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Surface Modification and its Influence on the Microstructure and Creep Resistance of Nickel Based Superalloy René 77 / Modyfikacja Powierzchniowa Oraz Jej Wpływ Na Mikrostrukture I Wytrzymałosc Na Pełzanie Odlewów Z Nadstopu Niklu Ren´E 77

100%

Sieniawski J., Zielinska M.

Archives of Metallurgy and Materials

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2013

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issue 1

2

Microstructure and mechanical properties of C355.0 cast aluminium alloy

100%

Mrówka-Nowotnik G., Sieniawski J.

Archives of Materials Science and Engineering

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2011

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vol. 47

3

Numerical Approach to Predicting Thermodynamic Properties of Ternary Al-Ni-Pt Alloys

81%

Zagula-Yavorska M., Romanowska J., Kotowski S., Sieniawski J.

Acta Physica Polonica A

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2015

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vol. 127

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issue 6

1573-1576

EN

Thermodynamic properties of ternary Al-Ni-Pt system, such as ^{ex}G_{AlNiPt}, μ_{Al(AlNiPt)}, μ_{Ni(AlNiPt)}, and μ_{Pt(AlNiPt)} at 1373 K were predicted on the basis of thermodynamic properties of binary systems included in the investigated ternary system. The idea of predicting ^{ex}G_{AlNiPt} values was regarded as calculation of values of ^{ex}G function inside a certain area (a Gibbs triangle) unless all boundary conditions, that is values of ^{ex}G on all legs of the triangle are known (^{ex}G_{AlNi}, ^{ex}G_{AlPt}, ^{ex}G_{NiPt}). This approach is contrary to finding the function value outside a certain area, if the function value inside this area is known. ^{ex}G and L_{ijk} ternary interaction parameters in the Muggianu extension of the Redlich-Kister formalism are calculated numerically using the Mathematica program. The accepted values of the third component concentration x_{x} differed from 0.01 to 0.1 mol fraction. Values of L parameters in the Redlich-Kister formula vary for different x_{x} values, the ^{0}L_{AlNiPt} value in particular. Values of thermodynamic functions: ^{ex}G_{AlNiPt}, μ_{Al(AlNiPt)}, μ_{Ni(AlNiPt)} and μ_{Pt(AlNiPt)} do not differ significantly for different x_{x} values. The choice of x_{x} value does not influence the accuracy of calculations.

4

Microstructural Characterization Of Quenched And Plastically Deformed Two-Phase α+β Titanium Alloys

81%

Motyka M., Sieniawski J., Ziaja W., Mrówka-Nowotnik G.

Archives of Metallurgy and Materials

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2015

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issue 3

5

Numerical Simulation of Directional Solidification Process of Single Crystal Ni- Based Superalloy Casting

81%

Sieniawski J., Szeliga D., Kubiak K.

Archives of Foundry Engineering

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2017

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vol. 17

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issue 2

6

Primary Creep Behaviour of Two-Phase Titanium Alloy with Various Microstructure

81%

Ziaja W., Sieniawski J., Kubiak K., Motyka M.

Archives of Metallurgy and Materials

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2016

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issue 2

7

Functional Properties of Aluminide Layer Deposited on Inconel 713 LC Ni-based Superalloy in the CVD Process Właściwości Użytkowe Warstwy Aluminidkowej Wytworzonej W Procesie CVD Na Stopie Niklu Inconel 713 LC

81%

Yavorska M., Sieniawski J., Zielińska M.

Archives of Metallurgy and Materials

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2011

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issue 1

8

Influence of Chemical Composition of Nickel Based Superalloy on the Formation of Aluminide Coatings Wpływ Składu Chemicznego Nadstopu Niklu Na Budowę Warstwy Aluminidkowej

81%

Zielińska M., Sieniawski J., Yavorska M., Motyka M.

Archives of Metallurgy and Materials

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2011

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issue 1

9

Crystal Perfection Studies of Single Crystal Superalloy Turbine Blades by X-Ray Diffraction Methods

81%

Gancarczyk K., Albrecht R., Bogdanowicz W., Sieniawski J.

Acta Physica Polonica A

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2016

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vol. 130

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issue 4

1088-1090

EN

In the paper the crystal structure of single crystal CMSX-4 blade casts, applied in high pressure turbine of aircraft engines was analyzed. The longitudinal section of blade, cast at withdrawal rate of 3 mm/min was used as a sample. During the conducted research, following X-ray diffraction methods were applied: EFG Ω-scan, Auleytner X-ray topography and analysis of diffraction reflex profile ("rocking curve"). The authors determined crystal orientation in entire blade casts on the basis of set criterion concerning values of angle α - deviation of [001] direction from the direction of cast withdrawal. Conclusions concerning the crystal structure quality of the blade were drawn based on results from three different research methods. Local changes in crystal orientation on the surface of blade cast, also areas with significant structure defect degree and the presence of internal stresses were characterized.

10

Microstructure and Oxidation Resistance of an Aluminide Coating on the Nickel Based Superalloy Mar M247 Deposited by the CVD Aluminizing Process

81%

Zielińska M., Sieniawski J., Zagula-Yavorska M., Filip R.

Archives of Metallurgy and Materials

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2013

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issue 3

11

Some Properties of Platinum and Palladium Modified Aluminide Coatings Deposited by CVD Method on Nickel-Base Superalloys

81%

Zagula-Yavorska M., Sieniawski J., Gancarczyk T.

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issue 2

12

Evaluation of the Cutting Force Components and the Surface Roughness in the Milling Process of Micro- and Nanocrystalline Titanium

81%

Sieniawski J., Habrat W., Motyka M., Topolski K.

Archives of Metallurgy and Materials

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2016

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issue 3

13

Mould Walls Inclination and Dendritic Morphology of CMSX-4 Blades Airfoils

81%

Krawczyk J., Bogdanowicz W., Sieniawski J., Kubiak K.

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EN

The airfoils of single-crystalline turbine blades were studied. The blades made of industrial CMSX-4 superalloy were obtained by the Bridgman technique. Five different withdrawal rates (1-5 mm/min) were used. Series of as-cast samples were prepared by cutting the airfoils at different distances from the blade root. The metallographic sections, prepared for each cutting planes, were subjected to scanning electron microscopy observations and Laue diffraction studies. Macrostructure images of whole area of airfoil cross-sections were obtained by stitching several obtained SEM images. Morphology of dendrites in different area of cross-sections were analysed. The crystal orientation of each sample were determined by analysis of Laue pattern. It was found that the morphology of dendrites changes in the area, where the dendrite growth is limited by inclined mould walls.

14

Characterization of Casting Defects in the Single Crystal Turbine Blade Airfoil

81%

Albrecht R., Bogdanowicz W., Sieniawski J., Kubiak K.

Acta Physica Polonica A

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2016

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vol. 130

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issue 4

1091-1093

EN

In the paper turbine blades made from single crystal CMSX-4 superalloy were investigated by X-ray diffraction methods (topography, Ω-scan mapping) complemented by scanning electron microscopy observations. By the X-ray diffraction topography method several misorientation defects were visualized as well as dendrites arrangement. It was discussed that tip of the airfoil and thin walled area of the turbine blades located near the trailing edge can accumulate more growth defects than other airfoil part, due to the complex shape of the mould.

15

Hot Deformation Of 6xxx Series Aluminium Alloys

71%

Sieniawski J., Mrówka-Nowotnik G., Kotowski S., Nowotnik A., Motyka M.

Archives of Metallurgy and Materials

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2015

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issue 2

16

The Ni-Al-Hf Multiphase Diffusion

71%

Sieniawski J., Romanowska J., Wierzba B., Markowski J., Zagula-Yavorska M.

Archives of Metallurgy and Materials

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2016

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issue 2

17

The Control of Solidification Kinetics of the Vacuum-cast Thin-wall Nickel-based Superalloys by Changing the Geometrical Characteristics of the Ceramic Mold

71%

Cygan R., Sieniawski J., Szeliga D., Suchy J. S., Rokicki P.

Archives of Foundry Engineering

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2013

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issue 4

18

Dendrite Growth in Selector-Root Area of Single Crystal CMSX-4 Turbine Blades

71%

Bogdanowicz W., Tondos A., Krawczyk J., Albrecht R., Sieniawski J.

Acta Physica Polonica A

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2016

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vol. 130

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issue 4

1107-1109

EN

The single crystal turbine blades made of CMSX-4 nickel-based superalloy were studied. The turbine blades were obtained by the Bridgman technique with withdrawal rate of 5 mm/min. The samples, cut-off from root part of blades and containing the fragment of the selector, were studied. The effect of selector geometry on the dendrites growth and defects formation in the selector-root area of the blade were analyzed. The Laue diffraction, scanning electron microscopy, and X-ray diffraction topography were applied. It was found that, during crystallization of the selector, the dendrite cores, after reaching the surface of mould, may bend, if the angle between dendrite cores and the mould surface was equal to 12°. When the angle was equal to 24° the growth of dendrites has been stopped. It can be stated that the defects, which appeared in the selector were inherited by the root part.

19

Analysis of CMSX-4 Single-Crystalline Turbine Blades Root by Electron and X-Ray Diffraction Methods

71%

Krawczyk J., Zubko M., Bogdanowicz W., Tondos A., Sieniawski J.

Acta Physica Polonica A

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2016

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vol. 130

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issue 4

1104-1106

EN

The root of single-crystalline turbine blade made of CMSX-4 superalloy were studied. The studied blade was produced by the Bridgman technique in industrial ALD furnace at withdrawal rate of 3 mm/min. The samples for investigations were cut from the blade root parallel to the withdrawal direction. Metallographic sections of longitudinal samples planes were prepared for further investigations. The samples were analysed using scanning electron microscopy and the Laue diffraction studies. The crystal orientations in macro-scale were determined by analysis of the Laue pattern and local crystal orientations were studied by electron backscattered diffraction technique. Morphology of dendrites were examined by analysis of scanning electron microscopy macro-images. Study of subgrain structure was performed by X-ray diffraction topography. The sharp parallel contrast bands, visible on the X-ray topograms, were related with dendrite cores, arranged with the same direction. Additionally, the low angle boundaries were formed in certain samples, visible on the topograms as contrast shifts. Step changes of local crystal orientation in certain areas were observed on the electron backscattered diffraction maps. The electron backscattered diffraction crystal orientation maps were related to the misorientation visualized in topograms.

20

Microstructure and Residual Stress in AMS 6308 Steel after Vacuum Carburizing and Gas Quenching

62%

Dychtoń K., Kocurek P., Rokicki P., Wierzba B., Drajewicz M., Sieniawski J.

Acta Physica Polonica A

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2016

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vol. 130

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issue 4

953-955

EN

In this work, the vacuum carburizing and gas quenching has been done on gears box made of high strength alloy steel AMS 6308 in four different temperatures. The measurements of hardness was done to evaluate the effective case depth for each temperature. The analysis of retained austenite was presented as a factor which can affect values of residual stress. The residual stresses were measured in Protoi XDR portable diffractometer and the analysis was examined to find influence of temperature and carburizing time on the direction and values of residual stresses.

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Surface Modification and its Influence on the Microstructure and Creep Resistance of Nickel Based Superalloy René 77 / Modyfikacja Powierzchniowa Oraz Jej Wpływ Na Mikrostrukture I Wytrzymałosc Na Pełzanie Odlewów Z Nadstopu Niklu Ren´E 77

Microstructure and mechanical properties of C355.0 cast aluminium alloy

Numerical Approach to Predicting Thermodynamic Properties of Ternary Al-Ni-Pt Alloys

Microstructural Characterization Of Quenched And Plastically Deformed Two-Phase α+β Titanium Alloys

Numerical Simulation of Directional Solidification Process of Single Crystal Ni- Based Superalloy Casting

Primary Creep Behaviour of Two-Phase Titanium Alloy with Various Microstructure

Functional Properties of Aluminide Layer Deposited on Inconel 713 LC Ni-based Superalloy in the CVD Process Właściwości Użytkowe Warstwy Aluminidkowej Wytworzonej W Procesie CVD Na Stopie Niklu Inconel 713 LC

Influence of Chemical Composition of Nickel Based Superalloy on the Formation of Aluminide Coatings Wpływ Składu Chemicznego Nadstopu Niklu Na Budowę Warstwy Aluminidkowej

Crystal Perfection Studies of Single Crystal Superalloy Turbine Blades by X-Ray Diffraction Methods

Microstructure and Oxidation Resistance of an Aluminide Coating on the Nickel Based Superalloy Mar M247 Deposited by the CVD Aluminizing Process

Some Properties of Platinum and Palladium Modified Aluminide Coatings Deposited by CVD Method on Nickel-Base Superalloys

Evaluation of the Cutting Force Components and the Surface Roughness in the Milling Process of Micro- and Nanocrystalline Titanium

Mould Walls Inclination and Dendritic Morphology of CMSX-4 Blades Airfoils

Characterization of Casting Defects in the Single Crystal Turbine Blade Airfoil

Hot Deformation Of 6xxx Series Aluminium Alloys

The Ni-Al-Hf Multiphase Diffusion

The Control of Solidification Kinetics of the Vacuum-cast Thin-wall Nickel-based Superalloys by Changing the Geometrical Characteristics of the Ceramic Mold

Dendrite Growth in Selector-Root Area of Single Crystal CMSX-4 Turbine Blades

Analysis of CMSX-4 Single-Crystalline Turbine Blades Root by Electron and X-Ray Diffraction Methods

Microstructure and Residual Stress in AMS 6308 Steel after Vacuum Carburizing and Gas Quenching