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外部附件振动环境试验的正弦叠加随机载荷谱

李继世 王鑫 张大义 高东武 刘中华

李继世, 王鑫, 张大义, 等. 外部附件振动环境试验的正弦叠加随机载荷谱[J]. 航空动力学报, 2025, 40(8):20230747 doi: 10.13224/j.cnki.jasp.20230747
引用本文: 李继世, 王鑫, 张大义, 等. 外部附件振动环境试验的正弦叠加随机载荷谱[J]. 航空动力学报, 2025, 40(8):20230747 doi: 10.13224/j.cnki.jasp.20230747
LI Jishi, WANG Xin, ZHANG Dayi, et al. Sine-on-random vibration profile for vibration environment test of external accessories[J]. Journal of Aerospace Power, 2025, 40(8):20230747 doi: 10.13224/j.cnki.jasp.20230747
Citation: LI Jishi, WANG Xin, ZHANG Dayi, et al. Sine-on-random vibration profile for vibration environment test of external accessories[J]. Journal of Aerospace Power, 2025, 40(8):20230747 doi: 10.13224/j.cnki.jasp.20230747

外部附件振动环境试验的正弦叠加随机载荷谱

doi: 10.13224/j.cnki.jasp.20230747
基金项目: 国家科技重大专项(J2019-Ⅰ-0008-0008)
详细信息
    作者简介:

    李继世(1995-),男,博士生,研究方向为航空发动机振动分析及抑制。E-mail:lijishien@buaa.edu.cn

    通讯作者:

    张大义(1979-),男,教授、博士生导师,博士,研究方向为航空发动机振动分析及抑制。E-mail:dayi@buaa.edu.cn

  • 中图分类号: V233

Sine-on-random vibration profile for vibration environment test of external accessories

  • 摘要:

    为了有效开展航空发动机外部附件的振动环境试验,研究振动试验载荷谱的制订方法。通过分析发动机外部振动环境的实测数据,确认环境载荷为正弦和随机混合激励,且正弦激励具有阶次特征,提出制订多分量正弦扫频叠加随机载荷谱以实现真实振动环境的准确刻画。建立基于振动实测的正弦叠加随机载荷谱的制订流程,基于疲劳损伤等效理论,实现多分量扫频谱型的确认并与随机谱型匹配叠加。通过机匣外部4个区域的载荷谱制订实例分析,结果表明:叠加载荷谱相比单成分载荷谱能完整刻画真实环境载荷的混合激励特征,相比于现行标准/规范中规定的载荷谱,新编载荷谱的频域特征与真实环境载荷一致,且振动能级严格等于真实载荷的统计容限。

     

  • 图 1  振动试验载荷谱制订的一般流程

    Figure 1.  General process of vibration profile development for vibration test

    图 2  不同转速工况的振动环境实测上限谱

    Figure 2.  Measured upper limit spectrum of vibration environment under different rotational speed conditions

    图 3  正弦分量关于高/低压转子转频阶次跟踪

    Figure 3.  Order track of sine components by high/low pressure rotors rotation frequencies

    图 4  正弦阶次分量的频率-幅值曲线

    Figure 4.  Curve of frequency and amplitude of sine order components

    图 5  正弦叠加随机载荷谱制订流程

    Figure 5.  Developing process of sine-on-random vibration profile

    图 6  阶次分量$i$的扫频过程(单程升频扫频)

    Figure 6.  Sweeping process of order component $i$ (single pass upward frequency sweep)

    图 7  随机谱型与随机实测谱对比

    Figure 7.  Comparison between random profile and measured random spectrums

    图 8  各正弦激励阶次对应的扫频分量谱型

    Figure 8.  Sweeping components profiles corresponding to sine excitation orders

    图 9  保留的扫频分量和谱型的简化

    Figure 9.  Reserved sweep components and their patterns simplification

    图 10  中介机匣区域正弦叠加随机载荷谱对比振动环境实测谱以及现行载荷谱

    Figure 10.  Sine-on-random vibration profile in intermediate casing area comparing with measured environmental vibration spectrums and standards’ profiles

    图 11  风扇机匣区域正弦叠加随机载荷谱对比振动环境实测谱以及现行载荷谱

    Figure 11.  Sine-on-random vibration profile in fan casing area comparing with measured environmental vibration spectrums and standards’ profiles

    图 12  外涵机匣区域正弦叠加随机载荷谱对比振动环境实测谱以及现行载荷谱

    Figure 12.  Sine-on-random vibration profile in bypass duct casing area comparing with measured environmental vibration spectrums and standards’ profiles

    图 13  涡轮-加力机匣区域正弦叠加随机载荷谱对比振动环境实测谱以及现行载荷谱

    Figure 13.  Sine-on-random vibration profile in turbo-booster casing area comparing with measured environmental vibration spectrums and standards’ profiles

    图 14  载荷谱中各扫频分量的最大幅值

    Figure 14.  Maximum amplitude of each sweep component in vibration profile

    表  1  载荷谱制订相关信息表

    Table  1.   Information table related to vibration profile development

    转速工况
    n2/n2max)/%
    $T_k^{{\text{life}}}$/h ${R_k}$/g $T_k^{{\text{test}}}$/h
    79 0.0304 7.52 3.225×10−4
    80 0.0350 12.58 2.904×10−3
    82 0.0396 11.12 2.004×10−3
    83 0.0441 12.52 3.593×10−3
    84 0.0487 12.28 3.669×10−3
    85 0.0533 13.66 6.144×10−3
    86 0.0578 13.24 5.888×10−3
    87 0.0624 14.28 8.596×10−3
    88 0.0670 14.29 9.251×10−3
    89 0.0670 16.74 1.742×10−2
    91 0.0658 16.17 1.491×10−2
    92 0.0647 14.84 1.039×10−2
    93 0.0635 16.60 1.598×10−2
    95 0.0624 16.14 1.403×10−2
    96 0.0613 14.83 9.816×10−3
    97 0.0601 16.50 1.476×10−2
    98 0.0590 18.86 2.472×10−2
    100 0.0578 22.53 4.937×10−2
    下载: 导出CSV

    表  2  不同区域载荷谱随机部分的方均根值

    Table  2.   Root mean square of random sections in different area vibration profiles

    风扇机匣区域中介机匣区域外涵机匣区域涡轮-加力机匣区域军标[2]参考谱
    19.97g23.44g38.98g48.66g18.10g
    下载: 导出CSV
  • [1] 中国人民解放军总装备部. 军用装备实验室环境试验方法 第16部分: 振动试验: GJB 150.16A-2009[S]. 北京: 中国标准出版社, 2009.
    [2] MIL-STD-810H Committee. Environmental engineering considerations and laboratory tests: MIL-STD-810H[S]. Washington, US: Department of Defense, 2019: 333-547.
    [3] 《航空发动机设计手册》总编委会. 航空发动机设计手册 第17册: 载荷及机匣承力件强度分析[M]. 北京: 航空工业出版社, 2001: 202-207.
    [4] 刘海年, 刘志强, 张大义, 等. 航空发动机成品振动环境分析与试验载荷谱确定[J]. 航空维修与工程, 2013(4): 63-65. LIU Hainian, LIU Zhiqiang, ZHANG Dayi, et al. Study on the vibration environment characteristics and test spectrum of aero-engine accessories[J]. Aviation Maintenance & Engineering, 2013(4): 63-65. (in Chinese doi: 10.3969/j.issn.1672-0989.2013.04.027

    LIU Hainian, LIU Zhiqiang, ZHANG Dayi, et al. Study on the vibration environment characteristics and test spectrum of aero-engine accessories[J]. Aviation Maintenance & Engineering, 2013(4): 63-65. (in Chinese) doi: 10.3969/j.issn.1672-0989.2013.04.027
    [5] Radio Technical Commission for Aeronautics (RTCA). Environmental conditions and test procedures for airborne equipment section 8 Vibration: RTCA/DO-160G [S]. Washington, US: Radio Technical Commission for Aeronautics, 2010: 8-14.
    [6] 中华人民共和国工业和信息化部. 民用飞机机载设备环境条件和试验方法 第6部分: 振动试验: HB 6167.6-2014[S]. 北京: 中国标准出版社, 2014.
    [7] 中华人民共和国航空工业部. 机载设备环境条件及试验方法: 振动: HB 5830.5-1984[S]. 北京: 航空工业部第三〇一研究所, 1985.
    [8] 王志会, 刘海年, 翟月, 等. 航空发动机转速传感器振动试验载荷确定及应用[J]. 航空发动机, 2016, 42(3): 82-87. WANG Zhihui, LIU Hainian, ZHAI Yue, et al. Formulation and application for vibration test loading spectrum of an aeroengine revolution transmitter[J]. Aeroengine, 2016, 42(3): 82-87. (in Chinese

    WANG Zhihui, LIU Hainian, ZHAI Yue, et al. Formulation and application for vibration test loading spectrum of an aeroengine revolution transmitter[J]. Aeroengine, 2016, 42(3): 82-87. (in Chinese)
    [9] 王桂华, 刘海年, 张大义, 等. 航空发动机成附件振动环境试验剖面确定方法研究[J]. 推进技术, 2013, 34(8): 1101-1107. WANG Guihua, LIU Hainian, ZHANG Dayi, et al. Study on formulating method for vibration environment test profiles of aero-engine accessories[J]. Journal of Propulsion Technology, 2013, 34(8): 1101-1107. (in Chinese

    WANG Guihua, LIU Hainian, ZHANG Dayi, et al. Study on formulating method for vibration environment test profiles of aero-engine accessories[J]. Journal of Propulsion Technology, 2013, 34(8): 1101-1107. (in Chinese)
    [10] 李继世, 张大义, 黄爱萍, 等. 航空发动机外部附件振动试验载荷谱编制[J]. 航空发动机, 2021, 47(3): 53-59. LI Jishi, ZHANG Dayi, HUANG Aiping, et al. Compilation of vibration test load spectrum for aeroengine external accessory[J]. Aeroengine, 2021, 47(3): 53-59. (in Chinese

    LI Jishi, ZHANG Dayi, HUANG Aiping, et al. Compilation of vibration test load spectrum for aeroengine external accessory[J]. Aeroengine, 2021, 47(3): 53-59. (in Chinese)
    [11] ANGELI A, CORNELIS B, TRONCOSSI M. Synthesis of Sine-on-Random vibration profiles for accelerated life tests based on fatigue damage spectrum equivalence[J]. Mechanical Systems and Signal Processing, 2018, 103: 340-351. doi: 10.1016/j.ymssp.2017.10.022
    [12] MA Yi, CHEN Huaihai, ZHENG Ronghui. Control strategy for multi-axial swept sine on random mixed vibration testing[J]. Journal of Sound and Vibration, 2022, 527: 116846. doi: 10.1016/j.jsv.2022.116846
    [13] ZHENG Ronghui, CHEN Huaihai, VANDEPITTE D, et al. Generation of sine on random vibrations for multi-axial fatigue tests[J]. Mechanical Systems and Signal Processing, 2019, 126: 649-661. doi: 10.1016/j.ymssp.2019.02.046
    [14] MARQUES V, MEOLA T, DUARTE M. Development of sine-on-random accelerated tests applied to turbocharger electronics actuators[C]//Proceedings of the 22nd International Congress of Mechanical Engineering. Ribeirão Preto, Brazil: Brazilian Association of Mechanical Engineering, 2013.
    [15] CORNELIS B, MANZATO S, PEETERS B, et al. A mission synthesis procedure for sine-on-random excitations in a helicopter application[M]//Shock & Vibration, Aircraft/Aerospace, Energy Harvesting, Acoustics & Optics: Volume 9. Cham, US: Springer International Publishing, 2017: 197-209.
    [16] KIM C J. Accelerated sine-on-random vibration test method of ground vehicle components over conventional single mode excitation[J]. Applied Sciences, 2017, 7(8): 805. doi: 10.3390/app7080805
    [17] HALFPENNY A, KIHM F, PLASKITT R, et al. Vibration fatigue analysis of components on rotating machinery under sine and swept-sine-on-random loading[R]. Darmstadt, Germany: 5th Symposium on Structural Dynamics, 2017.
    [18] 中国航空综合技术研究所. 军用飞机平台环境数据分析与处理方法: HB 20236-2014[S]. 北京: 国家国防科技工业局, 2015.
    [19] 中国航空综合技术研究所. 军用飞机平台环境测量数据归纳方法: HB 20237-2014[S]. 北京: 国家国防科技工业局, 2015.
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  • 收稿日期:  2023-11-27
  • 网络出版日期:  2025-04-18

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