主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
发动机燃油泵附件的管路动力学等效设计及实现
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作者单位:

1.中国飞机强度研究所;2.贵州红林航空动力控制科技有限公司

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中图分类号:

V219

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Dynamic equivalent design and realization of the pipeline of engine fuel pump accessory
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Affiliation:

Aircraft Strength Research Institute of China,Aviation

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    摘要:

    燃油泵附件的管路空间构型复杂,在振动环境试验中直接模拟难以实现。为满足试验要求,采用SEREP 方法对管路进行动力学等效设计,选取管路上特定结点为主自由度,并将原管路模型缩减至主自由度模型上,得到缩减质量和刚度矩阵;对子振型矩阵用SVD 分解,使得缩减质量和刚度矩阵进一步简化,得到低阶管路模型的新缩减质量刚度矩阵参数;提出“质量球—梁弹簧”结构模型,分别用“质量球”和“梁弹簧”来映射缩减的质量和刚度矩阵,进而可确定等效设计加工参数;最后通过实例验证了等效设计方法的可行性。结果表明:等效管路与原管路的第一阶频率误差大多数在10% 以内,满足工程应用要求。

    Abstract:

    The pipeline space configuration of fuel pump accessory is complex, and it is difficult to simulate directly in vibration environment test. In this paper, the system equivalent reduction expansion process(SEREP) is used for the dynamic equivalent design of the pipelines to meet the test requirements. Select the specific nodes on the pipeline as the main DOFs, and reduce the original pipeline model to the main DOFs model, then the reduced mass and stiffness matrix is obtained. The sub-mode matrix is decomposed by SVD to further simplify the reduced mass and stiffness matrix, then the new reduced mass and stiffness matrixes of low-order pipeline model are obtained. The "mass ball-beam spring" structure model is proposed, , which maps the reduced mass and stiffness matrices using "mass ball" and "beam spring" respectively, thereby determining equivalent design and processing parameters. Finally, the implementation of the equivalent design method was verified through examples, and the first frequency error between the equivalent pipeline and the original pipeline was mostly within 10%, meeting the requirements of engineering applications.

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刘继军,李凯翔,胡文佳.发动机燃油泵附件的管路动力学等效设计及实现[J].航空工程进展,2024,15(5):155-161

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历史
  • 收稿日期:2023-11-11
  • 最后修改日期:2024-05-20
  • 录用日期:2024-05-23
  • 在线发布日期: 2024-09-02
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