ANALYSIS OF TECHNICAL CONDITION ASSESSMENT OF GAS TURBINE BLADES WITH NON-DESTRUCTIVE METHODS

Structural components of gas turbines, particularly the blades, sustain a variety of damages during the operation process. The most frequent cause of these damages are the overheating and thermal fatigue of the material. A primary technique to assess condition of the blades is the metallographic exa...

Full description

Bibliographic Details
Main Author: Błachnio Józef
Format: Article
Language:English
Published: Sciendo 2013-12-01
Series:Acta Mechanica et Automatica
Subjects:
Online Access:https://doi.org/10.2478/ama-2013-0034
id doaj-0676123e05c845988e9253b17895f5a5
record_format Article
spelling doaj-0676123e05c845988e9253b17895f5a52021-09-06T19:41:05ZengSciendoActa Mechanica et Automatica 2300-53192013-12-017420320810.2478/ama-2013-0034ANALYSIS OF TECHNICAL CONDITION ASSESSMENT OF GAS TURBINE BLADES WITH NON-DESTRUCTIVE METHODSBłachnio Józef0Bialystok University of Technology, Faculty of Mechanical Engineering, ul. Wiejska 45C, 15-351 Bialystok, PolandStructural components of gas turbines, particularly the blades, sustain a variety of damages during the operation process. The most frequent cause of these damages are the overheating and thermal fatigue of the material. A primary technique to assess condition of the blades is the metallographic examination. In spite of the fact that metallographic analysis delivers much more information on the structure of examined blade material, it is a type of destructive test resulting in the destruction of the blade which makes further utilization of the item impossible. The paper has been intended to discuss non-destructive testing methods and to present capabilities of applying them to diagnose objectively changes in the microstructure of a turbine blade with computer software engaged to assist with the analyses. The following techniques are discussed: a visual method, based on the processing of images of the material surface in visible light, active thermography, based on the detection of infrared radiation, and the X-ray computed tomography. All these are new non-destructive methods of assessing technical condition of structural components of machines. They have been intensively developed at research centers worldwide, and in Poland. The computer-aided visual method of analyzing images enables diagnosis of the condition of turbine blades, without the necessity of dismantling of the turbine. On the other hand, the active thermography and the X-ray computed tomography, although more sensitive and more reliable, can both be used with the blades dismounted from the turbine. If applied in a complex way, the non-destructive methods presented in this paper, are expected to increase significantly probability of detecting changes in the blade’s condition, which in turn would be advantageous to reliability and safety of gas turbine servicehttps://doi.org/10.2478/ama-2013-0034gas turbinebladediagnosingtechnical condition
collection DOAJ
language English
format Article
sources DOAJ
author Błachnio Józef
spellingShingle Błachnio Józef
ANALYSIS OF TECHNICAL CONDITION ASSESSMENT OF GAS TURBINE BLADES WITH NON-DESTRUCTIVE METHODS
Acta Mechanica et Automatica
gas turbine
blade
diagnosing
technical condition
author_facet Błachnio Józef
author_sort Błachnio Józef
title ANALYSIS OF TECHNICAL CONDITION ASSESSMENT OF GAS TURBINE BLADES WITH NON-DESTRUCTIVE METHODS
title_short ANALYSIS OF TECHNICAL CONDITION ASSESSMENT OF GAS TURBINE BLADES WITH NON-DESTRUCTIVE METHODS
title_full ANALYSIS OF TECHNICAL CONDITION ASSESSMENT OF GAS TURBINE BLADES WITH NON-DESTRUCTIVE METHODS
title_fullStr ANALYSIS OF TECHNICAL CONDITION ASSESSMENT OF GAS TURBINE BLADES WITH NON-DESTRUCTIVE METHODS
title_full_unstemmed ANALYSIS OF TECHNICAL CONDITION ASSESSMENT OF GAS TURBINE BLADES WITH NON-DESTRUCTIVE METHODS
title_sort analysis of technical condition assessment of gas turbine blades with non-destructive methods
publisher Sciendo
series Acta Mechanica et Automatica
issn 2300-5319
publishDate 2013-12-01
description Structural components of gas turbines, particularly the blades, sustain a variety of damages during the operation process. The most frequent cause of these damages are the overheating and thermal fatigue of the material. A primary technique to assess condition of the blades is the metallographic examination. In spite of the fact that metallographic analysis delivers much more information on the structure of examined blade material, it is a type of destructive test resulting in the destruction of the blade which makes further utilization of the item impossible. The paper has been intended to discuss non-destructive testing methods and to present capabilities of applying them to diagnose objectively changes in the microstructure of a turbine blade with computer software engaged to assist with the analyses. The following techniques are discussed: a visual method, based on the processing of images of the material surface in visible light, active thermography, based on the detection of infrared radiation, and the X-ray computed tomography. All these are new non-destructive methods of assessing technical condition of structural components of machines. They have been intensively developed at research centers worldwide, and in Poland. The computer-aided visual method of analyzing images enables diagnosis of the condition of turbine blades, without the necessity of dismantling of the turbine. On the other hand, the active thermography and the X-ray computed tomography, although more sensitive and more reliable, can both be used with the blades dismounted from the turbine. If applied in a complex way, the non-destructive methods presented in this paper, are expected to increase significantly probability of detecting changes in the blade’s condition, which in turn would be advantageous to reliability and safety of gas turbine service
topic gas turbine
blade
diagnosing
technical condition
url https://doi.org/10.2478/ama-2013-0034
work_keys_str_mv AT błachniojozef analysisoftechnicalconditionassessmentofgasturbinebladeswithnondestructivemethods
_version_ 1717767058030067712