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Acta Metall Sin  2025, Vol. 61 Issue (5): 699-716    DOI: 10.11900/0412.1961.2023.00289
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Effect of Boron on Solidification Behavior, Strength-Toughness, and Wear Resistance of Fe-Cr-B-C Alloy
ZHAO Guangdi1(), LI Yang1, YAO Xiaoyu2, WANG Liang3, LI Weibin3, PAN Yuhua1, LI Weijuan1, WANG Zhaoyu1
1 School of Materials and Metallurgy, University of Science and Technology Liaoning, Anshan 114051, China
2 Shi -changxu Innovation Center for Advanced Materials, Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China
3 Liaoning Fengde Wear Resistant New Material Product Co. Ltd., Anshan 114018, China
Cite this article: 

ZHAO Guangdi, LI Yang, YAO Xiaoyu, WANG Liang, LI Weibin, PAN Yuhua, LI Weijuan, WANG Zhaoyu. Effect of Boron on Solidification Behavior, Strength-Toughness, and Wear Resistance of Fe-Cr-B-C Alloy. Acta Metall Sin, 2025, 61(5): 699-716.

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Abstract  

The Fe-Cr-B-C alloy is a new wear-resistant boron cast iron alloy developed from high-chromium cast iron. This alloy is inexpensive, easy to process, and exhibits excellent wear resistance and good formability, making it suitable for the manufacturing of wear-resistant parts with high dimensional accuracy. The Fe-Cr-B-C alloy has great potential for application and is gradually replacing chromium wear-resistant alloys. In recent years, studies have shown that after composition optimization, the Fe-Cr-B-C alloy can be directly used in the as-cast state without subsequent heat treatment, resulting in a significant decrease in cost. Thus, optimization of the composition of the Fe-Cr-B-C alloy is of great significance for the development of wear-resistant materials. The strength-toughness and wear resistance of the boron cast iron mainly depend on the characteristics of the B-rich precipitates. Reasonable control of the B addition can optimize the characteristic of the B-rich precipitates, thereby improving the service properties of the as-cast Fe-Cr-B-C alloy. However, the role of B in the Fe-Cr-B-C alloy has been scarcely investigated. Therefore, the effects of B content on the solidification behavior, as-cast microstructure, hardness, impact toughness, and wear resistance of the Fe-Cr-B-C alloy were examined in this study. The results show that with increasing B content, the liquidus temperature and formation temperature of precipitates significantly decrease, the formation range of precipitates expands, and the solidification temperature range first increases and then decreases. At a B content of 0.0006% (mass fraction), the solidification of the Fe-Cr-B-C alloy proceeds as follows: L→δγ dendrite→primary Nb(C, B)→eutectic [γ + Cr7C3]. After solidification, the dendrite arm comprised of martensite, and the interdendritic region was composed of residual γ and trace amounts of Nb(C, B), [γ + Cr7C3]. With the increase in the B content to 0.51%, the growth of γ dendrites was significantly hindered, resulting in the refinement of the dendritic structure. The solidification process changed to L→γ dendrite→primary (Fe, Cr)2(B, C)→primary Nb(C, B)→eutectic [γ + (Fe, Cr)2(B, C)]. After solidification, martensitic transformation occurred in both the interdendritic region and dendrite arms, and a continuous boron-carbide network was formed along the interdendritic region. With the further increase in B content to 2.89%, a large amount of boron-carbide was formed at the initial stage of solidification, which not only caused the disappearance of the dendritic structure but also consumed most of the B atoms, seriously reducing the hardenability of γ matrix and inhibiting its martensite transformation. The solidification process changed to L→primary γ→primary (Fe, Cr)2(B, C)→eutectic [γ + (Fe, Cr)2(B, C)]→peritectic [γ + (Fe, Cr)2(B, C) + (Fe, Cr)3(C, B)]. The alloy with a B content of 0.0006% possesses the highest impact toughness, and moderate Rockwell hardness and wear resistance. The alloy with a B content of 0.51% possesses the highest Rockwell hardness, optimal wear resistance, and moderate impact toughness. The alloy with a B content of 2.89% possesses the lowest Rockwell hardness and impact toughness, and the poorest wear resistance. The change in boron-carbide characteristic and the martensitic transformation of matrix are the main reasons for the significant differences in strength-toughness and wear resistance among these alloys. The obtained results provide a theoretical basis for optimizing the composition and improving the wear resistance of the as-cast Fe-Cr-B-C alloy.

Key words:  Fe-Cr-B-C alloy      B      solidification behavior      boron-carbide      strength-toughness      wear resistance     
Received:  07 July 2023     
ZTFLH:  TG113.1  
Fund: National Natural Science Foundation of China(51904146)
Corresponding Authors:  ZHAO Guangdi, Tel: (0412)5929381, E-mail: gdzhao12s@alum.imr.ac.cn

URL: 

https://www.ams.org.cn/EN/10.11900/0412.1961.2023.00289     OR     https://www.ams.org.cn/EN/Y2025/V61/I5/699

Fig.1  Schematics of sampling positions and sizes in the ingots (unit: mm)
(a) stereoscopic view (b) cross section view
Fig.2  Relationships between mass fraction of equilibrium precipitated phases and temperature in Fe-Cr-B-C alloys with B contents of 0.0006% (No.1) (a), 0.51% (No.2) (b), and 2.89% (No.3) (c) (L—liquid phase, γ—austenite, δ—delta ferrite)
Fig.3  XRD spectra of the Fe-Cr-B-C alloys with different B contents (α—ferrite)
Fig.4  Low (a-c) and high (d-f) magnified OM images of the Fe-Cr-B-C alloy ingots with B contents of 0.0006% (a, d), 0.51% (b, e), and 2.89% (c, f)
Fig.5  Low (a-c) and high (d-f) magnified BSE images of the Fe-Cr-B-C alloy ingots with B contents of 0.0006% (a, d), 0.51% (b, e), and 2.89% (c, f) (Inset in Fig.5a shows the thin strip-like phases precipitated along grain boundaries)
Fig.6  EDS results of points A1 (a), B1 (b), A2 (c), B2 (d), and A3 (e) marked in Figs.5d-f (Insets in Figs.6d and e show the enlarged views of B and C peaks)
Fig.7  Differential thermal analysis (DTA) cooling curves of the Fe-Cr-B-C alloys with B contents of 0.0006% (a), 0.51% (b), and 2.89% (c) (Cooled from super-solidus temperature with cooling rate of 10 oC/min; P-C1, P-C2, and P-C3 represent the exothermic peaks)
Fig.8  Low (a-c) and high (d-f) magnified OM images of the solidified DTA samples of Fe-Cr-B-C alloys with B contents of 0.0006% (a, d), 0.51% (b, e), and 2.89% (c, f) (Inset in Fig.8c is the high magnified OM image)
Fig.9  BSE images and EDS elemental distribution maps of interdendritic regions of solidified DTA samples of Fe-Cr-B-C alloys with B contents of 0.0006% (a), 0.51% (b), and 2.89% (c)
Fig.10  OM images of as-quenched microstructures of Fe-Cr-B-C alloys with B contents of 0.0006% (a), 0.51% (b), and 2.89% (c)
Fig.11  BSE images of as-quenched microstructures of Fe-Cr-B-C alloys with B contents of 0.0006% (a, b), 0.51% (c), and 2.89% (d)
Fig.12  EDS analysis of the strip-like precipitate in Fig.11a (a), and the spectral line scanning along the yellow arrows in Fig.11b (b), Fig.11c (c), and Fig.11d (d)
Alloy

Rockwell hardness

HRC

Impact toughness

J·cm-2

No.156.67 ± 0.568.40 ± 0.30
No.260.07 ± 0.173.40 ± 0.25
No.341.43 ± 0.131.80 ± 0.17
Table 1  Average Rockwell hardnesses and impact toughnesses of Fe-Cr-B-C alloy ingots with different B contents
AlloyInterdendritic region

Dendrite

arm

γ matrix[γ + Cr7C3]

Primary

(Fe, Cr)2(B, C)

[γ + (Fe, Cr)2(B, C)][γ + (Fe, Cr)2(B, C) + (Fe, Cr)3(C, B)]
No.1421 ± 38848 ± 35-571 ± 56---
No.2739 ± 23851 ± 89--1540 ± 51599 ± 76-
No.3--275 ± 74-2245 ± 537550 ± 137603 ± 115
Table 2  Average Vickers microhardnesses of different areas in Fe-Cr-B-C alloy ingots with different B contents (HV)
Fig.13  Impact fracture surfaces of Fe-Cr-B-C alloy ingots with B contents of 0.0006% (a, d, g, j), 0.51% (b, e, h, k), and 2.89% (c, f, i, l)
(a-c) macro morphologies of the fracture surfaces (d-f) low magnified SEM images of the cracks (g) Nb-rich boron-carbide along cracked grain boundaries (h, i) cracks at (Fe, Cr)-rich boron-carbides/matrix interface (j) Cr-rich carbide along cracked grain boundaries (k, l) cracked (Fe, Cr)-rich boron-carbides
Fig.14  EDS results of precipitates on the impact fracture surfaces of Fe-Cr-B-C alloy ingots with different B contents
(a) Nb-rich boron-carbide in No.1 alloy
(b) Cr-rich carbide in No.1 alloy (c, d) Fe, Cr-rich boron-carbides in No.2 (c) and No.3 (d) alloys (Insets show the corresponding high magnified curves)
Fig.15  Friction coefficient-time curves of Fe-Cr-B-C alloy ingots with different B contents
Fig.16  Low (a-c) and high (d-f) magnified OM images of the worn surfaces of Fe-Cr-B-C alloy ingots with B contents of 0.0006% (a, d), 0.51% (b, e), and 2.89% (c, f)
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