Registration Number
0222U000089,
0119U002248
, R & D reports
Title
Improvement of reliability and forecasting of the safe operational life of elements for turbine engines of aviation engineering
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Head
Duriagina Zoya A., Доктор технічних наук
Registration Date
02-01-2022
Organization
Lviv Polytechnic National University
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Titanium alloy VT8 grade and heat-resistant 13Х11Н2В2МФ (ЭИ961) steel used for the production of components of gas turbine engines in the initial state and after crack growth resistance tests were studied by transmission electron microscopy. Peculiarities of microstructure, morphology of structure, and character of phase and structural components distribution were determined. Defects of crystal structure, formation of dislocation inhomogeneities and local concentrators of internal stresses were identified using a JEM-200CX transmission electron microscope. The scalar density of dislocations was determined by the secant method. The distributions of deformations in the process zone determined by both the finite element method and the method of digital correlation of images were compared. It was shown that the use of a true deformation diagram in the finite element calculation algorithm ensures the correctness of numerical solutions. The minimum discrepancy between the calculated and experimental results of determining local deformations in the vicinity of the crack tip was obtained. A method for determining the operating life of blades of a compressor for gas turbine engines in the Matlab software environment was proposed and an algorithm for calculating the operating life of a blade made of 13H11N2V2MF (EI961) steel was developed.
Product Description
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Ivanytskyi Yaroslav L
Bohun Lidiya I
Vavrukh Valentyna I
Hrydova Halyna A
Kovbasiuk Taras M
Kulyk Volodymyr V
Lemishka Ihor A
Lenkovskyi Taras M
Lyutyy Pavlo Ya
Molkov Yuriy V
Tepla Tetiana L
Trostianchyn Andrii M
Filimonov Oleksiy S
Shevchuk Vira H
Shyshkovskyi Roman O
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2022-03-09
