Analysis of the Impact of Fan Blade Geometric Deviations on the Strength Properties
- 作者: Arkhipov A.1, Volgina M.2, Matushkin A.1, Ravikovich Y.1, Kholobtsev D.1
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隶属关系:
- Moscow Aviation Institute
- PAO United Engine Corporation Saturn
- 期: 卷 62, 编号 4 (2019)
- 页面: 535-543
- 栏目: 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
如何引用文章
详细
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.
作者简介
A. Arkhipov
Moscow Aviation Institute
编辑信件的主要联系方式.
Email: nio203_mai@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
M. Volgina
PAO United Engine Corporation Saturn
Email: nio203_mai@mai.ru
俄罗斯联邦, ul. Lenina 163, Rybinsk, 152903
A. Matushkin
Moscow Aviation Institute
Email: nio203_mai@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
Yu. Ravikovich
Moscow Aviation Institute
Email: nio203_mai@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
D. Kholobtsev
Moscow Aviation Institute
Email: nio203_mai@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993