论述了近年来发展较为迅速的基于时频转换算法的高阶谐波平衡法的基本思想，并介绍了在进行时频转换分析过程中的弧长延拓法等关键技术.最后，论述了航空发动机中干摩擦阻尼器的设计和发展所面临的困难和未来的发展方向.
- 干摩擦阻尼器 /
- 干摩擦模型 /
- 接触运动模型 /
- 高阶谐波平衡法 /
- 时频转换算法
Abstract: Various typical dry friction dampers in aero-engine were summarized, and different typical dry friction models and contact kinematics models as well as their merit, demerit and range of application were introduced. Various computational methods to obtain the response of dry friction system were reviewed, and the multi-harmonic balance method combined with an alternating frequency-time domain method procedure was introduced in detail for particular interest. Furthemore, the key points of alternating frequency-time domain procedure, such as the arc-length continuation, were introduced. In the end, the difficulties and research directions in this research field were discussed.
- dry friction damper /
- dry friction model /
- contact kinematics model /
- multi-harmonic balance method /
- alternating frequency-time domain method

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参考文献(83)

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