Email this article Analysis of stress state in a root-airfoil transition zone of hollow wide chord fan blades
- Authors: Berdin V.K.1, Smyslov A.M.1, Berdin N.V.1, Luk’yanov V.V.1
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Affiliations:
- Ufa State Aviation Technical University
- Issue: Vol 59, No 1 (2016)
- Pages: 134-137
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/229618
- DOI: https://doi.org/10.3103/S1068799816010219
- ID: 229618
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Abstract
In this paper, under consideration is the complex approach to analyzing the operation of a simulator for the hollow blade made from the VT6 titanium alloy. The stress state parameters in the hollow-monolithic part transition zone of the cantilevered simulator at bending under the distributed load are determined.
About the authors
V. K. Berdin
Ufa State Aviation Technical University
Author for correspondence.
Email: berdinvk@mail.ru
Russian Federation, ul. Karla Marksa 12, Ufa, 450000
A. M. Smyslov
Ufa State Aviation Technical University
Email: berdinvk@mail.ru
Russian Federation, ul. Karla Marksa 12, Ufa, 450000
N. V. Berdin
Ufa State Aviation Technical University
Email: berdinvk@mail.ru
Russian Federation, ul. Karla Marksa 12, Ufa, 450000
V. V. Luk’yanov
Ufa State Aviation Technical University
Email: berdinvk@mail.ru
Russian Federation, ul. Karla Marksa 12, Ufa, 450000
