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航空发动机两级燃油泵耦合振动特性分析
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四川省教育厅自然科学一般项目(18ZB0684);中国民用航空飞行学院面上项目(THZX2018-07);中央高校教育教学改革专项资金项目(E2019017)。


Coupled Vibration Characteristic Analysis of an Aero Engine Two-stage Fuel Pump
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    摘要:

    基于结构模态分析基本理论,建立两级燃油泵转动部件装配体结构耦合振动特性仿真分析方法。选取民航发动机上常用的两级燃油泵转动部件为分析对象,基于通用有限元软件平台建立其耦合振动特性分析的三维有限元模型,考虑工作转速范围内各零件间的实际连接情况,在能够线性求解的前提下,使相互接触零件的质量-刚度分布成为彼此振动的边界条件,同时又能计入相互接触零件间应力状态对振动特性的影响。利用该模型,计算了转动部件装配体结构在各转速工况下耦合振动的振型和频率,并结合其工作情况,画出共振特性曲线。分析发现了外载荷对结构耦合振动特性的影响规律及振动薄弱环节,在结构和维护上给出相应措施,以提高该两级燃油泵整体可靠性。

    Abstract:

    Based on basic theory of structural modal analysis,a simulation analysis method for coupled vibration characteristics of the rotating assembly structure of two-stage fuel pump was established.A rotating assembly of a two-stage fuel pump,which is commonly used on civil aviation engine,was selected as the analysis object,and a 3-D finite element model for the analysis of its coupled vibration characteristics was established based on the general finite element software platform.Considering the actual contact relationship between parts within working speed range,on the premise of linear solution,the mass-stiffness distribution of the parts in contact was made become the boundary condition of each others vibration,and at the same time,the influence of stress state between the parts in contact on the vibration characteristics was also taken into account.By using the model,the coupled vibration modes and frequencies of the rotating assembly structure under all rotating speed conditions were calculated.And combined with its working conditions,the Campbell curve was figured out.The results show the affect rules of the external loads on the coupled vibration characteristics of the rotating assembly,and the vibration weak areas.In order to improve the overall reliability of the two-stage fuel pump,some structural and maintenance measures were given.

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魏武国.航空发动机两级燃油泵耦合振动特性分析[J].机床与液压,2021,49(18):153-159.
WEI Wuguo. Coupled Vibration Characteristic Analysis of an Aero Engine Two-stage Fuel Pump[J]. Machine Tool & Hydraulics,2021,49(18):153-159

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  • 在线发布日期: 2023-03-21
  • 出版日期: 2021-09-28