Abstract
Methodological foundation and back-ground technology, providing function-oriented properties of the structure of gas turbine engine components, are presented. A composition of the components for an integrated multi-connected technological process, providing functionally oriented properties of the gas turbine engine structural units, is given. The article presents data for improving gas turbine engine serviceability on condition that equal operational properties are provided through functionally oriented properties of the components and subsystems due to special coatings.
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