Keyword: «automatic control system»

The article describes the original design of the torque meter on the output shaft of a serial helicopter engine.

The article substantiates the need to effectively limit the power of a helicopter gas turbine engine. The original design of the hydromechanical limiter is proposed.

The paper considers the assessment of the technical condition of the automatic flight control system ACS-1T-2B according to the data of the on-board recorder MSRP-64-2 in order to improve flight safety, combat readiness and reliability of control.

The article discusses the need to develop new ways to actively ensure flight safety by identifying negative factors and the subsequent development of means and systems to counter then.

The article describes the evolution of the Mi-8MT helicopters power plant from the initial version to the present day/ The main attention is paid to the improvement engines installed on increasingly modern versions of the Mi-8MT. The influence of new engine modifications on the characteristics of the most common helicopter in Russia is shown.