Снижение вибрации малоразмерного летательного аппарата с конвертированным поршневым двигателем

Abstract

This article presents the application of the theory of vibration diagnostics and the theory of vibrations to the object of operation - a single-cylinder small-sized converted piston engine for domestic use, upgraded into an aircraft engine. The effect of vibration in the composition of small-sized aircraft - the «BENZYNYCH» series flying laboratory (LL) is considered. A comprehensive assessment is given of the possibility of using cheaper and comparable characteristics with specialized ADF converted piston engines on small aircraft using experimental measurements of vibration acceleration values by on-board vibration monitoring equipment during engine operation.