Abstract
A generic gearbox containing one spur gear pair is examined using the statistical energy analysis with emphasis on the vibratory energy flow through rolling element bearings. A new analytical procedure has been developed to determine the associated coupling loss factor. Resulting formulation is applied to the NASA helicopter gear noise test facility. Vibro-acoustic predictions at the fundamental gear mesh frequency are found to be in reasonable agreement with measurements even though many simplifying assumptions are made. Such a model can be used for parametric design studies.
Original language | English (US) |
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Pages (from-to) | 63-69 |
Number of pages | 7 |
Journal | Noise Control Engineering Journal |
Volume | 37 |
Issue number | 2 |
DOIs | |
State | Published - 1991 |
Externally published | Yes |
All Science Journal Classification (ASJC) codes
- Building and Construction
- Automotive Engineering
- Aerospace Engineering
- Acoustics and Ultrasonics
- Mechanical Engineering
- Public Health, Environmental and Occupational Health
- Industrial and Manufacturing Engineering