TRANSITION PROCESS REGULATOR OF SELF-ORGANIZING AVIATION ENGINE CONTROL SYSTEM
DOI:
https://doi.org/10.18372/1990-5548.65.14984Keywords:
Automatic control system, aviation gas turbine engine, transition process, adaptive regulator, self-organizingAbstract
The article considers the trends in the development of aviation engine construction, which are determined by the use of the latest advances in science to ensure high requirements for operational reliability, cost-effectiveness, environmental and safety. Each new generation of aviation gas turbine engines is characterized by a set of technologies implemented in production and put into operation, a short list of which allows to form the definition of generations of aviation gas turbine engines based on the analysis of world practical training of aviation engines. The main features of the process of designing adaptive automatic control system gas turbine engines in order to integrate the control of the workflow in the engine and flight modes to reflect the methodological, mathematical, cybernetic and informational side of research have been defined. The main control laws and structural schemes of automatic control system can be defined in the form of control programs on the maximum mode of operation of the engine, throttle modes, the mode of small gas, reception and release of gas, on the forced and transition modes.The use with a variable structure of the regulator for the investigation of transition processes automatic control system is proposed and the practical implementation of transition processes is presented.
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