ОПТИМИЗАЦИЯ СБОРКИ ПЕРЕДНЕГО ЛОНЖЕРОНА КРЫЛА ТРАНСПОРТНОГО САМОЛЕТА

Abstract

This article is to optimize the assembly of the front wing spar of a transport aircraft. Particular attention is paid to reducing the complexity, assembly cycle and other parameters that determine the efficiency of the process. According to experts, the domestic civil aviation fleet today is characterized as obsolete both morally and physically. The most important advantage of new products is the increased resource provided by the use of new materials, new design and technological solutions. One of such solutions is the widespread use of bent profiles from promising aluminum sheet materials. The presence of a cladding layer, a more uniform structure provides an increased resource. An important part of the production process of an aircraft manufacturing enterprise is assembly work, which largely determines the quality of the product. The main ways to increase the efficiency of assembly work, preparation of production, reduce costs is to increase the manufacturability of products, the creation of new means of production, the wider use of mechanization and automation, as well as the selection of optimal technological processes and means of equipping assembly work in technological design.