Theoretical basis, concept and methodology of control and correction of turbojet engines thrust asymmetry

Abstract

Abstract The issues related to the study of the additional possibility of tightening the control of mutual conformity of the quality of turbojet engines in the conditions of their serial production and subsequent operation in the power plants of medium-haul aircraft and long-haul aircraft are considered. The purpose of the study is to develop new principles and corresponding digital methods for monitoring and correcting the thrust asymmetry of serial turbojet engines to improve the flight safety of medium-haul aircrafts and long-haul aircrafts with such engines. Methods of mathematical statistics and software modeling were used in the study. The results of the development of the concept and methodology of control and minimization of the thrust asymmetry of turbojet engines of one series in such conditions are presented.