Research on Reducing Residual Stress at Weld Joints Through Internal Surface Weld Overlay of Nozzles

1. Definition and Fundamental Principles

Residual stress at weld joints constitutes one of the most critical integrity concerns in pressure vessel and piping fabrication, particularly at nozzle-to-shell connections where geometric discontinuities, thermal gradients, and constraint factors converge to produce severe stress concentrations. The research addressed in this study focuses on the application of internal surface weld overlay to nozzle internals as a deliberate engineering strategy to mitigate residual stress levels at critical weld joints through controlled thermal cycling, metallurgical redistribution, and stress-relaxation mechanisms.

The fundamental principle underlying this approach rests on several interrelated phenomena:

2. Category and Business Positioning

This research falls squarely within the company's core competency in weld overlay engineering, specifically positioned at the intersection of:

Within the broader business framework of Cladding Technology Shanxi Co., Ltd, this research entry represents a knowledge-management and process-engineering asset. It documents lessons learned, establishes best-practice parameters, and creates a replicable methodology that can be applied across multiple product lines — from refinery reactor nozzles to nuclear-grade piping spools and cryogenic service vessels.

3. Technical Purpose and Value

3.1 Primary Technical Objectives

  1. Quantify residual stress reduction: Establish measurable stress reduction percentages (typically 30–60%) achievable through specified overlay parameters on nozzle internal surfaces.
  2. Define optimal process windows: Identify the range of heat input, interpass temperature, wire feed rate, and travel speed that maximizes stress relief while maintaining overlay integrity.
  3. Validate metallurgical compatibility: Confirm that the overlay weld metal does not introduce deleterious microstructural changes (e.g., martensitic transformation, carbide precipitation, or hot cracking susceptibility) in the base metal weld joint.
  4. Develop acceptance criteria: Establish NDT-based and stress-measurement-based acceptance thresholds for the overlay process.

3.2 Value Contribution

4. Key Process and Implementation Points

4.1 Pre-Overlay Preparation

Successful residual stress reduction through internal nozzle overlay requires meticulous surface preparation and pre-existing weld joint characterization:

4.2 Overlay Welding Parameters (TIG Method — Recommended for Internal Nozzle Surfaces)

Parameter Typical Range Rationale
Shielding Gas 99.99% Ar or Ar/He (75/25) Prevents oxidation; He blend improves heat input for thick sections
Heat Input 0.8–2.5 kJ/mm Must be sufficient to induce plastic relaxation without excessive HAZ softening
Interpass Temperature 80–150 °C (low); 150–250 °C (stress-relaxation mode) Higher interpass temps enhance stress relaxation via creep
Wire Diameter 1.6 mm or 2.4 mm (ER309L, ER316L, or ER2209) Selected per base metal composition and service environment
Travel Speed 30–60 mm/min Controls dilution and bead geometry; slower speed increases thermal cycling effect
Number of Passes 2–4 layers Multiple passes create cumulative thermal cycling for progressive stress relief
Current (DCEN) 80–180 A Dependent on wire diameter and travel speed
Voltage 12–18 V Controls arc length and bead width

4.3 Implementation Sequence

  1. Baseline stress measurement: Record residual stress distribution at the nozzle weld toe using strain gauges (per ASTM E2228) or the center-hole drilling method.
  2. First overlay pass: Apply a thin root pass with low heat input to establish a metallurgically sound bond without excessive thermal distortion.
  3. Subsequent passes: Increase heat input progressively for passes 2–4 to maximize thermal cycling effect on the underlying weld joint.
  4. Post-overlay stress measurement: Repeat residual stress measurement at identical locations and calculate percentage reduction.
  5. NDT of overlay: Perform dye penetrant inspection (PT per ASTM E709) and, where required, ultrasonic testing (UT per ASTM E1655) of the overlay layer.
  6. Documentation: Compile all parameters, measurements, and results into a formal PQR/WPS package.

4.4 Alloy Selection Matrix

Base Metal Recommended Overlay Key Consideration
Carbon steel (SA-106 Gr.B, SA-516 Gr.70) ER309L (310S equivalent) High dilution tolerance; Cr/Ni balance prevents cracking
Low-alloy steel (SA-387 Gr.11/22) ER309L or ER310 Higher Ni content compensates for higher CE of base metal
Austenitic stainless (SAF-304, SAF-316) ER309L or ER347 Match or slightly exceed base Cr/Ni; avoid 304L to prevent sensitization
Stellite / Hardfacing service ER309L transition + ER2209 or Stellite 6 Transition layer required; final layer for wear/corrosion resistance
Cr-Mo steels (SA-335 P91/P92) ER309L (thin) + ER316L Minimize thermal input; avoid exceeding 250°C interpass

5. Applicable Standards and Acceptance Criteria

5.1 Governing Standards

5.2 Acceptance Criteria for the Overlay Process

Criterion Acceptance Threshold Method
Residual stress reduction ≥30% reduction in peak tensile stress at weld toe Strain gauge (ASTM E2228)
Overlay penetration Full fusion to base metal; no lack of fusion RT (ASME V Art.4) or MT
Overlay surface quality No porosity > 2 mm, no cracks, no undercut PT (ASTM E709)
Overlay thickness uniformity ±0.5 mm of nominal; no thin spots < 1.5 mm UT thickness measurement
Microstructure (HAZ) No martensite in 309L weld; no brittle phases at interface Macro/Micro examination (ASTM E3)
Hardness (overlay) ≤35 HRC (for austenitic); within spec for hardfacing ASTM E18 (Rockwell C)

6. Common Risks and Controls

6.1 Risk Identification and Mitigation

Risk Mechanism Mitigation Strategy
Hot cracking in overlay Low-melting-point impurities (S, P) segregate at grain boundaries during solidification Use low-sulfur/low-phosphorus filler (ER309L); control heat input; preheat if CE > 0.45
Excessive HAZ softening Overheating during multiple overlay passes reduces base metal strength Monitor interpass temperature with thermocouples; limit passes to 4 maximum
Weld distortion of nozzle Asymmetric thermal input causes angular or bowing distortion Alternate welding direction; use backing plate; apply symmetric heat input
Incomplete stress relief Insufficient heat input fails to reach relaxation temperature in base metal Validate heat input calculations; use thermal imaging to confirm base metal temperature
Contamination of overlay Internal nozzle surfaces may contain mill scale, oil, or moisture Mandatory cleaning per AWS D1.1; gas-flow verification before and during welding
Post-overlay hydrogen cracking Dissolved hydrogen diffuses to high-stress regions post-weld Apply post-weld bake (150–200°C for 2h) or use low-hydrogen consumables

6.2 Quality Assurance Controls

7. Application Across the Company's Three Technology Routes

7.1 TIG/MIG Weld Overlay Route

This research directly strengthens the company's TIG/MIG weld overlay capability by providing:

Specific product applications include:

7.2 Hydraulic Explosive Bonding Route

While hydraulic explosive bonding (hydroforming-assisted bonding) is primarily a solid-state joining process, the residual stress research contributes indirectly through:

7.3 Explosion Welding Route

The research findings extend to explosion welding applications in the following ways:

8. Conclusions and Strategic Recommendations

The research on residual stress reduction through internal nozzle surface weld overlay represents a significant knowledge asset for Cladding Technology Shanxi Co., Ltd. It transforms the company's overlay capability from a purely corrosion-protection service into a comprehensive structural integrity enhancement offering. Key strategic actions recommended include:

  1. Formalize the research into a qualified WPS/PQR package compliant with ASME Section IX and GB/T 12466, making it available for client submission and regulatory approval.
  2. Develop a standardized stress-measurement protocol (per ASTM E2228) to be offered as a value-added service alongside overlay work, providing clients with quantifiable proof of stress reduction.
  3. Extend the methodology to MIG overlay for thicker sections and higher production-rate applications, developing parallel WPS packages for both TIG (precision) and MIG (throughput) methods.
  4. Integrate residual stress reduction claims into marketing and technical proposals for high-integrity applications (nuclear, offshore, critical refinery units) where fatigue life extension and SCC resistance are primary client concerns.
  5. Establish a continuous improvement loop by collecting field performance data from deployed overlay work and updating process parameters based on actual service outcomes.

By leveraging this research to build qualified procedures, generate traceable stress-reduction data, and position the company as a provider of integrity-enhanced overlay solutions, Cladding Technology Shanxi Co., Ltd can command premium pricing in high-specification markets while delivering measurable risk reduction to end-users.