Analysis of kinematic of the aviation mechanisms in NX

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The article deals with kinematic analysis of structural elements of aircraft, including the mechanical components in order to optimize the structure and ensure the efficiency of the mechanism assembly with mating parts. An example of practical work in the framework of the university project together now. Supplied in purpose made, design changes are agreed with the design office. The results will be used to further work on the analysis and optimization of aircraft structures.

Cae-система, kinematic analysis, kinematics optimization, cae-system

Короткий адрес: https://sciup.org/148204741

IDR: 148204741

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