Effect of Track Overlap on the Microstructure and Properties of the CoCrMoSi PTA Coatings

Abstract

Broadly speaking, the research and design of coatings are generally studied by way of single-track deposits; otherwise, the development of a coated part entails the understanding of how multi-track welding influences the microstructure and properties of the surface. This study evaluated the effect of track overlap on the microstructure and properties of the CoCrMoSi Tribaloy T400 alloy coatings produced on AISI 316L steel substrate. The characterization was performed by scanning electron microscopy, hardness and X-ray diffraction. The correlation between the degree of overlap and performance of the coatings was assessed by wear tests. The single track deposits showed hypoeutectic microstructure as a result of high Iron, Chromium and Nickel content. From the second track on, the chemical composition was displaced back to eutectic and then to hypereutectic with overlap of 25 and 50%, respectively. The microstructure dictated the hardness of the coatings (527 – 701 HV_0.5) and the lower mass loss rate was measured for hypereutectic with primary Laves phase.

CoMoCrSi alloy; plasma transferred arc; dilution; track overlapping; microstructure; wear behavior

1 Introduction

Different processes are used to produce coatings and the techniques which promote metallurgical bonding affect the microstructure features of alloys. In light of this, understanding the correlation among processing, microstructure and mechanical properties of the CoCrMoSi alloy coatings can be a challenge. A recent review of Plasma Transferred Arc (PTA) has pointed out the features that make the technique important and a potential solution for processing special alloys, due to the microstructure control and refinement of produced deposits¹.

Cobalt, Nickel and Iron-based superalloys are recognized as being able withstand harsh environments, involving wear, corrosion and corrosion-wear. Co-based alloy coatings have been applied to improve the service life of different components like valves and valve seats, bearings and bushings, sleeves, dies and punches. The high corrosion resistance of Cobalt-based alloys is related to Chromium content which also acts as a solid solution strengthener². However, when wear and corrosion are concurrent, the deleterious effect is usually synergic, requiring special alloys^{3, 4}.

The CoCrMoSi alloy system has shown better results under wear and corrosion-wear environments compared to carbides reinforced Co-based alloys. The superior performance is attributed to the presence of the hard intermetallic Laves phase in a lamellar eutectic and/or primary phase on the microstructure of the alloys (Laves phase is the Co, Mo and Si close-packed hexagonal (hcp) compound that can develop as Co₃Mo₂Si and/or CoMoSi)^{5, 6}.

Even though better wear and corrosion-wear results are observed due to the presence of the Laves phase, the low ductility and toughness of the alloys still limit many applications. Processing is also a challenge because of microstructure of the alloy is comprised of a large fraction of the hard Laves phase^7-9. Decreasing the Silicon and Molybdenum content on cast CoCrMoSi alloys seems to be a good way to reduce the hard phase volume fraction, thus improving the ductility and toughness^{8, 9}.

The production of welded coatings must consider the interaction between the deposition alloy and the substrate, as higher dilution induces lower hardness of the coatings. This reduction in hardness has been attributed to several factors, including the participation of the chemical elements (such as iron, chromium and nickel) from the steel substrates^10-12. Coatings are largely studied by way of dilution on single track deposits processed with different deposition current^{10, 11}. However, limited data are available regarding the processing of coated areas that require track overlap.

This study therefore evaluated CoCrMoSi alloy coatings in order to establish the correlation between the degree of track overlap on the PTA processing and the coatings features. To that end, single and multiple tracks were produced with 25 and 50% overlapping. Based on experimental results, the influence of overlapping degree on the microstructure, hardness and wear performance of the coatings was assessed.

2 Material and Methods

Atomized CoCrMoSi alloy with particle size ranging between 90 – 150 μm was deposited, as shown in Table 1. Single track with 100 mm length was processed on AISI 316L stainless steel substrate with thickness of 12.5 mm, as seen in Table 2. The extremities (20 mm) were discarded and the characterization was carried out in the middle of track length.

Table 1
Chemical Composition of the PTA alloy powder and steel substrate.

Alloy / Element	Chemical Composition, wt%
	Co	Cr	W	Mo	C	Fe	Ni	Si	Mn
CoMoCrSi – T400	Bal.	8.8	....	29.1	0.05	0.4	0.6	2.4	....
Substrate	Chemical Composition, wt%
	C	Mn	Si	P	S	Cr	Ni	Mo	Al
AISI 316L	0.02	1.35	0.43	0.03	0.01	16.78	10.12	2.13	0.002

Table 2
PTA processing parameters.

Parameters	First Track	Multiple Tracks
Shielding gas (l/min)	2	2
Protection gas (l/min)	15	15
Powder feeding gas (l/min)	2	2
Main arc current (A)	180	180
Powder feed rate	Constant in volume	Constant in volume
Travel speed (mm/min)	100	100
Distance torch / substrate (mm)	10	10
Electrode diameter (mm)	3.125	3.125
Overlapping	No	25 and 50%

First track coatings were evaluated concerning track geometry and dilution, seen in Figure 1a. The interaction with the substrate (dilution) was determined on the transverse cross-section by the ratio between the melted area of the substrate and the total melted area. Multiple tracks were processed with 25 and 50% overlapping to produce coated areas of 100 × 50 mm, as illustrated in Figure 1b and Figure 1c. The overlap displacement was determined by way of width of the first track and overlapping procedure considered the expression:

D_O = ((100 – O)/100)*W (1)

Where: D_O is the lateral linear displacement of overlapping (mm), O is the overlapping (%) and W is the width (mm) of the first track deposit.

Figure 1
Schematic showing the processing of first track and coatings with 25 and 50% overlapping.

The description and volume fraction of the microstructure were performed by scanning electron microscopy on the transverse cross section and Olympus Soft Imaging Solutions ^® software. The phases were identified using X-ray diffraction (XRD) analysis on the top surface of the coatings with K_αCu radiation from 20 to 120° with 1s time of exposure channel. Coatings hardness was measured on the transverse cross-section under 0.5 kgf load and results as an average of 5 measurements.

Wear performance of CoCrMoSi coated areas (25 and 50% overlapping) were assessed by abrasive sliding tests. Pins measuring 4 × 4 mm were cut out of the coatings and worn against silicon carbide paper (#220) assembled on a 63 HRC hardness metal disc, under 0.5 kgf axial load and 1.5 m/s tangential speed. Mass loss was measured by weighing pins before beginning tests and after each 250 m sliding distance up to 750 m, at room temperature.

3 Results and Discussion

3.1 Coatings integrity and track geometry

A visual inspection of the coatings revealed a smooth surface without welding defects. The first track of CoCrMoSi coating processed with 180 A deposition current exhibited 2.1 mm reinforcement thickness, 38° wettability angle (Θ) and 12.0 mm track width, as shown in Table 3. The high wettability expressed by the low angle Θ and large width (W) indicates processing quality coated areas is feasible.

Table 3
Geometry and dilution of deposited coatings.

CoCrMoSi Alloy - Tribaloy T400
Substrate	Evaluation	First Track	Coatings Multiple Tracks Coatings
	Overlapping	No	25%		50%
	Parameter	180 A	180 A		180 A
AISI 316L	Dilution (%)	38	17		13
	Reinforcement thickness, t (mm)	2.1	2.5		3.6
	Total Thickness (mm)	Not Applied	3.0		4.0
	Width, W (mm)	12.0	Not Applied
	Wettability Angle, Θ (0)	38
	Track Number	1	7	10
	Displacement on Overlapping (mm)	Not Applied	9	6

As can be seen in Equation 1, lateral linear displacement of 9 and 6 mm were used to produce coatings with 25 and 50% overlap (D_O). Compared to the first track (2.1mm), the reinforcement thickness (t) of the coatings increased to 2.5 and 3.6 mm as overlapping ranged from 25 and 50 %. Since the coatings fusion line is continuous for overlapping conditions, the real reinforcement (or total thickness of Co-based layer) was measured by the distance between the fusion line and the top of coatings, reaching 3.0 and 4.0 mm (Table 3).

3.2 Effect of track overlapping on the microstructure

The expected hypereutectic microstructure comprised of primary Laves phase and eutectic lamellar with Laves phase and Cobalt solid solution observed on cast CoCrMoSi alloy T400 was not identified on the first track of the coatings⁹. On the contrary, hypoeutectic Cobalt solid solution dendrites and interdendrictic eutectic lamellar (Laves phase and Cobalt solid solution) microstructure was observed, as shown in Figure 2. The differences in the microstructure are attributed to the high dilution measured for the first track (38%). It increased the amount of Iron, Chromium and Nickel on melting pool, changing therefore the chemical composition of the coatings, resulting in hypoeutectic microstructure, as observed previously on newly developed cast alloy^{9, 13}.

Figure 2
Hypoeutectic microstructure for first track of CoCrMoSi Coatings (180 A).

The dilution of the multi-track coatings was measured considering the melted area of stainless steel substrate and total melted area. An average dilution of 17% and 13% was measured for 25 and 50% track overlapping, respectively (Table 3). Compared with the first track, the dilution decreased 55 and 66%, confirming the direct dependence between dilution and track overlap degree. Once the overlapping induces dilution to decrease, the microstructure of the coatings is expected to change.

From the second track on, not just the stainless steel substrate melts but also the prior track, reducing then the amount of Iron, Chromium and Nickel on melting pool, changing the microstructure. Fully lamellar eutectic microstructure (Laves phase and Cobalt solid solution) was observed for 25% overlapping and a hypereutectic for 50% overlapping, as shown in Figure 3 and Figure 4, respectively. The lower dilution of 50% overlapping led to hypereutectic microstructure comprised of primary Laves phase and eutectic lamellar, as reported on cast CoCrMoSi alloy T400^[9].

Figure 3
Eutectic microstructure of PTA CoCrMoSi coating with 25% overlapping degree (180 A).

Figure 4
Hypereutectic microstructure of PTA CoCrMoSi coating with 50% overlapping degree (180 A).

Phase quantification indicated that the microstructure of the first track is comprised of 54% interdendrictic eutectic lamellar and 46% Cobalt solid solution dendrites. From the second track, the coatings with 25% overlapping showed microstructure 100% eutectic lamellar and the coatings with 50% overlapping presented 84% eutectic with 16% primary Laves phase, as seen in Figure 5.

Figure 5
Effect of processing on coatings microstructure.

Despite pronounced differences on the microstructure of the coatings, the main phases formed did not change. Cobalt solid solution (FCC) and Laves phase CoMoSi and Co₃Mo₂Si were observed for coatings, suggesting the measured dilution does not affect the developed phases but their volume fraction and distribution, as can be seen in Figure 6^{[5, 9, 12]}.

Figure 6
Developed phases on CoCrMoSi alloy coatings: (a) First Track and (b) Coatings.

Several studies have been carried out in order to improve CoCrMoSi T400 cast alloy ductility by way of the reduction of Molybdenum and Silicon alloying contents. As a result, the reduced volume fraction of Laves phase led to better ductility on cast alloys. Otherwise, the microstructure of the coatings depended directly on the track overlap. Since the microstructure varied from hypo to hypereutectic and different fraction of hard Laves phase was observed, the ductility of the coatings can be controlled and therefore better designed.

3.3 Coatings interface

The degree of interaction with the substrate and prior track altered the microstructure of the coatings. This section therefore provides details of the microstructure at the fusion line between tracks and track with steel substrate.

For the first track, the interface between coatings and stainless steel substrate showed an initial planar growth from 5 to 20 μm, as a continuous layer of Cobalt solid solution (Co SS). As the temperature on melting pool decreased, a Cobalt solid solution (Co-SS) columnar dendrictic narrow region was observed. Finally, a hypoeutectic microstructure of Cobalt solid solution dendrites and interdendrictic eutectic lamellar was identified among the bulk of the coatings, as seen in Figure 7a and Figure 8a, as a result of the higher amount of Iron, Chromium and Nickel near the interface.

Figure 7
Microstructure between Coatings and Steel Substrate for 25% overlapping: (a) First track, (b) Second track, (c) Third track and (d) Fifth track.

Figure 8
Microstructure between Coatings and Steel Substrate for 50% overlapping: (a) First track, (b) Second track, (c) Third track and (d) Fifth track.

For the second track on, for 25% and 50% overlapping degrees, the initial Cobalt solid solution planar growth was observed again, as well as an ensuing narrow columnar growth reaching a thickness of up to 100 μm. Furthermore, as constitutional undercooling increases and dilution decreases, two distinct microstructures were observed on the bulk of the coatings: lamellar eutectic for 25% overlapping degree and primary Laves phase in a lamellar eutectic for 50% overlapping. The planar growth observed and heretofore undescribed can be of relevance to reduction of the hardness gradient between substrate and T400 coatings.

With regard to the analysis of the interface between tracks, a coarsened Laves phase with spheroid shape within a eutectic was formed at the heat-affected zone, irrespective of overlapping degree. This microstructure extended from 500 to 800 μm thick, starting on the fusion line toward the top of the coatings for 25 and 50 % overlapping, as can be seen in Figure 9 and Figure 10. The thermal cycle due to successive welding passes induced Laves phase coarsening at inter-track heat-affected zone. This behavior was also observed on aging tests at 1000°C for T400 alloy PTA coatings¹⁴ and for laser cladding coatings ⁸.

Figure 9
Spheroid Laves phase on inter-track heat-affected zone: 25% overlapping.

Figure 10
Spheroid Laves phase on inter-track heat-affected zone: 50% overlapping.

3.4 Microstructure effect on hardness and wear performance

Co-based CoCrMoSi alloys are intermetallic reinforced materials and chemical composition is reported as the most important factor dictating volume fraction of Laves phase and, therefore, hardness and wear behavior^{9, 12, 14}. Since overlapping degree induced different interaction with the substrate causing microstructure to change, significant differences on coatings performance is likewise expected.

Indeed, the first observation that can be made is, the higher the interaction with the substrate, the lower the coatings hardness due to the reduction of Laves phase volume fraction (Figure 11). The lowest hardness (527 HV_0.5) was observed for the highest dilution which occurred on first track (or single track) deposits. The hypoeutectic solidification promoted lower volume fraction of Laves phase and lower amount of Cobalt solid solution alloying, as previously reported by literature ^{8, 9, 12}.

Figure 11
Hardness profile of first track and coatings.

A second observation is the higher track overlap, the higher the hardness of the coatings due to dilution decrease. In this way, the hardness reached 643 and 701 HV_0.5 for the coatings deposited with 25 and 50% overlapping, respectively. The observed microstructure and phase distribution, as well as the measured hardness are consistent with what has been predicted in the literature^{9, 12, 14}.

The hardness at the interface among tracks and steel substrate ranged from 480 and 500 HV_0.5, following the trend for hypoeutectic microstructure induced by higher Iron, Chromium and Nickel content. Otherwise, inter-track heat-affected zone showed hardness decrease, ranging from 580 – 590 HV_0.5, as a result of Laves phase coarsening, following the hardness reported previously for aged microstructures¹³.

The wear performance of the coatings was evaluated by way of abrasive sliding tests and reported as wear mass loss rate. The lower wear coefficient of 0.146 mg/m was obtained for hypereutectic microstructure of coatings (50% overlapping) in accordance with literature of such cast alloys^{5, 14}. Higher wear coefficients were measured for hypoeutectic first track (0.275 mg/m) and for eutectic microstructure of coatings produced with 25 % overlap (0.187 mg/m), as shown in Figure 12a.

Figure 12
Wear behavior of CoCrMoSi alloy coatings: (a) wear curves and (b) Mass loss rate.

Important differences in mass loss coefficient was measured, reaching 28 % increase since primary Laves phase was suppressed by 25 % overlapping and 88 % increase for hypoeutectic first track, as seen in Figure 12b. Higher overlapping led the chemical composition back to hypereutectic with primary Laves phase, resulting in higher hardness and better wear performance. Results revealed the effect of track overlap on the microstructure and properties of CoCrMoSi alloy coatings by PTA because it significantly altered the dilution with the substrate.

4 Final Remarks

This study analyzed the influence of overlapping on the microstructure and properties of the PTA CoCrMoSi coatings. The main contributions presented are as follows:

• -

  Track Overlap significantly altered the dilution with the substrate and, therefore, the microstructure of the CoCrMoSi coatings. The higher dilution observed for 25% overlapping induced the suppression of the primary Laves phase, changing the microstructure to a full eutectic.

• -

  The highest amount of Iron, Chromium and Nickel dictated the hypoeutectic microstructure at the interface between coatings and steel substrate. Otherwise, the inter-track heat-affected zone presented coarsened spheroid Laves phase as a result of welding thermal cycle. Thus, either chemical composition or thermal cycle affected the microstructure and hardness homogeneity of the coatings.

• -

  Overlapping did not change the formed phases but enabled controlling Laves phase fraction and distribution. The overlap altered the hypoeutectic microstructure of the single track to eutectic and then to hypereutectic. The degree of overlap also influenced the hardness and wear properties of the coatings, mainly because of high impact on the amount of Laves phase.

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Publication Dates

• Publication in this collection
  May-Jun 2015

History

• Received
  16 Oct 2014
• Reviewed
  01 May 2015