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Данная работа посвящена разработке поршневого авиационного бензино-вого двигателя внутреннего сгорания мощностью 15кВт. В ходе выполнения работы рассчитаны: силы и моменты, возникающие в элементах двигателя, произведен анализ уравновешенности и выполнены расчеты прочности основных деталей поршневой группы двигателя. Произведены расчеты влияния высоты на мощность двигателя. На основании расчетов разработаны поперечный и продольный разрезы двигателя.
This work is devoted to the development of a piston aviation gasoline internal combustion engine with a capacity of 15 kW. In the course of the work, the following were calculated: the forces and moments arising in the engine elements, the balance analysis was carried out, and the strength calculations of the main parts of the engine piston group were performed. Calculations of the effect of altitude on engine power have been made. On the basis of calculations, the transverse and longitudinal sections of the engine have been developed.
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