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Effects of rim thickness on spur gear bending stress
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Reddy, S. K. Savage, M. Bibel, G. D. Handschuh, R. F. |
| Copyright Year | 1991 |
| Description | Thin rim gears find application in high-power, light-weight aircraft transmissions. Bending stresses in thin rim spur gear tooth fillets and root areas differ from the stresses in solid gears due to rim deformations. Rim thickness is a significant design parameter for these gears. To study this parameter, a finite element analysis was conducted on a segment of a thin rim gear. The rim thickness was varied and the location and magnitude of the maximum bending stresses reported. Design limits are discussed and compared with the results of other researchers. |
| File Size | 722875 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910014187 |
| Archival Resource Key | ark:/13960/t9x110w20 |
| Language | English |
| Publisher Date | 1991-01-01 |
| Access Restriction | Open |
| Subject Keyword | Mechanical Engineering Finite Element Method Thickness Position Location Gears Bending Fatigue Deformation Gear Teeth Fillets Design Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
