Goal: knowledge acquisition about aircraft piston engine working process and design.

Task: study principles of the piston engine arrangement and operation, classification, working process and dynamics analysis.

Goal: knowledge acquisition about the analysis and partially the synthesis of the GTE control sys-tems.

Task: study the kinds and particularities of hydromechanical and digital different types GTE con-trol systems, mathematical models of control systems building, analysis of control systems properties.

Goal: formation of students' competencies related to the basics of determining the technical condition of aircraft and aircraft engines in general, their elements and functional systems.

Tasks: formation of knowledge:
- on general concepts of technical diagnostics of aircraft and aircraft engines;
- methods of solving diagnostic problems;
- characteristics of the main elements of the diagnostic system;
- methods and means of diagnosing aircraft and aircraft engines in general, their elements and functional systems.

Goal: modeling components and units of aircraft engines and power plants.

Task: study of methods and approaches of three-dimensional modeling of aircraft engine design in SolidWorks software package.

Goal: knowledge acquisition on aircraft engine design. The task is solved of initial images forming about engine elements and parts dynamics based on the theoretical and engineering disciplined that are studied previously.

Task: study theoretical course, make laboratory and practical works and the course project “Compressor of turbine engine”.

Goal: initial images forming about arrangement and strength of aircraft turbine engines, knowledge acquisition about the turbine engine components and parts composition and design.

Task: studying of the engine main components and structural units composition, design, operation conditions and loads, strength analysis.

Goal: provide the necessary knowledge on the use of aircraft engines and helicopters.

Task: study of parameters and characteristics of aircraft and helicopter engines.

Goal: forming knowledge about structure and operation of land gas turbine engine, features of GTE application in land power plants and instrumental methods of GTE condition control.

Task: The course is based on the knowledge from disciplines as Theory and Calculation of Impeller Machines, theory of air-jet engines, mechanics of materials and structures, design of machine elements, theory of mechanisms and machines, aviation materials science, fluid and gas dynamics, thermodynamics and heat transfer etc. The program shows logical interaction among the studied matters and partitions of the previously studied disciplines.

The purpose of the discipline is to provide students with the necessary knowledge about methods and means of diagnosing objects of aviation engineering, the regularities of changing their condition during operation and repair, assessing the suitability of machines and mechanisms for control of modern methods and tools.

The tasks of the discipline "Diagnostics and control systems of the technical state of aircraft and aircraft engines" are the mastering of the basic principles of practical methods of diagnosing aviation equipment and provisions of information provision of the process of controlling the technical condition of aviation equipment. For the diagnosis of aviation technology, computer technology and information processing techniques are used, which are based on the theory of pattern recognition and airworthiness control of aircraft and aviation engines, and the characteristics of control objects. The basic principles of constructing methods and means of technical diagnostics are applied.

After studying the course student

must know:

-     requirements for engines of different purposes, requirements of airworthiness standards;

-     static and dynamic loads acting on elements of gas turbine engines, characterized by changes in diagnostic parameters during the appearance of dangerous fluctuations or excess loads;

-     parameters controlled during the engine test and its operation, the ways of their registration;

-     modern methods and methods of processing diagnostic information, which is registered;

-     peculiarities of operation of engines and their systems;

-     diagnostic methods used in the operation of aircraft, as well as systems for controlling the technical condition of aircraft and aviation engines;

-     safety rules to be performed during the testing of functional systems of aircraft and aviation engines, measurement of diagnostic parameters;

-     the procedure for carrying out metrological inspections of means of control;

-     normative documentation on the issues of ensuring the accuracy of measurement parameters and calculations of errors and errors.

must be able to:

-     to solve tasks on processing of diagnostic parameters for estimation and forecasting of technical condition of aircraft, aviation engines and their systems;

-     to use methods and techniques for diagnosing aviation engineering in practice, to determine the causes of failure of elements of aircraft and aviation engines;

-     take into account the loading that acts on the aircraft from the engine, choose the types and characteristics of sensors and transducers;

-     to determine the list of engine parameters, probable indicators of diagnostics, to recognize the behavior of graphic dependencies of parameters in the presence and development of failures and malfunctions;

-     register, process and analyze diagnostic information, make conclusions about the state of the engine;

-     to solve practical and theoretical tasks of estimation and forecasting of technical condition of aircraft on the basis of data of onboard and ground systems;

-     to carry out the diagnostic parameters of the gas turbine engine to flight conditions and to one mode of operation, to smooth out the parameters and make conclusions about the state of engines and their aggregates;

-     monitor compliance with subordinate safety requirements when using diagnostic devices and devices.

Interdisciplinary calls: engineering analysis of the elements of the aviation technology, information technology of the security processes of the technical servicing of the avionics technology