CLADTECH-LOGOCLADDING TECHNOLOGY SHANXI CO., LTD
CLADDING TECHNOLOGY SHANXI CO., LTD
CLADDING · BIMETAL PRODUCT · BIMETAL PRESSURE VESSEL TECHNICAL STUDY

Reciprocating Friction Wear Behavior of Nitrogen-Alloyed Overlay Alloy

Literature Overview

This study investigates the reciprocating friction wear behavior of a nitrogen-alloyed overlay alloy, examining the influence of nitrogen content on microstructure, hardness, friction coefficient, and wear rate under reciprocating sliding conditions. Nitrogen alloying is an emerging approach to enhancing the surface properties of hardfacing alloys, offering the potential for improved hardness and wear resistance through the formation of nitrogen-rich phases and the modification of the matrix microstructure. The reciprocating wear mode is particularly relevant for applications such as reciprocating pumps, valve components, and engine cylinder liners.

Core Technical Points

Nitrogen alloying modifies the overlay microstructure in several key ways. First, nitrogen increases the hardness of the austenitic matrix through solid solution strengthening. Second, nitrogen promotes the formation of nitrogen-rich carbide phases such as CrN and Cr2N, which are harder than conventional carbides. Third, nitrogen affects the phase balance between austenite and martensite, generally stabilizing the austenitic phase and increasing the retained austenite content.

The study examines nitrogen contents ranging from 0.2 wt% to 1.5 wt%, revealing a non-linear relationship between nitrogen content and wear performance. The optimal nitrogen content for reciprocating wear resistance is approximately 0.5–0.8 wt%, beyond which the wear rate increases due to the formation of brittle nitride phases that are prone to fracture under reciprocating loading.

Nitrogen Content (wt%) Hardness (HRC) Friction Coefficient Wear Rate (mg/mm) Retained Austenite (%)
0.2 55 0.42 28.5 35
0.5 62 0.38 18.2 42
0.8 66 0.35 12.6 48
1.0 68 0.37 15.8 52
1.2 65 0.40 22.3 55
1.5 60 0.45 32.1 58

Microstructural Analysis

The nitrogen-alloyed overlay exhibits a microstructure consisting of a tempered martensitic matrix with dispersed CrN and Cr2N nitride particles. At low nitrogen contents (0.2–0.5 wt%), the nitrides appear as fine, uniformly distributed particles within the matrix. At intermediate nitrogen contents (0.5–0.8 wt%), the nitride particles coarsen slightly and begin to form clusters near grain boundaries. At high nitrogen contents (1.0–1.5 wt%), the nitrides form large, irregular aggregates that can serve as crack initiation sites.

The retained austenite content increases with nitrogen content due to the austenite-stabilizing effect of nitrogen. At 1.5 wt% nitrogen, the retained austenite content reaches 58%, which is significantly higher than in the nitrogen-free counterpart. While retained austenite can improve toughness through transformation-induced plasticity, excessive amounts compromise the dimensional stability and may lead to delayed cracking during cooling.

Reciprocating Wear Mechanisms

The reciprocating wear behavior was analyzed using scanning electron microscopy (SEM) of the worn surfaces. Three distinct wear mechanisms were identified:

  1. Adhesive wear: Dominant at low nitrogen contents (0.2–0.5 wt%), characterized by material transfer between the overlay and the counterface. The relatively soft matrix is susceptible to adhesive bonding with the counterface, leading to material removal through shearing of the adhesive junctions.
  2. Abrasive wear: Dominant at intermediate nitrogen contents (0.5–0.8 wt%), characterized by ploughing and cutting of the overlay surface by hard asperities on the counterface. The hard nitride particles embedded in the matrix resist abrasive removal, while the matrix material is gradually worn away.
  3. Fatigue wear: Dominant at high nitrogen contents (1.0–1.5 wt%), characterized by subsurface crack initiation and propagation beneath the worn surface. The large, brittle nitride aggregates act as stress concentrators, initiating microcracks that propagate under cyclic loading and lead to surface spalling.

The transition from abrasive to fatigue wear at high nitrogen contents is the primary reason for the increase in wear rate beyond 0.8 wt% nitrogen. The brittle nitride aggregates reduce the fatigue life of the overlay surface, leading to premature failure through spalling rather than gradual material removal.

Friction Behavior

The friction coefficient decreases with increasing nitrogen content up to 0.8 wt%, then increases at higher nitrogen contents. The minimum friction coefficient of 0.35 occurs at 0.8 wt% nitrogen, which corresponds to the optimal wear performance. The reduction in friction coefficient is attributed to the formation of a protective tribofilm composed of iron oxides and nitrogen-containing compounds that form on the worn surface during reciprocating sliding.

At high nitrogen contents, the increase in friction coefficient is attributed to the increased surface roughness resulting from nitride aggregate spalling. The rough surface increases the real contact area and promotes adhesive bonding, leading to higher friction and accelerated wear.

Engineering Practice Implications

The nitrogen-alloyed overlay alloy offers a promising approach for applications requiring high wear resistance under reciprocating sliding conditions. The optimal nitrogen content of 0.5–0.8 wt% provides a good balance between hardness, toughness, and wear resistance. This alloy system is particularly suitable for reciprocating pump components, valve seats, and engine cylinder liners where reciprocating wear is the dominant failure mechanism.

For production welding, the nitrogen-alloyed overlay alloy requires careful process control to maintain the nitrogen content within the optimal range. Nitrogen pickup from the atmosphere during welding can exceed the intended nitrogen content, particularly in processes with inadequate shielding. The use of a high-purity argon shielding gas with oxygen content below 50 ppm is recommended to minimize unwanted nitrogen pickup.

The overlay alloy is susceptible to hydrogen cracking due to the nitrogen-induced increase in hardness. Preheating to 150–200 °C and post-weld stress relief at 550–600 °C are essential for preventing cracking in thick-section applications. The post-weld heat treatment should be performed within 4 hours of welding to minimize the risk of hydrogen-induced cracking.

Study Insights and Reflections

The study demonstrates that nitrogen alloying is a powerful tool for enhancing the wear resistance of overlay alloys, but the benefits are limited to a narrow composition window. The non-linear relationship between nitrogen content and wear performance highlights the importance of composition optimization in alloy design. Engineers should avoid the temptation to maximize nitrogen content for maximum hardness, as this leads to detrimental effects on wear performance.

The identification of three distinct wear mechanisms as a function of nitrogen content provides a valuable framework for understanding the wear behavior of nitrogen-alloyed overlays. This framework can be applied to other alloy systems and wear conditions to predict and optimize the wear performance of nitrogen-alloyed materials. The study also underscores the importance of matching the alloy composition to the specific wear mechanism present in the application, rather than relying solely on hardness as a predictor of wear performance.