Analysis of stress state in a root-airfoil transition zone of hollow wide chord fan blades
- Авторлар: Berdin V.K.1, Smyslov A.M.1, Berdin N.V.1, Luk’yanov V.V.1
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Мекемелер:
- Ufa State Aviation Technical University
- Шығарылым: Том 59, № 1 (2016)
- Беттер: 134-137
- Бөлім: 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
Дәйексөз келтіру
Аннотация
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.
Негізгі сөздер
Авторлар туралы
V. Berdin
Ufa State Aviation Technical University
Хат алмасуға жауапты Автор.
Email: berdinvk@mail.ru
Ресей, ul. Karla Marksa 12, Ufa, 450000
A. Smyslov
Ufa State Aviation Technical University
Email: berdinvk@mail.ru
Ресей, ul. Karla Marksa 12, Ufa, 450000
N. Berdin
Ufa State Aviation Technical University
Email: berdinvk@mail.ru
Ресей, ul. Karla Marksa 12, Ufa, 450000
V. Luk’yanov
Ufa State Aviation Technical University
Email: berdinvk@mail.ru
Ресей, ul. Karla Marksa 12, Ufa, 450000
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