基于Virtual.Lab的燃油泵调节器结构的模态分析
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作者单位:

1.中国航空发动机集团有限公司,北京 100097;2.中国人民解放军陆军装备部航空军事代表局驻上海地区航空军事代表室,上海 200000;3.厦门大学机电工程系,厦门 361102

通讯作者:

何立强,男,高级工程师,E-mail:457743282@qq.com。

中图分类号:

O327


Modal Analysis of Fuel Pump Regulator Structure Based on Virtual.Lab
Author:
Affiliation:

1.Aero Engine Corporation of China,Beijing 100097, China;2.Aviation Military Representative Office of the Army Armament Department Aviation Military Representative Bureau in Shanghai,Shanghai 200000, China;3.Department of Mechanical and Electrical Engineering, Xiamen University, Xiamen 361102, China

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    摘要:

    在燃油泵调节器模态分析过程中,高集成装配体的模型简化和以螺钉连接为主的多种连接方式的有限元建模对分析结果的影响是一个难点。本文从实际工程应用角度出发,提出了关键子结构验证结合整体有限元建模的模态分析方法。首先,根据燃油泵调节器的结构特点对模型进行简化和网格处理;然后,开展了关键子结构壳体模态的仿真分析和实验测试,并在Virtual.Lab软件中对螺钉、密封圈、弹簧、紧配合和滑动配合等进行了连接方式的建模探索和多类型设置,解决了不同单元类型网格的过渡问题;在确保关键子结构有限元模型精度的前提下,最后开展了整体的有限元建模与模态特性研究,通过与实验结果的对比验证了仿真方法的可行性。结果表明:关键子结构法在处理复杂中小型结构装备的有限元分析上效果较佳,复杂结构有限元模型的连接处理方式不宜过多,否则求解不易收敛。多点约束法(Multipoint constraint method, MPC)能够高效处理非协调网格的过渡,适用小位移或变形的模型。

    Abstract:

    In the process of modal analysis of the fuel pump regulator, it is difficult to simplify the model of highly integrated assembly and establish finite element modeling of various connection modes mainly with screw connection, which have a great impact significant effect on the analysis results. From the perspective of practical engineering application, the modal analysis method of crucial substructure verification combined with global finite element modeling is proposed. Firstly, according to the structural characteristics of the fuel pump regulator, the model is simplified and meshed. Then, the crucial substructure shell modal analysis and experimental test are carried out. In the Virtual.Lab, different connection types are modeled, such as screw connection, seal ring connection, tight connection and sliding connection, and multi-type settings are carried out to solve the transition problems of different grid element types. Finally, under the premise of ensuring the accuracy of the key substructure finite element model, the overall finite element modeling and modal characteristics research are carried out, and the feasibility of the simulation method is verified by comparing with the experimental results. The results show that the crucial substructure method is better in dealing with the finite element analysis of complex small and medium-sized structural equipment, and the connection type of the finite element model of complex structure should not be too many, otherwise the solution is not easy to be converged. Multipoint constraint (MPC) method can deal with the transition of incompatible elements efficiently, and it is suitable for models with small displacement or deformation.

    表 4 燃油泵调节器计算模态和实验模态对比误差Table 4 Comparison error between calculation mode and experimental mode of fuel pump regulator
    表 2 壳体装配体模态分析结果(连接区域Rbe2等效)Table 2 Modal analysis results of shell assembly (Rbe2 equivalent in connection area)
    表 3 壳体计算模态和实验模态对比误差Table 3 Comparison error of shell calculation mode and experimental mode
    表 1 壳体装配体模态分析结果(连接区域弹簧等效)Table 1 Modal analysis results of shell assembly (spring equivalent in connection area)
    图1 调节器模型预处理流程Fig.1 Modulator model preprocessing process
    图2 简化后调节器模型Fig.2 Simplified rear regulator mode
    图3 螺钉连接简化示意图Fig.3 Simplified diagrammatic sketch of screw connection
    图4 密封圈连接简化示意图Fig.4 Simplified diagrammatic sketch of sealing ring connection
    图5 模态实验系统Fig.5 Modal experiment modal system
    图6 壳体模态实验线框模型Fig.6 Wireframe model of shell modal experiment
    图7 非协调网格MPC连接示意图Fig.7 MPC connection diagram of different element types
    图8 实体MPC连接(衬套和活门)Fig.8 Solid MPC connection (bushing and valve)
    图9 整机模态实验线框模型Fig.9 Wireframe model of complete equipment modal experiment
    图10 整机模态实验现场Fig.10 Complete equipment modal experiment site
    图11 第一阶模态振型对比Fig.11 Comparison of the first mode shapes
    图12 第三阶模态振型对比Fig.12 Comparison of the third mode shapes
    图13 第四阶模态振型对比Fig.13 Comparison of the fourth mode shapes
    图14 第八阶模态振型对比Fig.14 Comparison of the eighth mode shapes
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何立强,王鹏,胡学满.基于Virtual. Lab的燃油泵调节器结构的模态分析[J].南京航空航天大学学报,2021,53(4):537-545

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  • 收稿日期:2020-08-09
  • 最后修改日期:2021-03-08
  • 在线发布日期: 2021-08-05
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