Enviar artigo por via de e-mail Analysis of stress state in a root-airfoil transition zone of hollow wide chord fan blades
- Autores: Berdin V.1, Smyslov A.1, Berdin N.1, Luk’yanov V.1
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Afiliações:
- Ufa State Aviation Technical University
- Edição: Volume 59, Nº 1 (2016)
- Páginas: 134-137
- Seção: 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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Resumo
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.
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Sobre autores
V. Berdin
Ufa State Aviation Technical University
Autor responsável pela correspondência
Email: berdinvk@mail.ru
Rússia, ul. Karla Marksa 12, Ufa, 450000
A. Smyslov
Ufa State Aviation Technical University
Email: berdinvk@mail.ru
Rússia, ul. Karla Marksa 12, Ufa, 450000
N. Berdin
Ufa State Aviation Technical University
Email: berdinvk@mail.ru
Rússia, ul. Karla Marksa 12, Ufa, 450000
V. Luk’yanov
Ufa State Aviation Technical University
Email: berdinvk@mail.ru
Rússia, ul. Karla Marksa 12, Ufa, 450000
