journal article·2003-01

MCrAlY coating developed via a new electroless-like route: influence of deposition parameters

Marie-Pierre Bacos, Benoı̂t Girard, Pierre Josso, Catherine Rio

Surface and Coatings Technology· Volume 162· Issue 2-3
Publisher page

Abstract

Abstract Improvement in efficiencies of gas turbines can be achieved by increasing the gas inlet turbine temperature. This leads to increased blade and vane temperatures and therefore to enhanced oxidation and corrosion attack of the coatings on these components. Coatings such as MCrAlY are typically used to improve components’ high temperature properties. Various processing routes have been studied to produce MCrAlY coatings including plasma spray and electrolysis methods. Plasma spray is convenient and permits a large range of MCrAlY composition to be obtained but the directionality of the process leads to non-uniformity of the coating thickness distribution. More recently, an electrolytic route has been developed using sulfamate or sulfate baths, which cause contamination of the coatings and has a detrimental effect on the adherence of the protective oxide scale. A potentially attractive processing route is the electroless autocatalytic process, since this has the advantage of permitting non-directional and sulfur-free deposition. We have investigated MCrAlY deposition by an electroless-like autocatalytic process. Coatings were deposited on a single crystal nickel-based alloy (MC-NG) and the differences in microstructure and phase composition according to the different process stages are reported. The influence of process parameters on the coating characteristics is discussed.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: High-Temperature Coating Behaviors · Electrocatalysts for Energy Conversion · Catalytic Processes in Materials Science

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

References (18)

Show source-provided references
1. Protective coatings
2. Protective coating-purpose, role and design10.1179/mst.1986.2.3.194 ↗
3. Advanced high temperature coatings for gas turbine
4. Coatings for high temperature corrosion in aero and industrial gas turbine
5. E.C. Kedward, et al., Processes for the electrodeposition of composite coatings, United States Patent 4,305,792 December 15, 1981.
6. F.J. Honey, et al., Overlay coating, United States Patent 4,810,334 March 7, 1989.
7. J. Foster, Production of Coatings, United States Patent 5,037,513 August 6, 1991.
8. V.M. Wride, et al., Gas Turbine Blades, United States Patent 5,076,897 December 31, 1991.
9. J. Foster, Electrodeposited Composite Coatings, United States Patent 5,558,758 September 24, 1996.
10. J. Foster, et al., Jig for Coating Rotor Blades, United States Patent 5,702,574 December 30, 1997.
11. J. Foster, Protective Coating, United States Patent 5,824,205 October 20, 1998.10.1016/S0172-2190(99)00010-1 ↗
12. J. Foster, Protective coating, United States Patent 5,833,829 November 10, 1998.
13. The production of multi-component alloy coatings by particle codeposition10.1080/00202967.1985.11870719 ↗
14. Prediction of thickness distribution of electrodeposited coatings using a low-cost boundary element method
15. Rivoaland · 2001 · 6
16. P. Josso, et al., Hydrazine bath for chemically depositing nickel and/or cobalt, and a method of preparing such a bath, United States Patent 4,844,739, July 4, 1989
17. High γ′ solvus new generation nickel-based superalloys for single crystal turbine blade applications
18. B. Girard, M.-P. Bacos, E. Berger, P. Josso, Procédé pour former sur un substrat métallique un revêtement métallique protecteur exempt de soufre, French patent, 2 807 073.