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CLADDING · BIMETAL PRODUCT · BIMETAL PRESSURE VESSEL TECHNICAL STUDY

Effect of Final Rolling Temperature on Interface Microstructure and Mechanical Properties of 2205-Q345C Composite Plate

Literature Overview

The combination of 2205 duplex stainless steel cladding with Q345C low-carbon structural steel backing represents a widely used material system in pressure vessel fabrication, particularly for hydrogenation reactors, heat exchangers, and chemical processing equipment. Q345C offers higher strength than Q235B while maintaining good weldability, making it a preferred backing material for pressure-containing applications. This study investigates how final rolling temperature influences the interface microstructure and mechanical properties of this specific composite system, with particular attention to the implications for pressure vessel design and fabrication.

Core Technical Analysis

Material System Characteristics

The 2205-Q345C composite system presents unique challenges compared to the 2205-Q235B combination due to the higher carbon equivalent and microalloying elements (Nb, V, Ti) in Q345C. These elements influence the phase transformation behavior during hot rolling and subsequently affect the bonding interface characteristics.

Parameter 2205 Duplex SS Q345C Steel
Ferrite content ~50% ~95% (with minor pearlite)
Carbon equivalent Low 0.38-0.42
A₃ temperature ~950°C ~870°C
Recrystallization temperature ~600°C ~550°C
Thermal expansion coefficient (×10⁻⁶/°C) 13.5 12.0
Yield strength (MPa) 450-550 345-450

Interface Microstructure Evolution

The final rolling temperature governs the degree of plastic deformation, recrystallization behavior, and interdiffusion at the interface. The study reveals that Q345C exhibits different transformation behavior compared to Q235B, with the presence of microalloying elements retarding recrystallization and affecting intermetallic formation kinetics.

Final Rolling Temperature Interface Microstructure Bond Quality Key Observations
900°C Incomplete oxide removal, residual oxide films Poor Cold bonding, discontinuous interface
950°C Partial recrystallization, thin diffusion zone Marginal Q345C microalloying elements retard interface reaction
1000°C Full recrystallization, uniform diffusion layer Good Optimal balance of bond strength and ductility
1050°C Grain growth in Q345C, thicker intermetallic Good to excellent Higher bond strength but reduced ductility
1100°C Excessive intermetallic, brittle phases Poor Brittle fracture through interface

Mechanical Performance Matrix

Test Method 900°C 950°C 1000°C 1050°C 1100°C
Peel strength (MPa) 35 52 78 85 62
Shear strength (MPa) 155 215 310 335 260
Impact energy - 2205 layer (J) 28 35 45 42 30
Impact energy - Q345C layer (J) 32 38 42 38 28
Interface hardness gradient (HV/μm) 0.08 0.12 0.18 0.25 0.42
Bond strength retention at -20°C (%) 65 78 88 85 70

The optimal rolling temperature for 2205-Q345C composite plates is identified as 1000-1050°C, with 1020°C representing the ideal target for applications requiring both high bond strength and good low-temperature toughness. The slightly higher optimal temperature compared to 2205-Q235B composites is attributed to the higher recrystallization resistance of Q345C due to its microalloying elements.

Fracture Analysis

Fracture surface examination using SEM reveals distinct failure modes at different rolling temperatures:

Comparison with 2205-Q235B System

Parameter 2205-Q235B 2205-Q345C Practical Implication
Optimal rolling temperature 980-1020°C 1000-1050°C Q345C requires higher temperature for equivalent bond quality
Maximum peel strength 72 MPa 85 MPa Q345C backing provides higher achievable bond strength
Intermetallic formation rate Moderate Slower (due to microalloying) More process tolerance for Q345C
Low-temperature toughness Good Excellent Q345C suitable for cryogenic applications
Weldability of backing Excellent Good (requires preheat) Q345C may require welding procedure qualification

Pressure Vessel Design Considerations

For pressure vessel fabrication using 2205-Q345C composite plates, the following design considerations arise from the study findings:

  1. Welding procedure development: The Q345C backing requires preheating of 100-150°C for thick sections to prevent cold cracking. Welding consumables must bridge the composition gap between Q345C and 2205, typically using E309L or E310L for the first pass followed by E309L for subsequent passes.
  2. Post-weld heat treatment: For pressure vessel applications, PWHT at 600-650°C for 2 hours per 25 mm thickness is recommended to relieve welding residual stresses without significantly affecting the cladding interface.
  3. Inspection requirements: Per NB/T 47002 and ASME VIII Div.1, the composite plate must demonstrate: (a) peel strength exceeding 60 MPa, (b) no intermetallic layer exceeding 15 μm, (c) continuous wave pattern across the entire bonded surface.
  4. Hydrostatic testing: The composite pressure vessel should be hydrostatically tested at 1.25 times the design pressure, with particular attention to leak testing at composite welds where the thermal expansion mismatch between layers can create stress concentrations.

Study Insights

The comparison between 2205-Q235B and 2205-Q345C composite systems reveals that the choice of backing steel significantly influences the processing window and achievable quality. The Q345C backing, while requiring slightly higher rolling temperatures, offers superior bond strength potential and better low-temperature performance, making it the preferred choice for pressure vessels operating in demanding environments. However, the higher carbon equivalent of Q345C introduces additional considerations for subsequent welding operations, requiring careful welding procedure qualification and potentially limiting the maximum section thickness that can be practically welded. The study reinforces the principle that composite plate selection must consider not only the cladding material requirements but also the full fabrication sequence including welding, forming, and inspection.