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航空发动机关重件疲劳试验技术研究综述

陈鉴朋,  朱文慧,  谢里阳,  赵丙峰,  杨小玉,  许星元

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文章导航 > 航空动力学报  > 2026 >  41(3): 20240672
陈鉴朋, 朱文慧, 谢里阳, 等. 航空发动机关重件疲劳试验技术研究综述[J]. 航空动力学报, 2026, 41（3）：20240672 doi: 10.13224/j.cnki.jasp.20240672
引用本文: 陈鉴朋, 朱文慧, 谢里阳, 等. 航空发动机关重件疲劳试验技术研究综述[J]. 航空动力学报, 2026, 41（3）：20240672 doi: 10.13224/j.cnki.jasp.20240672
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CHEN Jianpeng, ZHU Wenhui, XIE Liyang, et al. Review of fatigue test techniques for key components of aero-engine[J]. Journal of Aerospace Power, 2026, 41（3）：20240672 doi: 10.13224/j.cnki.jasp.20240672
Citation: CHEN Jianpeng, ZHU Wenhui, XIE Liyang, et al. Review of fatigue test techniques for key components of aero-engine[J]. Journal of Aerospace Power, 2026, 41（3）：20240672 doi: 10.13224/j.cnki.jasp.20240672
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航空发动机关重件疲劳试验技术研究综述

doi: 10.13224/j.cnki.jasp.20240672
  • 1.

    东北大学 机械工程与自动化学院，沈阳 110819

  • 2.

    东北大学 航空动力装备振动及控制教育部重点实验室，沈阳 110819

  • 3.

    中国国际工程咨询有限公司 国防业务部，北京 100048

基金项目: 国家科技重大专项（J2019-Ⅳ-0002-0069，J2019-Ⅰ-0008-0008）
详细信息
    作者简介:

    陈鉴朋（1998-），男，博士生，主要从事机械结构疲劳寿命预测和系统概率风险分析。E-mail：jpchenneu@163.com

    通讯作者:

    谢里阳（1962-），男，教授，博士，主要从事机械结构疲劳寿命预测和系统概率风险分析。E-mail：lyxieneu@163.com

  • 中图分类号: V231.95

Review of fatigue test techniques for key components of aero-engine

  • 1.

    School of Mechanical Engineering and Automation，Northeastern University，Shenyang 110819，China

  • 2.

    Key Laboratory of Vibration and Control of Aero-Propulsion Systems，Ministry of Education，Northeastern University，Shenyang 110819，China

  • 3.

    Defense Business Department，China International Engineering Consulting Corporation，Beijing 100048，China

    摘要
  • 摘要:

    综述了航空发动机关重件疲劳试验技术和疲劳试验新技术的研究现状。梳理了航空发动机关重件疲劳试验技术的研究进展，分别对叶片、轮盘和轴的疲劳试验技术应用情况进行了阐述；归纳总结了可用于航机关重件疲劳试验的新技术的发展现状，包括非接触式状态测试技术、数字孪生技术和小样本试验数据统计分析技术；对目前航机关重件疲劳试验技术研究现状进行总结，从高精度高效率的疲劳损伤测试技术、数据驱动的部件级原位试验技术、数字孪生赋能的虚拟疲劳试验技术、智能稳健的小样本试验数据统计分析技术方面，对未来航空发动机关重件疲劳试验技术的发展方向做出展望。

     

    Abstract:

    The research status of fatigue test technology and new fatigue test technology of key components of aero-engine is reviewed. Firstly, the research progress of fatigue test technology of key components of aero-engine is reviewed, and the application of fatigue test technology of blades, disks and shafts is elaborated respectively. Secondly, the development status of new technologies that can be used for fatigue test of key components of aero-engine is summarized, including non-contact state test technology, digital twin technology and statistical analysis technology of small sample test data. Finally, the current research status of fatigue test technology of key components of aero-engine is summarized. The future development direction of fatigue test technology for key components of aero-engine is prospected from the high precision and efficient fatigue damage testing technology, data-driven component-level in-situ test technology, digital twin-enabled virtual fatigue test technology, intelligent and robust small sample test data statistical analysis technology.

     

    • HTML

  • 图 1  涡轮叶片热机械疲劳试验系统[19]

    Figure 1.  Thermo-mechanical fatigue test system for turbine blade[19]

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    图 2  涡轮叶片模拟试件[21]

    Figure 2.  Simulation specimen of turbine blade[21]

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    图 3  立式轮盘旋转试验台[29]

    Figure 3.  Vertical disk rotation test bench[29]

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    图 4  扭力涡轮盘加扭装置[36]

    Figure 4.  Torque turbine disk twisting device[36]

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    图 5  带梯度温度场的转子试验台[42]

    Figure 5.  Rotor test bench with gradient temperature field[42]

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    图 6  双轴加载试验件[46]

    Figure 6.  Biaxial loading specimen[46]

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    图 7  叶-盘组装结构试件[47]

    Figure 7.  Blade-disk assembly structure specimen[47]

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    图 8  轮盘榫槽局部结构试件[48]

    Figure 8.  Local structure specimen of disk mortise groove[48]

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    图 9  轮毂内孔局部结构试件及试验装置[49]

    Figure 9.  Local structure specimen and test device of wheel hub inner hole[49]

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    图 10  轮盘中心孔模拟试验件[51]

    Figure 10.  Simulated specimen of disk center hole[51]

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    图 11  轮盘低周疲劳模拟试验件[59]

    Figure 11.  Low cycle fatigue simulated specimen of disk[59]

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    图 12  轮盘锻造部件高温多轴疲劳试验[60]

    Figure 12.  High temperature multiaxial fatigue test of disk forging components[60]

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    图 13  涡轮盘本体试样试验[61]

    Figure 13.  Test of turbine disk body specimen[61]

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    图 14  涡轮盘本体取样示意图[62]

    Figure 14.  Schematic diagram of turbine disk body sampling[62]

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    图 15  发动机主轴立式综合加载试验器[69]

    Figure 15.  Vertical comprehensive loading tester for engine spindle[69]

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    图 16  发动机桨轴试验器[80]

    Figure 16.  Engine propeller shaft tester[80]

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    图 17  DIC非接触光学测量系统[81]

    Figure 17.  DIC non-contact optical measurement system[81]

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    图 18  谐振疲劳短裂纹显微图像采集系统[83]

    Figure 18.  Resonant fatigue short crack microscopic image acquisition system[83]

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    图 19  飞机旋翼DIC测试[98]

    Figure 19.  DIC test of aircraft rotor blade[98]

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    图 20  风电叶片DIC测试[103]

    Figure 20.  DIC test of wind turbine blade[103]

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    图 21  飞机机身DIC测试[105]

    Figure 21.  DIC test of fuselage[105]

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    图 22  高温超声疲劳试验系统[121]

    Figure 22.  High temperature ultrasonic fatigue test system[121]

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    图 23  复杂载荷加载力学性能原位测试装置[143]

    Figure 23.  In-situ test device for mechanical properties of complex load loading[143]

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    图 24  Inconel718镍基合金原位拉伸试验[144]

    Figure 24.  In-situ tensile test of Inconel718 nickel-based alloy[144]

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    图 25  基于同步辐射三维成像的功能集成型原位加载试验机[155]

    Figure 25.  Functional integrated in-situ loading testing machine based on synchrotron radiation three-dimensional imaging[155]

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    图 26  原位同步加速器UFT系统[163]

    Figure 26.  In-situ synchrotron UFT system[163]

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