Аванпроект ближньомагістрального літака вантажопідйомністю до 16 тонн

Abstract

Object of the design is a development of transportshortrange aircraft with cargo capacity up to16 tons. Subject of the design is theconceptual design of the upper cargo loading equipment such astelpher. Aim of the diploma work is the preliminary designof short range cargo aircraft and conceptual design of telpherto provide loading of the cargo and move it in horizontal direction. The method of design is analysis of the prototypes and selections of the most advanced decisions,the geometrical characteristics estimations, centre of gravity calculations, stress analysis of the drum axis. Practicalimplementation of the resultsis defined by the results of the designing of the short range aircraft with carrying capacity up to 16. The materials of the diploma could be recommended for theairlines,which carry out cargo transportation and for thestudents of the aviation specialities.