Volume 41 Issue 5
May  2026
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BIAN Jie, WANG Siji, LIU Feichun. Research progress on axial force measurement technology for aero-engine rotors[J]. Journal of Aerospace Power, 2026, 41(5):20250197 doi: 10.13224/j.cnki.jasp.20250197
Citation: BIAN Jie, WANG Siji, LIU Feichun. Research progress on axial force measurement technology for aero-engine rotors[J]. Journal of Aerospace Power, 2026, 41(5):20250197 doi: 10.13224/j.cnki.jasp.20250197

Research progress on axial force measurement technology for aero-engine rotors

doi: 10.13224/j.cnki.jasp.20250197
  • Received Date: 2025-04-21
    Available Online: 2025-11-07
  • The measurement of axial force in aero-engine rotors is a critical method for obtaining rotor axial forces during engine pressure balance tests. The results of axial force measurements are of great significance for assessing rotor structural safety, aerodynamic design improvements, and axial force adjustments. The requirements for axial force measurement in aero-engine rotors were outlined, and the characteristics of common measurement methods, along with their applicability in aero-engine applications, were analyzed. Focusing on the structural features and operational conditions of aero-engines, the study elaborated on the fundamental principles and application cases of key measurement techniques, including airflow pressure measurement method, force-measuring ring measurement method, and squirrel cage elastic support measurement method. Additionally, it highlighted the current challenges in these techniques and discussed their future development trends and potential obstacles. Airflow pressure measurement method, force-measuring ring measurement method, and squirrel cage elastic support measurement method will continue to be utilized as mainstream methods for measuring axial force in aero-engine rotors in the future. Further improvements are required for measurement accuracy, stability, and sensitivity to address the shortcomings that currently affect their measurement effectiveness.

     

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