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) |
|---|---|
| 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