ADVANCEMENT OF HELICAL GEAR DESIGN TECHNOLOGY
Abstract
An analytical and experimental study to evaluate factors for accurate appraisal of gear tooth bending strength is described. A design analysis consisting of a thorough review of current methods of calculating bending strength is presented. A dynamic test at high speed and an experimental evaluation of strain gage measured stresses are also presented for substantiation of the theoretical stress analysis. Results from a designed static fatigue test are presented to evaluate the effect of two geometric variables, i.e., pressure angle and helix angle, and two load positions. A final computer program is described to calculate bending stress as substantiated by design analysis, experimental evaluation, and static fatigue test. It is shown that the thorough consideration of geometric variables permits a more precise assessment of bending strength for life expectance of lightweight aircraft gearing.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1968
- Accession Number
- AD0675468
Entities
People
- Terry A. Lyon
- Wayne L. Mcintire
Organizations
- General Motors