2013
DOI: 10.2478/amm-2013-0057
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Microstructure and Oxidation Resistance of an Aluminide Coating on the Nickel Based Superalloy Mar M247 Deposited by the CVD Aluminizing Process

Abstract: An investigation was conducted to synthesize βNiAl coating on the nickel based superalloy Mar M247 in a chemical vapor deposition process (CVD). The low activity process of aluminizing was carried out for 8 hours at the temperature 1050• C. Surface morphology and cross-section microstructure of the diffusion coating were studied and compared by using an optical microscope, a scanning electron microscope (SEM) equipped with energy dispersive spectroscopy and an X-ray diffractometer. It was found that aluminide … Show more

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Cited by 30 publications
(32 citation statements)
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“…The aluminide coating was deposited using the CVD equipment BPXPR0325S manufactured by IonBond company [1,2,8,11,12,17]. The aluminizing process consisted of the following stages: I-heating from the room temperature up to 900 1C; II-aluminizing at 900 1C for 20 min; III-heating from 900 1C to 1020 1C; IV-aluminizing at 1020 1C for 5 min; V-aluminizing and zirconizing at 1020 1C for 4 min; VI-aluminizing at 1020 1C for 10 min; VII-cooling samples with the furnace.…”
Section: Methodsmentioning
confidence: 99%
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“…The aluminide coating was deposited using the CVD equipment BPXPR0325S manufactured by IonBond company [1,2,8,11,12,17]. The aluminizing process consisted of the following stages: I-heating from the room temperature up to 900 1C; II-aluminizing at 900 1C for 20 min; III-heating from 900 1C to 1020 1C; IV-aluminizing at 1020 1C for 5 min; V-aluminizing and zirconizing at 1020 1C for 4 min; VI-aluminizing at 1020 1C for 10 min; VII-cooling samples with the furnace.…”
Section: Methodsmentioning
confidence: 99%
“…It can be achieved by the increase of the volume of the air flowing through the turbine as well as by the increase of the temperature at its hot stage. The increase of the temperature of gases at the turbine inlet in modern engines depends on the efficient cooling systems of turbine blades and the usage of nickel or cobalt superalloys with protective thermal barrier coatings (TBC) [1][2][3][4][5][6]. The improvement of engine efficiency by the increase of turbine inlet temperature implicates the use of different types of protecting coatings including aluminide and MeCrAlY multicomponent ones.…”
Section: Introductionmentioning
confidence: 99%
“…The rhodium layer of 0.5-μm thick was deposited on CMSX 4 superalloy using the electroplating method. The rhodium coated superalloy was aluminized by the CVD method (Romanowska et al, 2013;Zielińska et al, 2013;Romanowska et al, 2015;Zagula-Yavorska et al, 2015). The chemical composition of the superalloy was as follows: 61.7% wt.…”
Section: Methodsmentioning
confidence: 99%
“…In this case the bond coating also serves to ensure top coating adhesion, mitigates thermal mismatch stresses with the substrate and is not solely for oxidation protection. The compatibility between the thermally grown oxide (TGO) scale (comprising of Al 2 O 3 and other oxides) forms during oxidation and TBCs plays a crucial role in governing coatings durability [ 3 ]. Leckie et al [ 4 ] studied the thermochemical compatibility between alumina (TGO) and Gd 2 Zr 2 O 7 .…”
Section: Introductionmentioning
confidence: 99%