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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2021, Vol. 42 ›› Issue (9): 224482-224482.doi: 10.7527/S1000-6893.2020.24482

• Solid Mechanics and Vehicle Conceptual Design • Previous Articles     Next Articles

High-frequency fatigue infrared heat dissipation of new Al-Li alloy AA2198

XU Luopeng1,2,3,4,5, HU Shi6, LIU Qingsong1,3, WANG Qingyuan2,7   

  1. 1. School of Science, Civil Aviation Flight University of China, Guanghan 618307, China;
    2. Failure Mechanics&Engineering Disaster Prevention and Mitigation, Key Laboratory of Sichuan Province, Sichuan University, Chengdu 610065, China;
    3. Key Laboratory of Photonic and Optical Detection in Civil Aviation, Civil Aviation Flight University of China, Guanghan 618307, China;
    4. Polymer Research Institute, State Key Laboratory of Polymer Materials Engineering, Sichuan University, Chengdu 610065, China;
    5. Zhejiang Guanlin Machinery Inc., Anji 313310, China;
    6. College of Civil Aviation Safety Engineering, Guanghan 618307, China;
    7. School of Mechanical Engineering, Chengdu University, Chengdu 610106, China
  • Received:2020-07-02 Revised:2020-08-26 Published:2020-10-16
  • Supported by:
    Sichuan University Failure Mechanics & Engineering Disaster Prevention and Mitigation Key Laboratory of Sichuan Province Open Foundation (2020FMSCU02); CAFUC Foundation (J2020-060, JG2019-19-02, J2020-057); Undergraduate Training Programs for Innovation and Entrepreneurship (S201910624213); Natural Science Foundation of Sichuan Province (16ZB0034); National Natural Science Foundation of China (U1433127)

Abstract: An infrared imaging technology is used to study the rule of fatigue heat dissipation evolution of a new Al-Li alloy AA2198 under a high-frequency fatigue test condition of 100 Hz. It is found that fatigue heat dissipation on specimens shows fluctuation characteristics under different stress conditions, with its average temperature inclined to increase with the rise of the loading stresses. However, the temperature rise on specimens during fatigue test is not obvious, and the amplitudes of temperature variation under different stress condition is generally smaller than 1℃. The beginning of fatigue test and the moment of fatigue fracture occurrence are accompanied by a rapid temperature rise. An energy conversion theory model is proposed to explain the evolution process of fatigue heat dissipation. Meanwhile, the residual compressive stress formed on specimen subsurface during the shot peening process helps to intensify the fatigue crack closure, inhibiting the temperature rise on specimens.

Key words: new Al-Li alloy, infrared imaging technology, high-frequency fatigue test, infrared heat dissipation, shot peening

CLC Number: