A Technique of Calculating a Load-Bearing Frame of Aircraft Passenger Seat Unit in Virtual Certification Tests
- 作者: Shabalin L.1, Sidorov I.1, Khaliulin V.1, Gorelov A.2
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隶属关系:
- Tupolev Kazan National Research Technical University
- Chistopol branch “Vostok”
- 期: 卷 61, 编号 4 (2018)
- 页面: 662-666
- 栏目: 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
如何引用文章
详细
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.
作者简介
L. Shabalin
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: leonid.shabalin@gmail.com
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111
I. Sidorov
Tupolev Kazan National Research Technical University
Email: leonid.shabalin@gmail.com
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111
V. Khaliulin
Tupolev Kazan National Research Technical University
Email: leonid.shabalin@gmail.com
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111
A. Gorelov
Chistopol branch “Vostok”
Email: leonid.shabalin@gmail.com
俄罗斯联邦, ul. Engel’sa 127a, Chistopol, Tatarstan, 422981