This paper explores the vibration spectra for planetary gear systems by studying a kinematic model of vibration and comparing the model with measurements of two helicopter transmissions made in flight. The model and flight data include systems with both uniformly and nonuniformly spaced planet gears. This model predicts vibration to occur only at frequencies that are integer multiples of the planet spacing repetition frequency and clustered around gear mesh harmonics. Vibration measurements show the model correctly predicts the frequencies with large components around the first several harmonics of the gear mesh frequency. Measurements do not confirm some of the more detailed features predicted by the model. Some features in the spectra from the numerically derived model can be used to separate the model data with and without planted faults. These features were not found useful for detecting faults in the vibration measurements of real gearboxes in flight due to added complexity in the spectra from real gearboxes.
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ASME 2003 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference
September 2–6, 2003
Chicago, Illinois, USA
Conference Sponsors:
- Design Engineering Division and Computers and Information in Engineering Division
ISBN:
0-7918-3702-5
PROCEEDINGS PAPER
Understanding Vibration Spectra of Planetary Gear Systems for Fault Detection
Marianne Mosher
Marianne Mosher
NASA Ames Research Center, Moffett Field, CA
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Marianne Mosher
NASA Ames Research Center, Moffett Field, CA
Paper No:
DETC2003/PTG-48082, pp. 645-652; 8 pages
Published Online:
June 23, 2008
Citation
Mosher, M. "Understanding Vibration Spectra of Planetary Gear Systems for Fault Detection." Proceedings of the ASME 2003 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. Volume 4: 9th International Power Transmission and Gearing Conference, Parts A and B. Chicago, Illinois, USA. September 2–6, 2003. pp. 645-652. ASME. https://doi.org/10.1115/DETC2003/PTG-48082
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