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Sun Gear Fault Detection on an OH-58C Helicopter Transmission(30)

时间:2011-10-26 20:59来源:蓝天飞行翻译 作者:admin
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The 2nd method exploited the use of the kinematic sim-ulation program and the carefully monitored geometry of the planetary system during testing. The geometrically syn-chronized measurement method matches the signal’s re-sponse with the sun gear teeth in mesh and tallies a condi-tion indicator parameter. For this study, the sum of the sixth power of the amplitude was used. Consistent with SGVS -SASP , the best responses are obtained for the low-power cases. This is due to the increased vibration often associ-ated with lower powers. Plots showed that for the baseline case, there was no biasing of the values of each bin. For the sun gear with a single tooth spall, there was an emer-gence of mesh groups indicating increased damage, but the result, based on the condition indicator used, was inconclu-sive. The results for the multiple spall case clearly shows that the damage is on the sun gear.
References

1Stewart, R., “Some Useful Analysis Techniques for Gearbox Diagnostics,” Report MHM/R/10/77 -Machine Health Monitoring Group-Institute of Sound and Vibration Research, University of Southampton, July 1997.
2Zakrajsek, J., “A Review of Transmission Diagnostics Research at NASA Lewis Research Center,” NASA TM-106746, Vol. ARL-TR-599, 1994.

3Zakrajsek, J., Townsend, D., and Decker, H., “An Anal-ysis of Gear Fault Detection Methods as Applied to Pitting Fatigue Failure Data,” NASA TM-105950, Vol. AVSCOM TR-92-C-035, 1993.
4Decker, H., Handschuh, R., and Zakrajsek, J., “An En-hancement to the NA4 Gear Vibration Diagnostic Parame-ter,” NASA TM-106553, Vol. ARL-TR-389, 1994.
5Lewicki, D. G., Decker, H. J., and Shimski, J. T., “Devel-opment of a Full-Scale Transmission Testing Procedure to Evaluate Advanced Lubricants,” Technical Report NASA TP-3265, AVSCOM TR-91-C-026, NASA and the U.S. Army Aviation Systems Command, August 1992.
6Lewicki, D., Spievak, L., Wawrynek, P., Ingraffea, A., and Handschuh, R., “Consideration of Moving Tooth Load in Gear Crack Propagation Predictions,” NASA TM-2000-210227, July 2000.
 
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