Аванпроект вантажного ближньомагістрального літака вантажопідйомністю до 5,5 тон

Abstract

Object of the design is development of cargo short-range aircraft with cargo capacity 5,5 tons. Subject of the design – the conceptual design of the hook suspension improvement with stress-strain analysis of the hook. The aim of the diploma work is the preliminary design of the aircraft and its design characteristic estimation. The method of design is analysis of the prototypes and selections of the most advanced technical decisions, the geometrical characteristics estimation, centre of gravity calculations of the designing aircraft, stress-strain analysis of the hook and its modification. The diploma work contains drawings of the short-range aircraft with a carrying capacity of 5,5 tons, calculations and drawings of the aircraft layout and hook suspension design. The materials of the diploma could be recommended for the students of aviation specialties, for the aircraft operational companies, also it can be used for the design bureaus.