Olejnik A. The concept and methods of lifetime depletion monitoring of gas turbine air-engine based on a dynamic identification of thermal and stress condition of main details

Українська версія

Thesis for the degree of Doctor of Science (DSc)

State registration number

0506U000669

Thesis Registration Form

0506U000669.pdf

Applicant for

Specialization

  • 05.07.05 - Двигуни та енергоустановки літальних апаратів

17-11-2006

Specialized Academic Board

Д 64.062.02

National Aerospace University "Kharkiv Aviation Institute"

Essay

The main concept of designing GTE lifetime depletion monitoring based on a dynamic identification of thermal and stress condition is proposed. It includes: structural and functional (non-parametric) identification a detail thermal and stress condition; evaluation of this conditions using a compact monitoring models; consideration of a non-stationary and non-linear factors: dynamics of temperature and temperature stresses, clearances, dependence of material properties on a temperature, heat exchange on a operational mode and so on; estimation of errors.

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Files

aref.doc

Диссертация Олейника.doc

Диссертация Олейника.doc

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