Abstract

This article described the concept of a dropping mechanism for a special purpose quadcopter using graphical design methods. Also described is the information support for the creation of a dropping mechanism for special purpose quadcopters with wide modification possibilities, ease of maintenance of the dropping mechanism, and most importantly - with a low cost in the execution of the mechanism. The article described the developed and implemented dropping mechanism for special-purpose quadcopters with a wide range of modernization possibilities and fairly easy operational characteristics, namely: the dropping mechanism is designed to deliver cargo with a payload of up to 8 kg. During the implementation of the project, information support for the creation of a dropping mechanism for special-purpose quadcopters was described, in particular: a graphical calculation of the strength of the dropping mechanism under the conditions of payloads of different weights was performed and it was found that with a payload of up to 8 kg, the structure of the dropping mechanism can withstand the required load. A 3D model of the dropping mechanism was made, which combines ease of maintenance and wide possibilities for modernization. After the analysis of existing mechanisms, the basic form factor of the mechanism and its purpose were determined. Focusing on the calculations and construction of the developed dropping mechanism, an experimental model of the dropping mechanism was made using 3D printing.

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