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Dynamics Analysis and Experiment of Cantilever High-speed Rotor of Turbofan Engine
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Wei-jian NIE1, 2, Wang-qun DENG1, 2, Xiao-guang YANG3, Ge WANG1, 2, Wei YUAN1, 2
Science Technology and Engineering | 2025, 25(20) : 8707 - 8713
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Science Technology and Engineering | 2025, 25(20): 8707-8713
Papers·Aeronautics and Astronautics
Dynamics Analysis and Experiment of Cantilever High-speed Rotor of Turbofan Engine
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Wei-jian NIE1, 2, Wang-qun DENG1, 2, Xiao-guang YANG3, Ge WANG1, 2, Wei YUAN1, 2
Affiliations
  • 1 AECC Hunan Aviation Powerplant Research Institute, Zhuzhou 412002, China
  • 2 Key Laboratory of Aero-engine Vibration Technology, Aero Engine Corporation of China, Zhuzhou 412002, China
  • 3 School of Energy and Power Engineering, Bei Hang University, Beijing 100191, China
Published: 2025-07-18 doi: 10.12404/j.issn.1671-1815.2404704
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Two schemes, hollow shaft and solid shaft were proposed for the cantilever high-speed rotor of a turbofan engine during the structural design stage. Based on the beam element finite element method, rotor dynamic analysis models with hollow shaft and solid shaft were established, and critical speed and vibration mode calculations were carried out. The calculation results show that hollow shaft structure is suitable for the rotor. Then, an analysis was conducted on the sensitivity of the unbalance response of a rotor with a hollow shaft to the unbalance amount at the characteristic position, providing a basis for the selection of balance surfaces in high-speed dynamic balance test. Finally, the dynamic characteristics test of the simulated rotor with hollow shaft within the full speed range and the high-speed dynamic balance test research at the working speed were completed. The rotor smoothly crossed the two orders bending critical speed and safely operated to the working speed, verifying the rationality of the rotor’s hollow shaft structure and dynamic design. Compared with the experimental results, the calculation error of the established finite element model is not more than 4.08%, which well reflects the dynamic characteristics of the rotor. After high-speed dynamic balancing, the deflection of the rotor at the working speed is significantly reduced, not less than 33.33%. The research results provide reference and technical support for the structural, dynamic design, and experimental research of real low-pressure rotors, and has important engineering value.

turbofan engine  /  high-speed rotor  /  dynamics analysis  /  finite element  /  high-speed dynamic balance
Wei-jian NIE, Wang-qun DENG, Xiao-guang YANG, Ge WANG, Wei YUAN. Dynamics Analysis and Experiment of Cantilever High-speed Rotor of Turbofan Engine[J]. Science Technology and Engineering, 2025 , 25 (20) : 8707 -8713 . DOI: 10.12404/j.issn.1671-1815.2404704
Year 2025 volume 25 Issue 20
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Article Info
doi: 10.12404/j.issn.1671-1815.2404704
  • Receive Date:2024-06-24
  • Online Date:2026-05-13
  • Published:2025-07-18
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History
  • Received:2024-06-24
  • Revised:2025-04-10
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Affiliations
    1 AECC Hunan Aviation Powerplant Research Institute, Zhuzhou 412002, China
    2 Key Laboratory of Aero-engine Vibration Technology, Aero Engine Corporation of China, Zhuzhou 412002, China
    3 School of Energy and Power Engineering, Bei Hang University, Beijing 100191, China
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表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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