Figure1: Comparison of different nozzle configurations for high pressure dispersing of Aerosil 200 V Figure 1 shows some effects of downstream boundary conditions for the jet discharging from a nozzle. The diagram shows the particle size in suspension as a function of the specific dispersing energy. The particle size was analysed by dynamic light scattering. The pre-dispersed suspension enters the nozzle at high pressure and is forced to pass a hole of 0.08 mm in diameter. In the first configuration the dispersion discharges directly axial out of the nozzle into a fluid reservoir, resulting in a mean particle size of about 180 nm applying a pressure difference of 1,000 bar. An impingement of the jet directly after the outlet of the nozzle leads to further reduction of the mean particle size. The distance between the nozzle and the impingement plate is of prime importance as indicated in figure 1.
Figure2: Comparison of different systems for dispersing nano-particles (Aerosil 200 V) A comparison of different systems for dispersion is shown in figure 2. The usage of rotor stator systems results in no satisfying effect. An increase of the solid content leads to a slight improvement in dispersion efficiency, only. In contrast, ultrasound or high pressure systems enable to improve disruption efficiency and thus diminish clearly the mean agglomerate size. Compared to ultrasound high pressure systems are more efficient in terms of the specific energy EV. For achieving a mean particle size of 160 nm only 75 % of the specific energy is required when using optimised high pressure configurations compared to ultrasound. The dispersions were stable over several weeks without adding any surfactant. In contrast, dispersions produced by rotor stator systems are not stable due to their wide particle size distribution.
References [1] F. Hinze, 1. Dresdner Seminar Partikeltechnik 2000, 45. [2] H. Karbstein, Dissertation, Karlsruhe 1994. Acknowledgment Financial support was provided by the European Commission in the 6th framework program within the project PROFORM.
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