sure 2018 - x-ray diffraction studies of cmas infiltrated ......x-ray diffraction and how the rays...

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RESEARCH POSTER PRESENTATION DESIGN © 2015 www.PosterPresentations.com 0.00% 10.00% 20.00% 30.00% 40.00% 50.00% 60.00% 70.00% 80.00% 90.00% 100.00% Phase Volume Fraction Tetragonal Phase Volume Fraction Tetragonal 1250 1h Tetragonal 1250 10h Tetragonal 1225 10h 0.00% 0.50% 1.00% 1.50% 2.00% 2.50% 3.00% 3.50% 4.00% Phase Volume Fraction Monoclinic Phase Volume Fraction Monoclinic 1250 1h Monoclinic 1250 10h Monoclinic 1225 10h Yttria-stabilized zirconia (YSZ) serves as a ceramic topcoat for thermal barrier coatings (TBCs) in gas turbines in the aviation and power generation industries to improve their efficiency. TBCs lower temperatures of turbine blades during operation. Siliceous surface contaminants, such as sand, volcanic ash, and runway debris, infiltrate and rapidly degrade TBCs. Calcium-magnesium-aluminum-silicate (CMAS) is a mixture used to represent these particulates. CMAS melts into the TBC at around 1240°C, depleting the yttrium into the CMAS. In industry, operating temperatures can reach up to 1400°C to 1600°C, which is well above this 1240°C threshold Background and Introduction Experimental and Theory Analysis and Results Siliceous containments, represented by CMAS, rapidly degrade the YSZ coating used to improve the efficiency in turbines. It was found that the ingression of CMAS is impacted by the time and the temperature of the ingression environment. This impact means that the more extreme temperatures found within the turbine over long durations of operation will dramatically increase the monoclinic phases present within the YSZ coating, causing more residual stresses to form. Eventually these stresses will lead to cracks forming in the coating and cause failure, spallation. References/Acknowledgements This material is based upon work supported by National Science Foundation grants DMR 1337758 and OISE 1460045 and by the German Aerospace Center (DLR). Bohorquez E., Sarley B., Hernandez J., Hoover R., Laurene Tetard, Naraparaju R., Schulz U. & Raghavan S., “Investigation of the Effects of CMAS-infiltration in EB-PVD 7% Yttria-Stabilized Zirconia via Raman Spectroscopy,” 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 812 January 2018, Kissimmee, Florida. Naraparaju R., Hüttermann M., Schuly U. & Mechnich P., „Tailoring the EB-PVD columnar microstructure to mitigate the infiltration of CMAS in 7YSZ thermal barrier coatings,“ Journal of the European Cermaic Society 37.1 (2017) 261-270. doi: 10.1016/j.jeurcerasoc.2016.07.027 XRD reveals information about a material’s atomic structure by observing the way an X-ray beam interacts with the sample. The angle of diffraction relates to the spacing of the atomic planes by Bragg’s Law, shown below. From XRD data, the phases present in a sample can be identified and quantified. Stein Z. a , Bohorquez E. a , Rossmann L. a , Naraparaju R. b , Raghavan S. a a Department of Mechanical and Aerospace Engineering, University of Central Florida, 4000 Central Florida Blvd., Orlando, FL 32816, USA b German Aerospace Center, Linder Höhe, 51147 Colonge, Germany X-Ray Diffraction Studies of CMAS Infiltrated Thermal Barrier Coatings Phase A (Å) B (Å) C (Å) β (°) Volume (*10 6 picometer 3 ) Tetragonal 3.63 3.63 5.14 90.00 67.55 Monoclini c 5.15 5.21 5.31 99.23 140.54 Cubic 3.64 3.64 5.15 90.00 68.33 Monoclinic Phase Volume Fractions of Samples Tetragonal Phase Volume Fractions of Samples Future Work CMAS YSZ TBC Now that the monoclinic phase has been found to be correlated with temperature and time of exposure with XRD, this correlation must be compared to previously collected Raman spectroscopy data. Raman is a non-destructive technique to measure vibrational scattering of a sample’s molecules to determine the material, its phases, and stresses present. Continue and compare the stresses found between Raman and XRD samples. Use 2D XRD (In-situ) to further validate Raman as the non- destructive method for CMAS infiltration analysis. The XRD used in this study had diffraction data at different points, 1D XRD. 2D XRD giving data from an area of diffraction through a diffraction cone, holds information about atomic arrangement, texture, microstructure, defects, stresses, pans phases. 2D XRD has high speed and high accuracy. This would allow for analysis of CMAS infiltration into TBCs without permanently destroying samples. m m c t m c t t m t c m t t c m t t t t t t 0% 10% 20% 30% 40% 50% 60% 70% 80% 90% 100% 15 20 24 29 34 38 43 48 52 57 62 66 71 76 80 85 90 Intensity (%) Diffraction Angle (2θ) Expected XRD plot of YSZ without CMAS with phases overlaid m m c t m t c t m t m t t c t m t t t t t t t 0% 10% 20% 30% 40% 50% 60% 70% 80% 90% 100% 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 Intensity (%) Diffraction Angle (2θ) XRD plot of 1225°C 10 hours with CMAS ingression m m c t m t c t m t c m c t t m t t t t t t 0% 10% 20% 30% 40% 50% 60% 70% 80% 90% 100% 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 Intensity (%) Diffraction Angle (2θ) XRD plot of 1250°C 1h with CMAS ingression m m c t m m t c t t c m t t m t t t t t t 0% 10% 20% 30% 40% 50% 60% 70% 80% 90% 100% 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 Intensity (%) Diffraction Angle (2θ) XRD plot of 1250°C 10h with CMAS ingression Conclusion Left: Turbine blades degraded due to CMAS infiltration. Right with out CMAS. When CMAS depletes nearby yttrium, it causes the zirconia to change phase - from a tetragonal (t-phase) crystal structure to monoclinic (m-phase). The m-phase phase has a larger volume, causing stresses in the coating. Trace amounts of cubic (c-phase) is also present and transforms into either t- or m-phases; however the c-phase has a similar volume to t-phases so typically YSZ coatings would be composed of t- and c-phases. Objectives: Conduct X-ray diffraction (XRD) to determine how temperatures below and above the CMAS melting point (1240°C) and time of exposure to CMAS effects the phases of YSZ. Obtain phase volume fraction calculations to quantify phase change of YSZ TBCs exposed to CMAS. Tetragonal Monoclinic SEM images of CMAS ingression in YSZ. Left: Appearance of monoclinic YSZ globular formations. Right: Intact columnar microstructure. X-ray diffraction and how the rays interact with molecules within a sample Phase PVF 1225°C 10 h (%) PVF 1250°C 1h (%) PVF 1250°C 10h (%) Tetragonal 91.2 90.8 95.2 Monoclinic 2.2 1.9 3.5 Cubic 6.5 7.3 1.3 Left: Summary of crystal structure for each phase of YSZ. Right: PVF of m-, t-, and c- phases for each sample (obtained from analysis from the XRD plots below). There are increases in the m-phases from 1h to 10h as well as compared to 1225 and 1250°C. Graph 1: The expected peaks of YSZ without CMAS. Mainly t- and c- phases. Minimal m-phases should be present, hence small peaks present at m. Graph 2: The c-, t-, and m-peaks of the samples. The relative intensities of the XRD peaks were used to determine the volume fractions of t- and m-phases. There was an increase of about 1.6% in the m-phase between 1 and 10 hours for the 1250°C sample indicating the impact of time on the ingression effects. There was about a 1.3% higher m-phase volume within the 1250°C compared to the 1225°C after 10 hours indicating that the temperature of the ingression environment plays a role in ingression effects. There was also an increase of about 4.4% in the t-phase within the 1250°C sample between 1 and 10 hours of exposure. This increase is due to the decrease in the c-phase within the samples. θ θ d nλ = 2dsinθ Motivation and Objectives Since 1225°C is below the melting point of CMAS, only one sample with long exposure (10 h) was chosen and since 1250°C is above the melting point of CMAS, 2 samples were chosen where one was with short exposure (1 h) and one with long exposure (10 h). The XRD data was compared to literature to identify the phases present. The left table below summarizes the crystal structure of the phases present in YSZ; meanwhile the right table displays the PVFs obtained from analyzing the XRD plots shown below.

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Page 1: SURE 2018 - X-Ray Diffraction Studies of CMAS Infiltrated ......X-ray diffraction and how the rays interact with molecules within a sample Phase PVF 1225°C 10 h (%) PVF 1250°C 1h

RESEARCH POSTER PRESENTATION DESIGN © 2015

www.PosterPresentations.com

0.00%10.00%20.00%30.00%40.00%50.00%60.00%70.00%80.00%90.00%

100.00%

Ph

ase V

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Tetragonal Phase Volume Fraction

Tetragonal 1250 1h

Tetragonal 1250 10h

Tetragonal 1225 10h

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1.00%

1.50%

2.00%

2.50%

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Monoclinic Phase Volume Fraction

Monoclinic 1250 1h

Monoclinic 1250 10h

Monoclinic 1225 10h

Yttria-stabilized zirconia (YSZ) serves as a ceramic topcoat for

thermal barrier coatings (TBCs) in gas turbines in the aviation

and power generation industries to improve their efficiency.

TBCs lower temperatures of turbine blades during operation.

Siliceous surface contaminants, such as sand, volcanic ash,

and runway debris, infiltrate and rapidly degrade TBCs.

Calcium-magnesium-aluminum-silicate (CMAS) is a mixture

used to represent these particulates. CMAS melts into the TBC

at around 1240°C, depleting the yttrium into the CMAS. In

industry, operating temperatures can reach up to 1400°C to

1600°C, which is well above this 1240°C threshold

Background and Introduction

Experimental and Theory

Analysis and Results

Siliceous containments, represented by CMAS, rapidly degrade

the YSZ coating used to improve the efficiency in turbines. It

was found that the ingression of CMAS is impacted by the time

and the temperature of the ingression environment. This impact

means that the more extreme temperatures found within the

turbine over long durations of operation will dramatically

increase the monoclinic phases present within the YSZ coating,

causing more residual stresses to form. Eventually these

stresses will lead to cracks forming in the coating and cause

failure, spallation.

References/Acknowledgements

This material is based upon work supported by National Science

Foundation grants DMR 1337758 and OISE 1460045 and by the

German Aerospace Center (DLR).

Bohorquez E., Sarley B., Hernandez J., Hoover R., Laurene Tetard,

Naraparaju R., Schulz U. & Raghavan S., “Investigation of the Effects

of CMAS-infiltration in EB-PVD 7% Yttria-Stabilized Zirconia via

Raman Spectroscopy,” 2018 AIAA/ASCE/AHS/ASC Structures,

Structural Dynamics, and Materials Conference, 8–12 January 2018,

Kissimmee, Florida.

Naraparaju R., Hüttermann M., Schuly U. & Mechnich P., „Tailoring

the EB-PVD columnar microstructure to mitigate the infiltration of

CMAS in 7YSZ thermal barrier coatings,“ Journal of the European

Cermaic Society 37.1 (2017) 261-270. doi:

10.1016/j.jeurcerasoc.2016.07.027

• XRD reveals information about a material’s atomic structure

by observing the way an X-ray beam interacts with the

sample.

• The angle of diffraction relates to the spacing of the atomic

planes by Bragg’s Law, shown below.

• From XRD data, the phases present in a sample can be

identified and quantified.

Stein Z.a, Bohorquez E.a, Rossmann L.a, Naraparaju R.b, Raghavan S.a

a Department of Mechanical and Aerospace Engineering, University of Central Florida, 4000 Central Florida Blvd., Orlando, FL 32816, USA

b German Aerospace Center, Linder Höhe, 51147 Colonge, Germany

X-Ray Diffraction Studies of CMAS Infiltrated Thermal Barrier

Coatings

Phase A (Å) B (Å) C (Å) β (°) Volume (*106

picometer3)

Tetragonal 3.63 3.63 5.14 90.00 67.55

Monoclini

c 5.15 5.21 5.31 99.23 140.54

Cubic 3.64 3.64 5.15 90.00 68.33

Monoclinic Phase Volume Fractions of Samples Tetragonal Phase Volume Fractions of Samples

Future Work

CMAS

YSZ TBC

• Now that the monoclinic phase has been found to be correlated with temperature and time of exposure with XRD, this correlation must be compared to previously collected Raman spectroscopy data.

• Raman is a non-destructive technique to measure vibrational scattering of a sample’s molecules to determine the material, its phases, and stresses present.

• Continue and compare the stresses found between Raman and XRD samples.

• Use 2D XRD (In-situ) to further validate Raman as the non-destructive method for CMAS infiltration analysis.

• The XRD used in this study had diffraction data at different points, 1D XRD. 2D XRD giving data from an area of diffraction through a diffraction cone, holds information about atomic arrangement, texture, microstructure, defects, stresses, pans phases. 2D XRD has high speed and high accuracy.

• This would allow for analysis of CMAS infiltration into TBCs without permanently destroying samples.

m m

c

t

m

c t

t m

t c

m t

t c

m t t t t t

t 0%

10%

20%

30%

40%

50%

60%

70%

80%

90%

100%

15 20 24 29 34 38 43 48 52 57 62 66 71 76 80 85 90

Inte

ns

ity (

%)

Diffraction Angle (2θ)

Expected XRD plot of YSZ without CMAS with phases overlaid

m m

c

t

m

t c

t

m

t

m

t

t c

t m

t

t t

t t

t t

0%

10%

20%

30%

40%

50%

60%

70%

80%

90%

100%

15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90

Inte

ns

ity (

%)

Diffraction Angle (2θ)

XRD plot of 1225°C 10 hours with CMAS ingression

m m

c

t

m

t c

t

m

t

c

m

c

t

t

m

t

t

t t t t

0%

10%

20%

30%

40%

50%

60%

70%

80%

90%

100%

15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90

Inte

ns

ity (

%)

Diffraction Angle (2θ)

XRD plot of 1250°C 1h with CMAS ingression

m m

c

t

m m

t

c

t

t

c

m

t

t

m

t

t t t t

t

0%

10%

20%

30%

40%

50%

60%

70%

80%

90%

100%

15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90

Inte

ns

ity (

%)

Diffraction Angle (2θ)

XRD plot of 1250°C 10h with CMAS ingression

Conclusion

Left: Turbine blades degraded due to CMAS infiltration. Right with out

CMAS.

• When CMAS depletes nearby yttrium, it causes the zirconia

to change phase - from a tetragonal (t-phase) crystal

structure to monoclinic (m-phase).

• The m-phase phase has a larger volume, causing stresses in

the coating.

• Trace amounts of cubic (c-phase) is also present and

transforms into either t- or m-phases; however the c-phase

has a similar volume to t-phases so typically YSZ coatings

would be composed of t- and c-phases.

Objectives: • Conduct X-ray diffraction (XRD) to determine how

temperatures below and above the CMAS melting point

(1240°C) and time of exposure to CMAS effects the phases

of YSZ.

• Obtain phase volume fraction calculations to quantify phase

change of YSZ TBCs exposed to CMAS.

Tetragonal Monoclinic

SEM images of CMAS ingression in YSZ. Left: Appearance of monoclinic

YSZ globular formations. Right: Intact columnar microstructure.

X-ray diffraction and how the rays interact

with molecules within a sample

Phase PVF 1225°C 10 h (%) PVF 1250°C 1h (%) PVF 1250°C 10h (%)

Tetragonal 91.2 90.8 95.2

Monoclinic 2.2 1.9 3.5

Cubic 6.5 7.3 1.3

Left: Summary of crystal structure for each phase of YSZ. Right: PVF of m-, t-, and c- phases for each sample (obtained from analysis from the XRD plots

below). There are increases in the m-phases from 1h to 10h as well as compared to 1225 and 1250°C.

Graph 1: The expected peaks of YSZ without CMAS. Mainly t- and c- phases.

Minimal m-phases should be present, hence small peaks present at m. Graph 2: The c-, t-, and m-peaks of the samples.

• The relative intensities of the XRD peaks were used to determine the volume fractions of t- and m-phases.

• There was an increase of about 1.6% in the m-phase between 1 and 10 hours for the 1250°C sample indicating the impact of time on the

ingression effects.

• There was about a 1.3% higher m-phase volume within the 1250°C compared to the 1225°C after 10 hours indicating that the temperature of the

ingression environment plays a role in ingression effects.

• There was also an increase of about 4.4% in the t-phase within the 1250°C sample between 1 and 10 hours of exposure.

• This increase is due to the decrease in the c-phase within the samples.

θ θ

d

nλ = 2dsinθ

Motivation and Objectives

Since 1225°C is below the melting point of CMAS, only one sample with long exposure (10 h) was chosen and since 1250°C is above the

melting point of CMAS, 2 samples were chosen where one was with short exposure (1 h) and one with long exposure (10 h). The XRD

data was compared to literature to identify the phases present. The left table below summarizes the crystal structure of the phases

present in YSZ; meanwhile the right table displays the PVFs obtained from analyzing the XRD plots shown below.