Theoretical Model of the Methodology of Landing Gear Bracket Design Taking into Account the Adjusted Calculation for Shear Bolt Design

Abstract

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).