A Technique of Calculating a Load-Bearing Frame of Aircraft Passenger Seat Unit in Virtual Certification Tests
- Авторы: Shabalin L.P.1, Sidorov I.N.1, Khaliulin V.I.1, Gorelov A.V.2
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Учреждения:
- Tupolev Kazan National Research Technical University
- Chistopol branch “Vostok”
- Выпуск: Том 61, № 4 (2018)
- Страницы: 662-666
- Раздел: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230765
- DOI: https://doi.org/10.3103/S1068799818040244
- ID: 230765
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Аннотация
An aircraft seat unit under static and dynamic types of loading is simulated. The technique offers the possibility to determine stressed state and strength of the unit under conditions corresponding to the certification tests of passenger seats. It takes into account the energy absorber (damper) and kinematic connections between load-bearing elements.
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Об авторах
L. Shabalin
Tupolev Kazan National Research Technical University
Автор, ответственный за переписку.
Email: leonid.shabalin@gmail.com
Россия, ul. Karla Marksa 10, Kazan, 420111
I. Sidorov
Tupolev Kazan National Research Technical University
Email: leonid.shabalin@gmail.com
Россия, ul. Karla Marksa 10, Kazan, 420111
V. Khaliulin
Tupolev Kazan National Research Technical University
Email: leonid.shabalin@gmail.com
Россия, ul. Karla Marksa 10, Kazan, 420111
A. Gorelov
Chistopol branch “Vostok”
Email: leonid.shabalin@gmail.com
Россия, ul. Engel’sa 127a, Chistopol, Tatarstan, 422981
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