Email this article Study of Dynamic Loads of Aircraft Bevel Gear Systems
- Authors: Suslin A.V.1, Pilla C.K.1
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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
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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.
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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
