ICMCTF 2012! - CD-Lab Application Oriented Coating Development
ICMCTF 2012! - CD-Lab Application Oriented Coating Development
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 (