FIELD: physics.
SUBSTANCE: invention relates to the field of engineering, and more specifically - to the gas turbine exhaust gas thermal field epicenter position evaluation method. Present invention can be used in creation, operation, control and monitoring of systems for various purposes, including complex technical systems, in which gas turbine units are integrated, used in power engineering, machine building, municipal services and other industries. Increase in inhomogeneity leads to burnout of guide vanes of the first stage of gas turbine and reduction of its efficiency.
EFFECT: disclosed method has high universality and flexibility and enables to achieve better results, in particular, based on obtained data, objective opinion on variation of degree of non-uniformity of temperature field.
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