Отправить статью по E-mail Analysis of the Impact of Fan Blade Geometric Deviations on the Strength Properties
- Авторы: Arkhipov A.1, Volgina M.2, Matushkin A.1, Ravikovich Y.1, Kholobtsev D.1
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Учреждения:
- Moscow Aviation Institute
- PAO United Engine Corporation Saturn
- Выпуск: Том 62, № 4 (2019)
- Страницы: 535-543
- Раздел: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/231113
- DOI: https://doi.org/10.3103/S1068799819040020
- ID: 231113
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Аннотация
The paper presents the results of calculating the strength properties for the fan blades of a regional aircraft gas turbine engine under consideration of manufacturing deviations. The models of blades with different geometric deviations on the airfoil being analyzed, the design model of the fan assembly, the strength properties being estimated, and the design scheme for a set of blades are described. An example of the calculation results is given.
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Об авторах
A. Arkhipov
Moscow Aviation Institute
Автор, ответственный за переписку.
Email: nio203_mai@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
M. Volgina
PAO United Engine Corporation Saturn
Email: nio203_mai@mai.ru
Россия, ul. Lenina 163, Rybinsk, 152903
A. Matushkin
Moscow Aviation Institute
Email: nio203_mai@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
Yu. Ravikovich
Moscow Aviation Institute
Email: nio203_mai@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
D. Kholobtsev
Moscow Aviation Institute
Email: nio203_mai@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
