Mathematical modelling of аero-acoustic, fiber optic complex adaptive control
Abstract
Mathematical modelling of аero-acoustic, fiber optic complex adaptive control
Incoming article date: 21.07.2018In the present article the current state and the main problems of nondestructive control methods of working shovels of turbomachines are considered, scopes of nondestructive control methods in a flowing part of turbomachines are defined. The main control methods are considered; the reasons limiting possibilities of these methods are defined; the geometry of shovels, stream parameters, the main defects are defined; are considered hot and cold start-up; gasdynamic control methods are analysed; acoustic control methods, the systems of scanning of a cut of a nozzle are defined; the analysis of systems capable to exercise control of operability of a flowing part of turbomachines is carried out; the mathematical models describing acoustic processes in a flowing part of turbomachines and a way of their improvement are designated. The current state of works on creation of the methods and control devices aimed at improvement of metrological characteristics and expansion of functionality of an acoustic method of nondestructive control of working shovels of a flowing part of turbomachines on a nozzle cut is analysed. For control of working shovels of a flowing part of turbomachines it is necessary to use informative and reliable parameters in complex structure of their understanding. Defects in working shovels of a flowing part of turbomachines are found in operation at surveys by various devices therefore development of the minimum defect to greatest possible can happen for a short time interval that will lead to an emergency. The existing means of regular control прогар shovels don't come to light because of the depth or a sektornost for the reason that defects of motionless parts is insignificant a little influence vibration characteristics of the engine in general. Whereas defects in mobile parts can be revealed also sensors of vibration.
Keywords: distributed fiber systems, аero acoustic control, acoustic field, process simulation, recovery