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High-Temperature Aging Properties of Self-Developed High-Temperature Resistant Overlay Electrode - Literature Study Note

Literature Overview

This 1999 study by engineers from Jiangsu Lidai Building Materials Machinery Group Company investigates the high-temperature aging behavior of a self-developed overlay welding electrode designed for high-temperature service applications. In building materials machinery—particularly cement kilns, rotary dryers, and calcination equipment—wear parts are exposed to temperatures ranging from 400 to 900 °C, where conventional overlay materials lose hardness and wear resistance due to tempering and phase transformations. This research addresses the critical challenge of maintaining overlay performance under prolonged high-temperature exposure.

High-Temperature Service Requirements

The overlay electrode was designed for the following application conditions:

Application Component Operating Temperature (°C) Wear Mechanism Required Service Life
Kiln wear plates 600–900 Abrasive + thermal ≥ 12 months
Rotary dryer liners 400–700 Abrasive + erosion ≥ 18 months
Calciner refractory support 500–800 Abrasive + thermal fatigue ≥ 12 months
Fan blades (hot gas) 300–500 Erosion + oxidation ≥ 24 months
Chute liners 200–600 Abrasive ≥ 12 months

The key requirement is that the overlay material must maintain adequate hardness and wear resistance after prolonged exposure at the maximum service temperature, not merely at room temperature.

Electrode Design Philosophy

The self-developed electrode incorporates the following design principles for high-temperature performance:

Composition Strategy

Design Element Purpose Typical Range
High Cr content Form stable Cr₂O₃ scale and Cr-rich carbides 20–35 wt%
Mo addition Retain solution strengthening at high temperature 3–8 wt%
V or Nb addition Form stable carbides resistant to coarsening 1–3 wt%
Controlled C content Balance carbide volume fraction with matrix strength 1.5–3.5 wt%
Ni addition Stabilize austenite, improve hot hardness 5–15 wt%

Microstructural Design Goals

  1. High volume fraction of hard carbides (M₇C₃, M₆C, or Cr₇C₃) that resist coarsening at elevated temperature
  2. Stable matrix that does not undergo significant softening through tempering or phase transformation
  3. Thermal barrier oxide (Cr₂O₃) formation capability for oxidation resistance
  4. Thermal fatigue crack resistance through appropriate toughness retention

High-Temperature Aging Test Results

The aging tests were conducted at various temperatures for extended durations to simulate long-term service:

Aging Temperature (°C) Aging Time (h) Room Temperature Hardness Before Aging (HRC) Hardness After Aging (HRC) Hardness Retention (%)
400 100 52–55 50–53 96–98%
500 100 52–55 48–51 90–95%
600 100 52–55 45–48 82–88%
700 100 52–55 40–44 72–80%
800 100 52–55 35–38 62–70%
900 100 52–55 30–34 55–62%

Microstructural Changes During Aging

Aging Temperature Primary Microstructural Change Mechanism
400 °C Minimal change Carbon and alloy elements remain in solution
500 °C Slight carbide coarsening Early-stage Ostwald ripening
600 °C Noticeable carbide coarsening Diffusion-accelerated growth
700 °C Significant coarsening + matrix softening Carbon diffusion + carbide dissolution
800 °C Severe coarsening + phase transformation Matrix softening + carbide reversion
900 °C Extensive phase transformation Austenite → ferrite transformation + carbide dissolution

Comparative Performance with Conventional Electrodes

Electrode Type Room Temp Hardness (HRC) Hardness at 700°C after 100h (HRC) Retention at 700°C (%)
Conventional CrMo hardfacing 48–52 32–35 62–67%
Self-developed electrode 52–55 40–44 72–80%
Ni-base alloy overlay 35–40 33–36 83–90%
High-Cr cast iron overlay 50–54 38–42 72–78%

The self-developed electrode demonstrates superior high-temperature hardness retention compared to conventional CrMo hardfacing electrodes, approaching the performance of Ni-base alloys while maintaining significantly higher room-temperature hardness.

Engineering Application and Verification

The electrode was applied to kiln wear plates in a cement production line operating at approximately 700–800 °C. The field performance results confirmed:

Study Insights and Engineering Recommendations

This research highlights a fundamental principle in high-temperature overlay design: room-temperature hardness is not a reliable predictor of high-temperature service performance. The microstructural stability of the overlay at operating temperature is the governing factor for wear resistance retention.

Key engineering recommendations derived from this study:

  1. Always perform high-temperature aging qualification for overlay materials intended for elevated-temperature service. Room-temperature hardness testing alone is insufficient.
  2. The optimal Cr content for high-temperature applications is in the 25–35% range, providing both carbide stability and oxidation resistance.
  3. Mo and V additions are critical for maintaining solution strengthening at elevated temperatures, as these elements have low diffusivity and resist partitioning.
  4. Carbide morphology control during welding is essential—fine, uniformly distributed carbides resist coarsening better than coarse, segregated carbides.
  5. The service temperature threshold for this electrode class is approximately 800 °C; above this temperature, Ni-base alloy overlays become necessary.

This study represents an important contribution to the practical development of high-temperature overlay consumables for the building materials industry, where the cost-performance ratio of overlay solutions is critical for economic viability. The systematic aging test methodology employed provides a template for qualification testing of overlay materials for any high-temperature application.