TAN JIAZHEN, BIAN XINXIAO, and WANG XIAOQUN, RELIABILITY OF AEROCRAFT GEAR FATIGUE STRENGTH, J. Univ. Sci. Technol. Beijing, 2(1995), No. 1, pp. 31-34.
Cite this article as:
TAN JIAZHEN, BIAN XINXIAO, and WANG XIAOQUN, RELIABILITY OF AEROCRAFT GEAR FATIGUE STRENGTH, J. Univ. Sci. Technol. Beijing, 2(1995), No. 1, pp. 31-34.
TAN JIAZHEN, BIAN XINXIAO, and WANG XIAOQUN, RELIABILITY OF AEROCRAFT GEAR FATIGUE STRENGTH, J. Univ. Sci. Technol. Beijing, 2(1995), No. 1, pp. 31-34.
Citation:
TAN JIAZHEN, BIAN XINXIAO, and WANG XIAOQUN, RELIABILITY OF AEROCRAFT GEAR FATIGUE STRENGTH, J. Univ. Sci. Technol. Beijing, 2(1995), No. 1, pp. 31-34.
With the method of group test, fourty pairs of carburization-quenching gears made from 16NCD13 steel for aerocraft were tested to research the contacting fatigue strength on tooth flank. As a result, the samples of fatigue life at the moments when the pitting appears and reaches failure criterion were obtained at four stressing levels respectively. The distribution rule of fatigue life were distinguished, and the distribution parameters were estimated by statistical analysis. Based on that, the R-S-N curves with confidence 95% of contacting fatigue on gear tooth flank were evaluated. Therefore, the basic data were provided for the reliability design of the gears and prediction of their life.
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