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飞机发动机变阻尼变刚度吊挂系统隔振性能的计算分析

闫鹏嗣 马建敏

噪声与振动控制2018,Vol.38Issue(1):16-20,5.
噪声与振动控制2018,Vol.38Issue(1):16-20,5.DOI:10.3969/j.issn.1006-1355.2018.01.003

飞机发动机变阻尼变刚度吊挂系统隔振性能的计算分析

Calculation and Analysis of Vibration Isolation Performance of Airplane Engine Pylon Systems with Variable Damping and Stiffness

闫鹏嗣 1马建敏1

作者信息

  • 1. 复旦大学 航空航天系,上海200433
  • 折叠

摘要

Abstract

In order to study the vibration isolation performance of engine pylon systems,Voigt elements are added to the models of engine mounting joint and pylon connection rod respectively.By adjusting variable damping of the Voigt elements, the stiffness of the engine mounting joint and pylon connection rod can be altered so that two different engine-pylon-wing systems with variable damping and stiffness can be constituted. The mechanical models and dynamic equations of the two different systems are established. By solving the dynamic equations, the vibration transmission ratios of the systems are obtained.The calculation results show that a reasonable design can suppress the resonance peaks for the system with variable damping and stiffness and effectively reduce the vibration transmission ratio of the system in the non-resonance region.

关键词

振动与波/隔振/飞机发动机/吊挂系统/振动传递率/变阻尼变刚度

Key words

vibration and wave/vibration isolation/aero-engine/pylon system/vibration transmission ratio/variable damping and stiffness

分类

航空航天

引用本文复制引用

闫鹏嗣,马建敏..飞机发动机变阻尼变刚度吊挂系统隔振性能的计算分析[J].噪声与振动控制,2018,38(1):16-20,5.

噪声与振动控制

OACSCDCSTPCD

1006-1355

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