2.1. The structure of Pyro-Breaker
The structure of the pyro-breaker is illustrated in
Figure 1. Functionally, it is divided into two main units: the isolated unit and the current unit. The isolated unit comprises the isolated contact, upper current lead, insulation cylinder, explosion chamber 1, and explosive tube 1. The current unit consists of the epoxy support plate, lower current lead, and cutting grid. Additionally, the current conversion unit includes an epoxy support plate, lower current lead, cutting grid, current contacts, explosion chamber 2, and explosive tube 2.
The structural design of the pyro-breaker utilizes a series connection of the upper and lower current leads, which are effectively integrated into the main circuit. In this configuration, the current initially flows through the upper current lead, then passes through the isolated contact to the center current lead. From there, the current flows through the current contact, ensuring efficient current conduction before exiting through the lower current lead. Upon detection of the quench signal, the detonation device immediately sends a detonation signal to the detonator and explosives. The resulting explosion generates a powerful blast wave that quickly propagates through the transmission medium to the contact surface. The shock wave causes the current contact to be divided into several segments, each with a distinct gap. This separation leads to the formation of a high-voltage arc between the segments, which facilitates the rapid transfer of circuit current to the discharge resistance. The arc is extinguished by high-velocity deionized water from explosion chamber 2, while the gap between the segments is completely filled with uncontaminated deionized water. This process maintains insulation for several milliseconds, ensuring the successful interruption of the circuit. Simultaneously, the isolated insulation cylinder, subjected to the blast pressure from explosion chamber 1, moves downward, severing the isolated contact and providing long-term high-strength insulation through the insulation cylinder.
2.2. Current Unit Modelling
As illustrated in
Figure 1, the pyro-breaker current contact adopts a copper thin-walled cylindrical configuration featuring seven equally spaced weakening notches on its outer surface. Each notch maintains dimensional specifications of 0.5 mm in depth and 1 mm in height. Current implementations in major tokamak devices (ITER, JT-60SA, K-STAR) predominantly employ V-notch geometries. This study proposes an innovative R-notch configuration, with comparative analysis of dynamic fracture characteristics between the two notch types conducted through integrated LS-DYNA simulations and experimental detonation tests.
The fracture process of the current contact primarily involves two nonlinear problems: one is the near-field explosion problem, in which the blast wave and explosion products interact with the water; the other is the fluid-solid coupling problem, in which the shock wave in the water interacts with the copper cylinder. Due to the complexity of these nonlinear problems involving multiple material interactions, obtaining an analytical solution is challenging. Therefore, this study employs LS-DYNA simulation software to analyze the dynamic fracture process of the contact structure under different notch configurations, subjected to blast shock wave loading, using a fluid-solid coupling algorithm.
Due to the structural symmetry of the explosive and current contact, and to reduce computational time, the simulation is modeled using only a single fracture unit. Based on the actual structure of the pyro-breaker, the numerical model consists of five components: explosive, water, air, copper, and epoxy. The model dimensions are consistent with those of the physical prototype, as shown in
Figure 2. The explosive is represented as an elongated cylinder with a radius of 0.5 cm and a height of 4 cm. The copper cylinder has a wall thickness of 0.2 cm and a height of 4 cm, while the epoxy component is 1 cm in height. The surrounding air domain has a diameter of 10 cm. To evaluate the fracture performance, both V-notch and R-notch are introduced at the midpoint of the current contact as intentional weak points. Except for the notch geometry, all other parameters are kept identical for comparative analysis.
The model adopts a unit system based on cm-g-µs, where the explosive, water, and air are represented using Eulerian meshes, while the copper and epoxy cutting grids are modeled using Lagrangian meshes. This approach allows for precise tracking of the deformation, displacement, and other mechanical responses of the solid components, accurately reflecting their physical behavior under explosive impact. A fluid-solid coupling algorithm is applied between the Eulerian and Lagrangian grids, enabling the bidirectional transfer of forces, displacements, and other physical quantities between the fluid and solid domains, ensuring a cohesive and coordinated simulation system. Fixed constraints are applied to the periphery of the epoxy cutting grid to effectively limit its displacement and simulate real-world working conditions. Non-reflective boundaries are set at the upper and peripheral ends of the air domain to prevent wave reflections from interfering with the simulation results. This study comprehensively simulates the entire dynamic process of the current unit, from the initial stable state through explosion impact, energy release, pressure transfer, and disconnection. Ultimately, the differences in fracture time and fracture spacing between the two contact structures are successfully revealed.
The explosive used in this study is high-density RDX, modeled using the MAT_HIGH_EXPLOSIVE_BURN material model. The Jones-Wilkins-Lee (JWL) equation of state is employed to describe the relationship between explosion pressure, internal energy, and relative volume. The equation is expressed as follows:
where
p is the burst pressure,
A, B,
R1,
R2 and
ω are parameters obtained by experimental fitting.
The deformation and rupture of the copper are the primary focus of this study. Given that the copper undergoes a wide range of strains, strain rates, and temperatures under explosive loading, the Johnson-Cook material model is employed. The equation is expressed as follows:
where σ is the flow stress, ɛ is the equivalent plastic strain, T is the homologous temperature, and A, B, C, m, and n are the material constants determined experimentally.
2.3. Analysis of Numerical Simulation
As illustrated in
Figure 3, the propagation process of the shock wave following an explosive detonation is demonstrated using a V-notch as an example. The detonation commenced at time zero at the central point atop the explosive charge. At 1.5 µs, high-temperature, high-pressure gaseous detonation products began forming ahead of the detonation wavefront, expanding radially outward. Concurrently, the detonation wave traversed the explosive column and entered the surrounding aqueous medium, generating a secondary shock wave. The detonation wave velocity was approximately 4.5 times the speed of sound in water.
By 7.5 µs, the blast wave reaches the base of the explosive charge, signifying complete detonation. During the 1-7.5 µs interval, the wavefront pressure exceeds 10,000 MPa as the blast wave propagates within the column. By 12 µs, a hemispherical shockwave forms at the current contact interface. As this wave propagates toward the interface wall, its intensity attenuates significantly. By 19.5 µs, upon reaching the current contact wall, the shockwave pressure has diminished to several hundred MPa. Subsequently, the current contact structure undergoes severe elastic-plastic deformation under shock loading, ultimately leading to structural failure through material rupture.
Figure 4 chronologically presents the fracture progression in V-notch (top) versus R-notched (bottom) current contact interfaces, where positive values represent compressive stresses and negative values indicate tensile stresses. At 75 µs, initial surface fracture occurs at the outer region of the R-notch interface, whereas the V-notch counterpart remains in the plastic deformation phase. By 84 µs, complete fracture propagates through both surfaces of the R-notch, while the V-notch interface continues to exhibit pronounced bending deformation. The V-notch initiates outer surface fracture at 106.5 µs, coinciding with further propagation of the fracture in the R-notch. Final fracture completion occurs at 115.5 µs for the V-notch, accompanied by continued elongation of the fracture in the R-notch. Comparative analysis reveals that the R-notch achieves complete failure at 84 µs, representing a 27.3% reduction in fracture time compared to the 115.5 µs required for the V-notch interface.
Figure 5 presents a comparison of the stress response at the notches of the current contact structures. As shown in the figure, both notch configurations reach their maximum forward compressive stress at 31.49 µs. The V-notch contact exhibits a higher peak compressive stress of 51.44 MPa, compared to 36.99 MPa for the R-notch contact. When the shock wave reaches the outer surface of the copper material, a tensile wave is reflected due to the presence of the free boundary.
According to the stress curves, the R-notch contact reaches a maximum tensile stress of 225.20 MPa at 72 µs, while the V-notch contact reaches a higher tensile stress of 251.40 MPa at 99 µs. Following rupture, the internal stress of the contact rapidly drops to zero. It is observed from
Figure 6 that the R-notch contact fractures at 75 µs, while the V-notch contact fails at 106.5 µs.
Analysis of the stress curves indicates that fracture initiation is primarily driven by the reflected tensile wave generated by the initial blast-induced shock wave. Consequently, fracture tends to initiate at the outer surface rather than through direct shear failure from the inner surface.
As shown in
Figure 6, the fracture behavior differs significantly between the two notch profiles. The fracture surface of the R-notch exhibits notably greater flatness compared to that of the V-notch. Furthermore, its fracture interface is in complete adhesion with the epoxy grating, whereas a visible gap is present between the fracture surface of the V-notch and the epoxy plane. According to the fracture spacing graph in
Figure 6c, the final fracture spacing of the R-notch reaches 0.94 cm, which is 46.9% greater than that of the V-notch (0.64 cm).