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STEEL PIPE · FITTING · WELDING TECHNICAL STUDY

Deformation Prevention Measures for Large Diameter Overlay Welded Tube Plates

Literature Overview

This paper by Han Quanyong from Offshore Oil Engineering Co., Ltd. Huizhou Branch addresses the significant engineering challenge of controlling distortion during overlay welding of large diameter tube plates used in petrochemical heat exchange equipment. Published in Guangdong Chemical Engineering (Volume 43, Issue 12, 2016), the study focuses on a common but critical problem: the management of welding-induced deformation in large, thin-walled plate structures that require stainless steel overlay for corrosion protection.

Core Technical Challenge

Large diameter tube plates in petrochemical heat exchangers typically have diameters exceeding 1500 mm with thicknesses of 30–80 mm. The overlay welding of stainless steel on these plates introduces substantial thermal stresses that can cause significant distortion, including:

The deformation is particularly problematic because tube plates must maintain precise flatness to ensure proper sealing at the tube-to-tube-plate joints and at the shell-to-tube-plate connection.

Root Cause Analysis of Deformation

The deformation mechanisms in large diameter overlay welded tube plates can be understood through the following analysis:

Deformation Type Primary Cause Contributing Factors Severity
Warping Asymmetric heat input from one-sided welding Welding sequence; plate thickness; material thermal expansion mismatch High
Bowing Compressive stresses in overlay layer Overlay thickness; base material yield strength;拘束 conditions Moderate
Local buckling High compressive stresses in thin overlay Overlay thickness; interpass temperature;拘束 rigidity Moderate
Dimensional drift Cumulative thermal expansion and contraction Total heat input;拘束 conditions; cooling rate Low to Moderate

The fundamental cause of all deformation types is the thermal stress induced by the welding process. When stainless steel is deposited on a carbon steel base, the thermal expansion coefficient mismatch (stainless steel: ~17.3 × 10⁻⁶/°C vs. carbon steel: ~12.2 × 10⁻⁶/°C) creates additional stresses during cooling.

Deformation Prevention Measures

The paper proposes several deformation control strategies that can be categorized as follows:

Pre-Welding Measures

  1. Mechanical restraint: Use of heavy backing plates, clamping fixtures, or temporary stiffening ribs to restrict plate movement during welding.
  2. Pre-heating: Uniform pre-heating of the entire plate to 100–150°C to reduce the thermal gradient and minimize differential expansion.
  3. Symmetric design: Designing the welding sequence to ensure symmetric heat input distribution around the plate diameter.

During Welding Measures

  1. Symmetric welding sequence: Welding in a balanced pattern—typically starting from the center and working outward in concentric rings, or using a back-and-forth pattern from opposite edges.
  2. Reduced heat input: Using lower welding currents and higher travel speeds to minimize the heat-affected zone and reduce thermal distortion.
  3. Multi-pass thin layers: Depositing multiple thin layers rather than fewer thick layers to reduce peak temperatures and thermal gradients.
  4. Interpass temperature control: Maintaining interpass temperatures below 150°C to prevent excessive cumulative heat input.

Post-Welding Measures

  1. Mechanical straightening: Cold straightening or hot straightening to correct residual deformation within acceptable limits.
  2. Stress relief annealing: Heat treatment at 550–650°C for 2–4 hours to reduce residual stresses and improve dimensional stability.
  3. Vibration stress relief: Application of controlled vibration to reduce residual stresses without thermal treatment.

Process Parameter Optimization

The following table summarizes the recommended welding parameters for large diameter tube plate overlay welding:

Parameter Recommended Range Rationale
Welding current 180–250 A (SMAW); 250–350 A (FCAW) Reduced heat input to minimize distortion
Travel speed 150–250 mm/min Higher speed reduces heat input per unit length
Layer thickness 2–3 mm per pass Thin layers reduce peak temperature and thermal gradient
Interpass temperature < 150°C Prevents excessive cumulative heat input
Pre-heat temperature 100–150°C Reduces thermal gradient and cracking susceptibility
Post-weld stress relief 550–650°C for 2–4 hours Reduces residual stresses and improves dimensional stability

Engineering Practice Implications

For offshore and petrochemical applications, the deformation control of overlay welded tube plates is particularly critical because:

The paper's emphasis on a comprehensive approach—combining pre-welding, during-welding, and post-welding measures—reflects the practical reality that no single measure is sufficient to control deformation in large diameter tube plates.

Key Questions and Reflections

Several important questions arise from this study:

The systematic approach to deformation control presented in this paper is directly applicable to many other large plate overlay welding applications in the petrochemical and offshore industries.

Summary and Study Insights

This paper provides a practical and comprehensive framework for deformation control in large diameter overlay welded tube plates. The emphasis on a multi-faceted approach—combining mechanical restraint, symmetric welding sequences, reduced heat input, and post-weld stress relief—reflects the practical engineering reality that deformation control requires a holistic strategy. For engineers working on similar projects, the key takeaway is that deformation prevention must be planned from the design stage through to post-weld inspection, and that no single measure is sufficient to achieve acceptable dimensional control. The systematic approach presented here can serve as a template for developing deformation control procedures for other large plate overlay welding applications.