X-Ray Diffraction Measurements for Inconel 718 Alloy Elements Created by Incremental Methods

The work presented is the result of the implementation of diffraction measurements: phase composition and stresses resulting from additive manufacturing process of nickel superalloy Inconel 718 components print. With the help of diffraction methodologies, the key parameters from the point of view of...

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Main Authors: Gadalińska Elżbieta, Żuk Paweł, Bujak Michał
Format: Article
Language:English
Published: Sciendo 2024-06-01
Series:Fatigue of Aircraft Structures
Subjects:
Online Access:https://doi.org/10.2478/fas-2023-0005
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author Gadalińska Elżbieta
Żuk Paweł
Bujak Michał
author_facet Gadalińska Elżbieta
Żuk Paweł
Bujak Michał
author_sort Gadalińska Elżbieta
collection DOAJ
description The work presented is the result of the implementation of diffraction measurements: phase composition and stresses resulting from additive manufacturing process of nickel superalloy Inconel 718 components print. With the help of diffraction methodologies, the key parameters from the point of view of the quality of prints and their strength were determined. The existence of individual phases in the material after printing was demonstrated, and the surface variation of the stress values was presented, showing its dependence on the geometry of the printed part – measurements were made at various points on the surface of samples with different geometries. In addition, the variation of the stress level was shown depending on the distance of the measurement point from the build platform on which the additive manufacturing process was carried out. Components were printed on the surface of a single build plate in order to study the effect of printing differently oriented samples with respect to the platform geometry, as well as the mutual effect of the temperature of samples printed first on the stress state of elements printed in subsequent steps of the procedure, and the effect of the temperature of elements printed later on the rate of temperature decrease, and consequently on the stress state, of elements printed first.
format Article
id doaj-art-f65b801e781241aab6b8e0a19fbd2682
institution Kabale University
issn 2300-7591
language English
publishDate 2024-06-01
publisher Sciendo
record_format Article
series Fatigue of Aircraft Structures
spelling doaj-art-f65b801e781241aab6b8e0a19fbd26822024-12-02T12:05:36ZengSciendoFatigue of Aircraft Structures2300-75912024-06-01202315588910.2478/fas-2023-0005X-Ray Diffraction Measurements for Inconel 718 Alloy Elements Created by Incremental MethodsGadalińska Elżbieta0Żuk Paweł1Bujak Michał21Łukasiewicz Research Network – Institute of Aviation, Al. Krakowska 110/114, 02-256Warsaw, Poland2GE Aerospace Poland, Al. Krakowska 110/114, 02-256Warsaw, Poland2GE Aerospace Poland, Al. Krakowska 110/114, 02-256Warsaw, PolandThe work presented is the result of the implementation of diffraction measurements: phase composition and stresses resulting from additive manufacturing process of nickel superalloy Inconel 718 components print. With the help of diffraction methodologies, the key parameters from the point of view of the quality of prints and their strength were determined. The existence of individual phases in the material after printing was demonstrated, and the surface variation of the stress values was presented, showing its dependence on the geometry of the printed part – measurements were made at various points on the surface of samples with different geometries. In addition, the variation of the stress level was shown depending on the distance of the measurement point from the build platform on which the additive manufacturing process was carried out. Components were printed on the surface of a single build plate in order to study the effect of printing differently oriented samples with respect to the platform geometry, as well as the mutual effect of the temperature of samples printed first on the stress state of elements printed in subsequent steps of the procedure, and the effect of the temperature of elements printed later on the rate of temperature decrease, and consequently on the stress state, of elements printed first.https://doi.org/10.2478/fas-2023-0005diffractionstressadditive manufacturingdmlminconel 718
spellingShingle Gadalińska Elżbieta
Żuk Paweł
Bujak Michał
X-Ray Diffraction Measurements for Inconel 718 Alloy Elements Created by Incremental Methods
Fatigue of Aircraft Structures
diffraction
stress
additive manufacturing
dmlm
inconel 718
title X-Ray Diffraction Measurements for Inconel 718 Alloy Elements Created by Incremental Methods
title_full X-Ray Diffraction Measurements for Inconel 718 Alloy Elements Created by Incremental Methods
title_fullStr X-Ray Diffraction Measurements for Inconel 718 Alloy Elements Created by Incremental Methods
title_full_unstemmed X-Ray Diffraction Measurements for Inconel 718 Alloy Elements Created by Incremental Methods
title_short X-Ray Diffraction Measurements for Inconel 718 Alloy Elements Created by Incremental Methods
title_sort x ray diffraction measurements for inconel 718 alloy elements created by incremental methods
topic diffraction
stress
additive manufacturing
dmlm
inconel 718
url https://doi.org/10.2478/fas-2023-0005
work_keys_str_mv AT gadalinskaelzbieta xraydiffractionmeasurementsforinconel718alloyelementscreatedbyincrementalmethods
AT zukpaweł xraydiffractionmeasurementsforinconel718alloyelementscreatedbyincrementalmethods
AT bujakmichał xraydiffractionmeasurementsforinconel718alloyelementscreatedbyincrementalmethods