Determination of aircraft part masses based on a parametric 3D model at the stage of technical proposals

Боргест Н. М.; N. M. Borgest; Громов А. А.; A. A. Gromov; Тарабаева А. И.; A. I. Tarabaeva

doi:10.18287/1998-6629-2013-0-1(39)-55-62

Determination of aircraft part masses based on a parametric 3D model at the stage of technical proposals

Authors: Borgest N.M.¹, Gromov A.A.¹, Tarabaeva A.I.²
Affiliations:
1. Samara State Aerospace University
2. «NIK – Samara» plc, Samara
Issue: Vol 12, No 1 (2013)
Pages: 55-62
Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
URL: https://journals.ssau.ru/vestnik/article/view/122
DOI: https://doi.org/10.18287/1998-6629-2013-0-1(39)-55-62
ID: 122

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Abstract

The paper presents a computer model of masses of the basic aircraft units at the stage of technical proposals in a 3D CAD system CATIA .Comparative analysis of the models of aircraft part masses is carried out. An algorithm of automatic aircraft plane balance is proposed on the basis of the 3D model developed.