Abstract
With copper/steel composite pipe as research object, two-dimensional numerical simulation of explosive welding process was conducted through AUTODYN finite element software with SPH and ALE methods. The dynamic welding process and boundary effect were analyzed, and the explosive welding tests of copper/steel composite pipe were conducted. Results indicate that under the action of detonation waves, the composite pipe obliquely collides with the base pipe. The pressure in the collision zone remains stable at the order of 1
Explosive welding of metals involves metal physics, explosion, and welding technique, which can achieve high-quality solid metallurgical combination of different metal pipe combinations. Currently, explosive welding technique can achieve welding of similar or different metals and alloys of more than 260 types, which has been widely used in the engineering fiel
In the actual production, the edges of products manufactured by explosive welding may be unwelded or torn, namely the explosive welding boundary effects, which affects the quality of welding products and wastes metal material. Zhang et a
Copper, as a traditional thermal conductive rolling material, has been widely used in the metallurgy, power, and chemical industries. Stainless steel has the advantages of fine corrosion resistance, high strength, good fatigue resistance, good pressure resistance, and relatively low cost. Therefore, the copper/stainless steel composite pipes have wide application prospects due to their high thermal conductivity, fine corrosion resistance, and good mechanical strength. Based on AUTODYN software, a two-dimensional explosive welding model of copper/steel bimetal pipe was established through SPH and ALE algorithms in this research to simulate and analyze the explosive welding process of copper/steel composite pipe. The process parameters, such as velocity, pressure, and effective plastic strain, were discussed, and the simulated and experimental interface morphologies were compared to verify the accuracy of numerical simulation. Normally, the explosive welding causes boundary effect. In this research, the length of the composite pipe and explosive was increased to decrease the boundary effect. Numerical simulation and corresponding analyses of this new model were conducted, and the boundary effect of the composite pipe was studied.
The calculation process of explosive welding of copper/stainless steel pipe was simulated by AUTODYN software. Combined with the physical process of explosive welding, the two-dimensional model used SPH method to effectively and accurately simulate the steel pipe and copper pipe, avoiding the grid distortion. ALE method was used to simulate the explosives and moulds. ALE method could adaptively adjust and maintain high-quality grids, which was suitable for fluid structure coupling problem

Fig.1 Two-dimensional model of explosive welding of T2/316L composite pipe
Material | Length | Height |
---|---|---|
316L | 30 | 0.4 |
T2 | 30 | 0.4 |
ANFO | 30 | 2.8 |
Mould | 30 | 3.0 |
Jones Wilkins Lee (JWL) state equation was selected as the state equation of explosives, which is a semi-empirical state equation without detonation products by chemical reaction. This state equation could accurately describe the process of expansion-driven work produced by detonatio
(1) |
where P is the pressure of the detonation product; V is the
relative volume of the detonation product; E0 is the initial specific internal energy; e is the initial internal energy; A, B, R1, R2, and ω are related parameters. The state equation can describe the relationship between various physical quantities (pressure, specific volume, temperature, internal energy) in the detonation system after explosion. Thus, it is often used in the explosive welding simulation. Combined with the theoretical value of explosive welding windo
Relative volume of detonation product, V/m· | Density, ρ/kg· | Initial specific internal energy, E0/GJ | A/GJ | B/GJ | R1 | R2 | ω |
---|---|---|---|---|---|---|---|
3750 | 900 | 2.48 | 49.46 | 1.89 | 3.91 | 1.11 | 0.33 |
Shock state equation is suitable to characterize the dynamic behavior of materials under severe deformation. Mie-Gruneisen state equation was selected to simulate the steel pipe and copper pipe and to describe the basic relationship between particle velocity and impact velocity of SPH algorithm. The expression of this state equatio
(2) |
with
(3) |
(4) |
(5) |
(6) |
where Γ0 is the Gruneisen coefficient; Γρ is a constant; ρ0 and ρ are the initial density and current density of the material, respectively; p and pH are the material impact pressure and current pressure, respectively; eH is the material impact internal energy; μ is the compression ratio; s is the material constant; c0 is the volume sound velocity of the material. The parameters of the Mie-Gruneisen material model used in this research are shown in
Material | Gruneisen coefficient, Γ0 | Volumetric sound velocity, c0/m· | Constant, s | Initial temperature, Tr/K |
---|---|---|---|---|
316L | 2.17 | 4569 | 1.49 | 300 |
T2 | 1.99 | 3940 | 1.49 | 294 |
Johnson-Cook constitutive equation can accurately describe the relationship between stress and strain and that between strain rate and temperature under large deformation. Thus,
(7) |
where σ is flow stress for Von Mises; A is the initial yield stress; B is the hardening constant; εp is the equivalent plastic strain; is the equivalent plastic strain rate; n is the hardening index; C is the strain rate constant; m is the thermal softening index; is a dimensionless temperature; Tmelt and Troom represent the melting temperature of the material and room temperature, respectively. The Johnson-Cook material model parameters are shown in
Material | Density, ρ/kg· | Initial yield stress, A/MPa | Hardening constant, B/MPa | Hardening index, n | Strain rate constant, C | Thermal softening index, m | Melting temperature, Tmelt/K |
---|---|---|---|---|---|---|---|
316L | 7980 | 280 | 1250 | 0.76 | 0.021 | 0.82 | 1680 |
T2 Mould |
8930 7896 |
90 350 |
292 275 |
0.31 0.36 |
0.025 0.022 |
1.09 1 |
1356 1811 |

Fig.2 Simulated explosive welding process: (a) 0 ms, (b) 2.73×1

Fig.3 Simulated interface morphology of explosive welding process (a); relationship between Y velocity and time of different feature points (b); enlarged morphologies of unwelded area A (c1), straight area B (c2), wave area C (c3), smooth wave area D (c4), vortex wave area E (c5), and straight area F (c6) in Fig.3a
With the stable detonation of explosive, the interface presents a flat and straight interface in
When the composite pipe collides with the base pipe, huge pressure is generated at the collision point. During explosive welding of copper/steel composite pipe, the pressure distribution at 3.77×1

Fig.4 Pressure distribution on copper/steel composite pipe at 3.77×1
The pressure-time curve of the feature points in the middle part of the composite pipe shows the similar variation: the peak pressure value has the order of magnitudes of 1
The materials near the interface produce serious plastic deformation during explosive welding, thus forming plastic deformation zone. A clear narrow plastic deformation band appears near the collision zone. The effective plastic strain cloud map at 3.77×1

Fig.5 Distribution of effective plastic strain at 3.77×1
The distribution cloud diagram of shear stress in copper/steel composite pipe at 3.77×1

Fig.6 Shear stress nephogram of copper/steel composite pipe

Fig.7 Boundary effect at starting position (a) and ending position (b)
The boundary effect is caused by not only the insufficient energy generated by explosive detonation at the initial stage and ending stage, but also the effect of explosive rarefaction wave. To eliminate the boundary effect, the composite pipe, explosive length (extending of 5 mm at both ends), explosive initiation position, and other unchanged model parameters should be added into the original model, as shown in

Fig.8 Boundary effect in extended copper/steel composite pipe model: (a) overall model; (b) starting position; (c) ending position
The properties of the extended model are shown in

Fig.9 Relationship of Y velocity (a) and pressure (b) with time of different feature points
To conduct the explosive welding experiment of copper/steel composite pipe, the geometric parameters of copper/steel composite pipe are 10 times larger than those of the numerical simulation parameters, as shown in
Material | Length | Inside diameter | Thickness |
---|---|---|---|
316L | 300 | 28 | 4 |
T2 | 300 | 48 | 4 |

Fig.10 Appearances of copper/steel composite pipe: (a) side appearance; (b) cross-section appearance; (c) longitudinal-section appearance
The detailed waveform at area A–C in

Fig.11 Interface morphologies of waveform at area A (a), area B (b), and area C (c) in Fig.10a
1) Under the action of explosive detonation waves, the copper/steel composite pipe is accelerated and collides obliquely with the base pipe. When the explosive explodes stably, the pressure is at the order of magnitude of 1
2) The velocity, pressure, and effective plastic deformation at the initial position and end position of the explosion are all lower than the normal values. Besides, boundary effect exists in the explosive welding. The boundary effect can be eliminated by extending the composite pipe and explosive, which increases the binding energy at the edge.
3) The established numerical model of explosive welding is reasonable and reliable to simulate the explosive welding process of copper/steel bimetal pipe. In the simulation, the interface morphology changes from straight line to wave shape with the propagation of the explosion wave, which is consistent with the actual interface morphology of the T2/316L bimetal composite pipe after explosive welding.
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