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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2017, Vol. 38 ›› Issue (11): 221111-221111.doi: 10.7527/S1000-6893.2017.221111

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

Theory and model for metal calendar life calculated by corrosion damage

ZHANG Fuze   

  1. Aeronautical Armaments Research Institute, Equipment Academy of Air Force, Beijing 100076, China
  • Received:2017-01-06 Revised:2017-05-22 Online:2017-11-15 Published:2017-05-21

Abstract:

The theory and model for the metal calendar life calculated by corrosion damage is discussed based on the research on the T-H curve and temperature and humidity spectrum of metal corrosion damage. This model proposed is able to calculate the metal's real calendar life when the corrosion T-H curve and the temperature and humidity spectrum in the real operational environment are provided. A comparison of the results of the calendar life calculation of 30CrMnSiA steel, with the experiment results in the real environment shows that the relative error of the steel is 17.5%. The comparison result shows that this model and method for calculating the metal calendar life is feasible.

Key words: corrosion damage, calendar life, temperature and humidity spectrum, T-H curve, calculation model

CLC Number: