Мақаланы E-mail арқылы жіберу A Technique of Calculating a Load-Bearing Frame of Aircraft Passenger Seat Unit in Virtual Certification Tests
- Авторлар: Shabalin L.1, Sidorov I.1, Khaliulin V.1, Gorelov A.2
-
Мекемелер:
- Tupolev Kazan National Research Technical University
- Chistopol branch “Vostok”
- Шығарылым: Том 61, № 4 (2018)
- Беттер: 662-666
- Бөлім: 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
Дәйексөз келтіру
Ашық рұқсат
Рұқсат берілді
Тек жазылушылар үшін
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.
Негізгі сөздер
Авторлар туралы
L. Shabalin
Tupolev Kazan National Research Technical University
Хат алмасуға жауапты Автор.
Email: leonid.shabalin@gmail.com
Ресей, ul. Karla Marksa 10, Kazan, 420111
I. Sidorov
Tupolev Kazan National Research Technical University
Email: leonid.shabalin@gmail.com
Ресей, ul. Karla Marksa 10, Kazan, 420111
V. Khaliulin
Tupolev Kazan National Research Technical University
Email: leonid.shabalin@gmail.com
Ресей, ul. Karla Marksa 10, Kazan, 420111
A. Gorelov
Chistopol branch “Vostok”
Email: leonid.shabalin@gmail.com
Ресей, ul. Engel’sa 127a, Chistopol, Tatarstan, 422981
