| Issue |
E3S Web Conf.
Volume 446, 2023
2nd International Conference on High-Speed Transport Development (HSTD 2023)
|
|
|---|---|---|
| Article Number | 03006 | |
| Number of page(s) | 8 | |
| Section | Design, Strength, New Materials | |
| DOI | https://doi.org/10.1051/e3sconf/202344603006 | |
| Published online | 10 November 2023 | |
Theoretical Model of the Methodology of Landing Gear Bracket Design Taking into Account the Adjusted Calculation for Shear Bolt Design
Moscow Aviation Institute (National Research University), Moscow, Russia
* Corresponding author: TitovEI@mai.ru
The subject of this paper is the methodology of main landing gear (MLG) design, in particular, the algorithm. The new algorithm considered in this paper is intended for designing modern structures of the MLG using a large number of methods of mathematical modelling of the stress-strain state and maximum autonomy of this process. The initial conditions of this algorithm are the Airworthiness Standards for Transport Category Airplanes (NLG25).
© The Authors, published by EDP Sciences, 2023
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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