Email this article A Technique of Calculating a Load-Bearing Frame of Aircraft Passenger Seat Unit in Virtual Certification Tests
- Authors: Shabalin L.P.1, Sidorov I.N.1, Khaliulin V.I.1, Gorelov A.V.2
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Affiliations:
- Tupolev Kazan National Research Technical University
- Chistopol branch “Vostok”
- Issue: Vol 61, No 4 (2018)
- Pages: 662-666
- Section: 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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Abstract
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.
About the authors
L. P. Shabalin
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: leonid.shabalin@gmail.com
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
I. N. Sidorov
Tupolev Kazan National Research Technical University
Email: leonid.shabalin@gmail.com
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
V. I. Khaliulin
Tupolev Kazan National Research Technical University
Email: leonid.shabalin@gmail.com
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
A. V. Gorelov
Chistopol branch “Vostok”
Email: leonid.shabalin@gmail.com
Russian Federation, ul. Engel’sa 127a, Chistopol, Tatarstan, 422981
