Email this article Study of Dynamic Loads of Aircraft Bevel Gear Systems
- Authors: Suslin A.V.1, Pilla C.K.1
-
Affiliations:
- Samara University
- Issue: Vol 61, No 3 (2018)
- Pages: 434-440
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/230628
- DOI: https://doi.org/10.3103/S1068799818030170
- ID: 230628
Cite item
Open Access
Access granted
Subscription Access
Abstract
This paper studies the dynamic loads of bevel gears with circular and straight teeth with the overlap factors less than two (εα < 2) and more than two (εα > 2). The advantages of the gears with straight teeth with εα > 2 are shown.
Keywords
About the authors
A. V. Suslin
Samara University
Author for correspondence.
Email: pillaclovis@gmail.com
Russian Federation, Moskovskoe sh. 34, Samara, 443086
C. K. Pilla
Samara University
Email: pillaclovis@gmail.com
Russian Federation, Moskovskoe sh. 34, Samara, 443086
Supplementary files
