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ICMCTF 2012! - CD-Lab Application Oriented Coating Development

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<strong>Coating</strong>s for Use at High Temperature<br />

Room: Sunrise - Session A1-2<br />

Wednesday Afternoon, April 25, <strong>2012</strong><br />

<strong>Coating</strong>s to Resist High Temperature Oxidation,<br />

Corrosion and Fouling<br />

Moderator: J. Pérez, Universidad Complutense de Madrid,<br />

Spain, B. Hazel, Pratt and Whitney, US, L-G. Johansson,<br />

Chalmers University of Technology, Sweden, D. Naumenko,<br />

Forschungszentrum Jülich GmbH, Germany<br />

1:50pm A1-2-1 Microstructure degradation of simple, Pt- and Pt+Pdmodified<br />

aluminide coatings on CMSX-4 superalloy under cyclic<br />

oxidation conditions, R. Swadzba (rswadzba@gmail.com), Silesian<br />

University of Technology, Poland<br />

The paper presents results of simple, Pt/Pd- and Pt-modified aluminide<br />

coatings cyclic oxidation-induced degradation analysis. The coatings were<br />

deposited by Pt and Pt+Pd electroplating, followed by vapor phase<br />

aluminizing at 1050˚C. Cyclic oxidation tests were performed at 1100˚C in<br />

23h cycles. Microstructural and phase analysis conducted using SEM, EDS<br />

and EBSD methods revealed that the oxide layers that formed on the<br />

coatings were composed of three distinctive types of oxides growing<br />

according to a specific pattern which is described. The oxide layer that<br />

formed on the simple aluminide coating exhibited low adhesion in<br />

comparison to Pt- and Pt,Pd-modified aluminide coatings which managed to<br />

maintain an adherent oxide layer that contained higher amount of desirable<br />

α-alumina. The Al-depleted βNiAl grains remained much larger in the<br />

modified aluminide coatings, even after failure. What is more, stripes<br />

characteristic for martensitic transformation were discovered in the β phase<br />

grains in all coatings. Based on the results a microstructural degradation<br />

scheme of the investigated coatings is presented.<br />

2:10pm A1-2-2 Influence of vacuum parameters during heat treatment<br />

on surface composition of MCrAlY coatings, I. Keller (i.keller@fzjuelich.de),<br />

D. Naumenko, L. Singheiser, W.J. Quadakkers,<br />

Forschungszentrum Jülich GmbH, Germany<br />

MCrAlY type (M = Ni, Co) coatings are commonly used as overlay<br />

coatings and bond coats (BC`s) for thermal barrier coatings (TBC`s) in aero<br />

engines and industrial gas turbines. It is known that the life time of thermal<br />

barrier coatings is crucially affected by the properties of the thermally<br />

grown oxide (TGO), which is formed during high temperature service at the<br />

TBC/BC interface. The most relevant properties of the oxide scale are<br />

growth rate, adherence to the BC, and composition [1]. Several<br />

investigations have shown that the TGO-properties depend strongly on the<br />

parameters of vacuum heat treatment commonly applied to the MCrAlY<br />

coated components prior to TBC deposition [2-4]. Variation of the heat<br />

treatment parameters can result in formation of different types of oxide<br />

scales on BC`s with nominally the same composition, which leads to<br />

different lifetimes of the TBC.<br />

In the present study the influence of vacuum parameters and atmosphere<br />

composition on the phase equilibrium at the MCrAlY surfaces during heat<br />

treatment are investigated. For this purpose free standing MCrAlY coatings<br />

(manufactured via VPS or HVOF) with rough and polished surfaces were<br />

exposed at 1100 °C for times between 1 and 5 hours in different<br />

atmospheres (

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