Meaning
Spatial coordinates of the standing shock wave generated in supersonic gas jets determine the location of the highest pressure gradients relative to the nozzle exit. The mach disk position marks the boundary where the flow transitions from supersonic to subsonic speed, causing a sudden rise in density and temperature. Controlling this position is essential to prevent the molten metal stream from freezing prematurely at the tip of the delivery tube.
Flow Dynamic
High gas pressures force the stream into an under-expanded state, forming expansion and compression waves. Adjusting the supply pressure shifts this shock structure relative to the nozzle face. This movement changes the aspiration pressure at the metal tip.
Atomization Efficiency
Positioning the shock wave correctly ensures that the molten metal encounters the highest possible gas velocity for efficient disintegration. If the shock wave is too close, it can push liquid metal back onto the nozzle, causing severe blockages. When positioned too far, the gas loses kinetic energy, resulting in coarser, non-spherical powder that does not meet battery-grade standards.
Nozzle Maintenance
Incorrect alignment of the shock structure can cause local turbulence that accelerates the physical wear on the delivery tube tip. This accelerated wear leads to asymmetric gas flows and necessitates more frequent replacements of expensive ceramic parts. Technical teams monitor the shock structure to minimize mechanical stress on the nozzle components and extend the continuous operating lifetime of the atomization chamber.
Implementing a real-time optical tracking system to verify this position helps prevent costly shut-downs and reduces the total cost of ownership of the atomization equipment for high-purity powder production.