Nanoindentation of La-Cr-O Thin Films

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Nanoindentation of La-Cr-O Thin Films Anthony Coratolo1, Nina Orlovskaya1 Christopher Johnson2, Randall Gemmen2 1 Drexel University, Philadelphia, USA 2 National Energy Technology Laboratory, Morgantown, USA Acknowledgment The work at Drexel was supported by the National Energy Technology Laboratory, US Department of Energy under contract # 239811.

Objectives Develop a reliable method for the characterization of mechanical properties of La-Cr-O thin film Investigate the deformation behavior of the thin film during the contact loading by Berkovich indenter Measure Hardness and Modulus of films annealed in air over a range of temperatures

Background Interconnect Function- Electrically connect the cells in a stack, provide separation and flow control of gases, and provides mechanical stability. For Intermediate temperature SOFCs a Cr rich Stainless Steal can be used, but oxidation can be a problem. To improve oxidation resistance the stainless steal a thin layer of a conductive perovskite is applied to the surface.

Nano Indentation http://www.mts.com/nano/nano_indenter_xp.htm http://www.nanoindentation.cornell.edu/machine/nanoindentation-machine.htm

Load, P Load, P Load, P Load vs. displacement Curves Pure Plastic (P max, h end ) Pure Elastic (P max, h end ) Displacement, h Displacement, h Plastic and Elastic H P max area S E r 2 A loading Unloading (P max, h end ) 1 E r 1 v E 2 1 E v i 2 i Displacement, h s http://www.nanoindentation.cornell.edu/machine/nanoindentation-machine.htm

Oliver-Pharr Model of the Material Response h surface profile after load removal indenter h s h c h r P initial surface surface profile under load h s h h P max S c max h s A( h c ) 24.5h 7 2 1 i 2 c i C h i c P = applied force h c = contact depth h = indenter displacement h r = plastic deformation after load removal C i = material property h s = surface displacement at the contact perimeter Oliver & Pharr, J. Mater. Res. 1992

Materials under study LaCrO 3 Target, 4% porous 5W power Picture of the thin film LaCrO 3 on the Stainless Steel Substrate Coatings done by Arshad Mumtaz of Thin Films, Inc., Schematic presentation of the experiment set up, Custom Sputter Down System Stainless steel substrate coated with LaCrO3 perovskite by magnetron RF sputtering

X-Ray Amorphous Nanoscrystalline X-Ray Amorphous Monoclinic LaCrO 4 Orthorhombic LaCrO 3 4-495 C Beginning of oxygen absorption from air 495-53 C Amorphous to monoclinic LaCrO4 structure phase transition 78-84 C Monoclinic LaCrO4 to Orthorhombic LaCrO3 phase transition

Intensity, a.u. Intensity, a.u. Intensity, a.u. Intensity, a.u. Intensity, a.u. Intensity, a.u. Intensity, a.u. Intensity, a.u. Characterization of La-Cr-O Thin Film 25 2 15 1 As received 1 hour @ 5 C 1 hour @ 7 C 1 hour @ 8 C 3 29 24 Nanoindentation Nanoindentation Nanoindentation Nanoindentation H=4.27GPa E=188.74GPa Unloading 25 2 15 1 H=4.61GPa E=195.GPa Unloading 24 19 14 9 H=5.29GPa E=185.65GPa Unloading 19 14 9 H=3.61GPa E=179.2GPa Pop-in Unloading 5 Loading 1 2 3 4 5 5 Loading 1 2 3 4 5 4-1 Loading 1 2 3 4 5 4-1 Loading 1 2 3 4 5 358.5 722.4 817. 1 as deposited 9 8 7 6 5 3 5 1 15 2 Raman shift, cm-1 143.8 4 Raman spectroscopy 855.3 5 o C 5 45 4 35 3 25 2 732. 1714.515 363.1 1 175. 5 Raman spectroscopy 5 1 15 2 Raman shift, cm-1 813.4 Raman spectroscopy 182.2 141.8 326.7 832.6 352.2 868.71 913.3 966.5 6 5 4 3 2 6 o C 1648.7 1746.5 1 32.3 149.4 5 1 15 2 Raman shift, cm -1 152.44 171.1 711.43 56.52 254.46 439.37 1436.2 2 8 o C 18 16 14 12 855.95 1 8 Raman spectroscopy 6 4 5 1 15 2 Raman shift, cm -1 18 X-ray analysis SS 2 X-ray analysis Short range order Clusters formation SS 6 X-ray analysis Monazite type 5 Monoclinic 4 phase X-ray analysis Orthorhombic Perovskite 1 3 SS?? SS 2 1?? 2 25 3 35 4 45 2 Theta, o 2 25 3 35 4 45 2 Theta, o 2 25 3 35 4 45 2 Theta, o 2 25 3 35 4 45 2 Theta, o

Hardness, GPa Modulus, GPa Hardness and Young s modulus of La-Cr-O thin film after annealing at different temperatures for one hour 12 1 as recieved 3 C 4 C 6 C 5 C 7 C 8 C 9 C 23 22 21 2 as recieved 3 C 4 C 6 C 5 C 7 C 8 C 9 C 8 6 4 19 18 17 16 15 14 2 2 4 6 8 13 2 4 6 8 The effect of stainless steel substrate on hardness and Young s modulus is clearly seen as a function of a penetration depth of the indenter. As an indenter penetrates into the film (8 nm thickness), the influence of substrate become more and more pronounced. As the indenter penetrates on the full depth of the film, the mechanical properties of the SS substrate material are measured.

LaCrO 3 orthorhombic to rhombohedra Transition Under pressures of 5.4 GPa at room temperature orthorhombic LaCrO 3 will transform in to a rhombohedral configuration. Rhombohedral structure is less dense than orthorhombic. Phase transition could be induced by pressure under berkovich tip

ACP, GPa Mechanical Response after annealing at 8 C for 1 hour Indentation total area unload elastic recovery plastic deformation 5nm 17.56 7.122.46.594 2nm pop in 1317.842 271.745.26.794 2nm 758.292 157.15.27.793 4nm pop in 3864.46 18.384.261.739 4nm 3535.343 887.4.251.749 8nm pop in 18661.631 1876.85.11.899 8 nm 18736.88 1279.614.68.932 5 nm depth 1.2 1.8.6.4.2 1 2 3 4 5 6 4 3.5 3 2.5 2 1.5 1.5 1 2 3 4 5 6

ACP, GPa ACP, GPa 2 nm depth 9. 8. 7. 6. 5. 4. 3. 2. 1. 7. 5 1 15 2 25 1 9. 8. 7. 6. 5. 4. 3. 2. 1. 5 1 15 2 25 3 9. 6. 5. 4. 3. 2. 1. 5 1 15 2 25 8. 7. 6. 5. 4. 3. 2. 1. 5 1 15 2 25 3

ACP, GPa ACP, GPa 4 nm depth 25. 2 15. 1 5. 1 2 3 4 5 2 18. 16. 14. 12. 1 8. 6. 4. 2. 1 2 3 4 5 6. 5. 8. 7. 6. 4. 5. 3. 4. 2. 3. 2. 1. 1. 1 2 3 4 5 1 2 3 4 5

ACP, GPa ACP, GPa 8 nm depth 6 6 5 5 4 4 3 3 2 2 1 6. 5. 4. 3. 2. 1. 2 4 6 8 1 2 4 6 8 1 1 8. 7. 6. 5. 4. 3. 2. 1. 2 4 6 8 1 2 4 6 8 1

Conclusions Mechanical behavior of La-Cr-O thin films was studied by nanoindentation. As deposited and annealed at 5, 6, and 8 o C films were used for mechanical and structural characterization. Hardness and Young s modulus of the as deposited amorphous and annealed La-Cr-O thin films were measured using Berkovich diamond indenter. Load-displacement curves were obtained in a displacement control mode. As a result of an annealing at different temperatures, different film structure was formed. After annealing at 5 o C for 1 hour the short order structure was formed; annealing at 6 o C lead to the formation of LaCrO 4 monoclinic structure; after annealing at 8 o C the orthorhombic LaCrO 3 perovskite structure was formed, as confirmed by XRD and micro-raman spectroscopy. Hardness and Young s modulus change from 1-12 GPa and 12 GPa to 3 GPa and 14 GPa respectively, as a result of the phase transition of the LaCrO3 phase transitions.