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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1985, Vol. 6 ›› Issue (5): 474-477.

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AN AUTOMATED FATIGUE TEST SYSTEM

Lu Qixin, Wu Tieying   

  1. Nanjing Aeronautical Institute
  • Received:1985-01-23 Revised:1900-01-01 Online:1985-10-25 Published:1985-10-25

Abstract: This paper deals with design and operation of an automated fatigue test system with closed-cycle control. It compares favourably with previous systems with open-cycle load control in amplitude precision. The major advantage of its advanced core device YZP-2 is a highly uniform bending load provided by eliminating the perturbing effect of excitation. This electronically servo-controlled system with eddy-current transduser gives automatically the blade fatigue failure signal by monitoring frequency transition of the test specimen so as to provide precise test data for S-N curves. This new system works satisfactorily over 1000 hours in our laboratory.