Study of Dynamic Loads of Aircraft Bevel Gear Systems
- Авторы: Suslin A.1, Pilla C.1
-
Учреждения:
- Samara University
- Выпуск: Том 61, № 3 (2018)
- Страницы: 434-440
- Раздел: 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
Цитировать
Аннотация
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.
Ключевые слова
Об авторах
A. Suslin
Samara University
Автор, ответственный за переписку.
Email: pillaclovis@gmail.com
Россия, Moskovskoe sh. 34, Samara, 443086
C. Pilla
Samara University
Email: pillaclovis@gmail.com
Россия, Moskovskoe sh. 34, Samara, 443086