journal article·2018-08Open access

Mechanical properties of sprayed overlayers on superalloy substrates, obtained via indentation testing

J.E. Campbell, T. Kalfhaus, R. Vassen, R.P. Thompson, J. Dean, T.W. Clyne

Acta Materialia· Volume 154

Abstract

This paper concerns the use of a recently-developed methodology for inferring stress-strain curves from indentation data, based on iterative FEM simulation of the procedure. A relatively large indenter (2 mm diameter) is used, with deep penetration (to about 25% of the indenter radius). This has been carried out on (polished) free surfaces of sprayed superalloy overlayers on single crystal superalloy substrates. Both load-displacement data and residual indent profiles were obtained, with the overlayers being in two different conditions (as-sprayed and annealed). The overlayers were relatively thick (∼2.5 mm), so it was also possible to carry out uniaxial compression tests on them (in the through-thickness direction). The inferred stress-strain curves were similar in each case when derived from load-displacement data and indent profiles, and also close to the plots obtained by conventional uniaxial testing. The yield stress levels in both cases were around 1000 MPa, but the work hardening rate was significantly higher for the as-sprayed material. This kind of information is of considerable potential value when attempting to optimize the properties of such overlayers. The procedure can be employed, with some confidence, to cases for which uniaxial testing is difficult or impossible.
Source: openalex_inverted_index · Quality: baseline

Research context

OpenAlex topics: Metal and Thin Film Mechanics · High-Temperature Coating Behaviors · Diamond and Carbon-based Materials Research

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (37)

Show source-provided references
1. Low-temperature hot Corrosion of cobalt-base alloys 1. Morphology of the reaction product10.1007/BF02647841 ↗
2. Hot corrosion in gas turbine components10.1016/S1350-6307(00)00035-2 ↗
3. Hot corrosion of metals and alloys10.1007/s11085-011-9254-6 ↗
4. Investigation of the mechanisms of Type-II hot corrosion of superalloy CMSX-410.1016/j.corsci.2013.11.048 ↗
5. An overview of Na2SO4 and/or V2O5 induced hot corrosion of Fe- and Ni-based superalloys
6. The effect of microstructure on the type II hot corrosion of Ni-Base MCrAlY alloys10.1007/s11085-013-9405-z ↗
7. A method for investigation of hot corrosion by gaseous Na2SO410.1016/j.corsci.2013.04.006 ↗
8. On the hot corrosion of nickel at 700 a degrees C10.1007/s11085-015-9588-6 ↗
9. Single-crystal laser deposition of superalloys: processing-microstructure maps10.1016/S1359-6454(00)00367-0 ↗
10. Repair and manufacturing of single crystal Ni-based superalloys components by laser powder deposition-A review
11. Control of crystal orientation and continuous growth through inclination of coaxial nozzle in laser powder deposition of single-crystal superalloy10.1016/j.jmatprotec.2015.11.017 ↗
12. Single-crystal turbine blade tip repair by laser cladding and remelting10.1016/j.cirpj.2017.04.001 ↗
13. Evaluation of the low heat input process for weld repair of nickel-base superalloys10.1007/s11665-010-9749-3 ↗
14. Wide gap braze repair of gas turbine blades and vanes-a review
15. Comparison of single crystal Ni based superalloy repair by gas tungsten arc and electron beam processes10.1179/026708310X12701095964405 ↗
16. Improved mechanical properties of Ni-rich Ni3Al coatings produced by EB-PVD for repairing single crystal blades10.1007/s12598-014-0340-1 ↗
17. Repairing of degraded hot section parts of gas turbines by cold spraying
18. On deposition of Waspaloy coatings by cold spray10.1179/1743294413Y.0000000199 ↗
19. The influence of NiAl3 on the high temperature oxidation of a plasma-sprayed overlay coating10.3184/096034000783640811 ↗
20. Investigation of an as-sprayed NiCoCrAIY overlay coating - microstructure and evolution of the coating10.1002/maco.200403808 ↗
21. Damage repair in CMSX-4 alloy without fatigue life reduction penalty. Metallurgical and Materials Transactions a-Physical Metallurgy and Materials Science
22. Predictive model to estimate the stress-strain curves of bulk metals using nanoindentation10.1016/j.triboint.2005.03.019 ↗
23. Assessment of the constitutive law by inverse methodology: small punch test and hardness10.1016/j.jnucmat.2006.02.076 ↗
24. Determination of material properties using nanoindentation and multiple indenter tips10.1016/j.ijsolstr.2008.08.042 ↗
25. An accurate and fast approach for determining materials stress-strain curves by nanoindentation and its FEM-based simulation10.1016/j.matchar.2005.10.005 ↗
26. Material model calibration by indentation, imprint mapping and inverse analysis10.1016/j.ijsolstr.2004.01.025 ↗
27. Use of quasi-static nanoindentation Data to obtain stress-strain Characteristics for metallic materials10.1016/j.actamat.2010.02.031 ↗
28. Finite element analysis of spherical indentation to study pile-up/sink-in phenomena in steels and experimental validation10.1016/j.ijmecsci.2011.09.009 ↗
29. Correlation of spherical nanoindentation stress-strain curves to simple compression stress-strain curves for elastic-plastic isotropic materials using finite element models10.1016/j.actamat.2016.04.034 ↗
30. Extraction of plasticity parameters from a single test using a spherical indenter and FEM modelling10.1016/j.mechmat.2016.11.014 ↗
31. Experimental and computational issues for automated extraction of plasticity parameters from spherical indentation10.1016/j.mechmat.2018.06.004 ↗
32. Tensile deformation
33. Tensile behaviour of a new single crystal nickel-based superalloy (CMSX-4) at room and elevated temperatures10.1007/BF02645265 ↗
34. Influence of microstructure on macroscopic elastic properties and thermal expansion of nickel-base superalloys ERBO/1 and LEK9410.1002/mawe.201500406 ↗
35. Riley · 2006
36. A simplex Method for function minimization10.1093/comjnl/7.4.308 ↗
37. Implementing the Nelder-Mead simplex algorithm with adaptive parameters10.1007/s10589-010-9329-3 ↗