Abstract:We investigated the spatial-temporal dynamics characteristics of the spark-plasma-jet (SPJ) in the nitrogen of 0.1 MPa at different pulse energies by fast photography and optical emission spectrum. The spark plasma generated by spark discharge can be rapidly sprayed out of the micro-incentive cavity within several tens nanoseconds under the action of electric field, and the spraying delay time reduces gradually with increase of pulse energy. The outlet velocity of SPJ reaches up to 10 4 m s −1 . After that, th… Show more
“…The plasma propagation velocity drops sharply to 0.75 km s −1 in 4 μs, and then slowly decreases to zero in around 30 μs. The average velocity of the plasma is calculated to be 0.56 km s −1 for this spark discharge, similar to previous relevant reports on spark plasma jets [28,29].…”
“…N 2 (C-B) can be found in the region of 380-450 nm [34]. A second positive band of nitrogen molecules is detected at between 450 nm and 550 nm [35], and the first positive band is measured at between 620 nm and 700 nm [28,36]. The nitrogen atom was measured at 780 nm and the oxygen atom at 610 nm [36].…”
Section: Spectral Characteristicsmentioning
confidence: 89%
“…This is because increasing the applied voltage can improve the discharge energy and transferred charge, which are input into the spark reactor when the air gap is broken down. The increased energy and charge enable the plumes to propagate to a longer distance [28][29][30].…”
Section: Optical Characteristicsmentioning
confidence: 99%
“…where C is around 0.33 F and U 2 is around 3 kV. Then E is estimated to be 1.48 J, which is large enough to generate a peak current with a magnitude of several hundred amperes [28,32].…”
Section: Electrical Characteristicsmentioning
confidence: 99%
“…The ICCD images mainly reveal the time evolution of the discharge particle optics and motion trajectory. In addition, the spark discharge rapidly heats and presses the gas, and the gas is exhausted through the small holes to form a gas jet stream at a velocity of up to 10 km s -1 [28]. With the ICCD images, the velocity v of spark plasma can be estimated by…”
Atmospheric pressure low-temperature plasma is a promising tool in biomedicine applications including blood coagulation, bacterial inactivation, sterilization, and cancer treatment, due to its high chemical activity and limited thermal damage. It is of great importance to develop portable plasma sources that are safe to human touch and suitable for outdoor and household operation. In this work, a portable and rechargeable low-temperature plasma spark discharge device (130 mm×80 mm× 35 mm, 300 g) was designed. The discharge frequency and plume length were optimized by the selection of resistance, capacitance, electrode gap, and ground electrode aperture. Results show that the spark plasma plume is generated with a length of 12 mm and a frequency of 10 Hz at a capacitance of 0.33 μF, resistance of 1 MΩ, electrode gap of 2 mm, and ground electrode aperture of 1.5 mm. Biological tests indicate that the plasma produced by this device contains abundant reactive species, which can be applied in plasma biomedicine, including daily sterilization and wound healing.
“…The plasma propagation velocity drops sharply to 0.75 km s −1 in 4 μs, and then slowly decreases to zero in around 30 μs. The average velocity of the plasma is calculated to be 0.56 km s −1 for this spark discharge, similar to previous relevant reports on spark plasma jets [28,29].…”
“…N 2 (C-B) can be found in the region of 380-450 nm [34]. A second positive band of nitrogen molecules is detected at between 450 nm and 550 nm [35], and the first positive band is measured at between 620 nm and 700 nm [28,36]. The nitrogen atom was measured at 780 nm and the oxygen atom at 610 nm [36].…”
Section: Spectral Characteristicsmentioning
confidence: 89%
“…This is because increasing the applied voltage can improve the discharge energy and transferred charge, which are input into the spark reactor when the air gap is broken down. The increased energy and charge enable the plumes to propagate to a longer distance [28][29][30].…”
Section: Optical Characteristicsmentioning
confidence: 99%
“…where C is around 0.33 F and U 2 is around 3 kV. Then E is estimated to be 1.48 J, which is large enough to generate a peak current with a magnitude of several hundred amperes [28,32].…”
Section: Electrical Characteristicsmentioning
confidence: 99%
“…The ICCD images mainly reveal the time evolution of the discharge particle optics and motion trajectory. In addition, the spark discharge rapidly heats and presses the gas, and the gas is exhausted through the small holes to form a gas jet stream at a velocity of up to 10 km s -1 [28]. With the ICCD images, the velocity v of spark plasma can be estimated by…”
Atmospheric pressure low-temperature plasma is a promising tool in biomedicine applications including blood coagulation, bacterial inactivation, sterilization, and cancer treatment, due to its high chemical activity and limited thermal damage. It is of great importance to develop portable plasma sources that are safe to human touch and suitable for outdoor and household operation. In this work, a portable and rechargeable low-temperature plasma spark discharge device (130 mm×80 mm× 35 mm, 300 g) was designed. The discharge frequency and plume length were optimized by the selection of resistance, capacitance, electrode gap, and ground electrode aperture. Results show that the spark plasma plume is generated with a length of 12 mm and a frequency of 10 Hz at a capacitance of 0.33 μF, resistance of 1 MΩ, electrode gap of 2 mm, and ground electrode aperture of 1.5 mm. Biological tests indicate that the plasma produced by this device contains abundant reactive species, which can be applied in plasma biomedicine, including daily sterilization and wound healing.
Capillary discharge based pulsed plasma thrusters have great prospects of applications in in-orbit maneuvering of<bold/> micro-nano satellites. In this paper, the influence of different capillary cavity structure parameters on the thruster's energy deposition process, ablation characteristics, output thrust parameters and plasma plume parameters under an energy level of 5 J were studied. The experimental results indicate that the increase of the inner diameter of the capillary cavity will significantly reduce the discharge current density, which leads the deposition energy and equivalent power to decrease; the increase of the cavity length helps to improve the energy transfer efficiency. The influence of cavity structure on the ablation characteristics is reflected in the influence of deposition energy per unit area on the tube wall temperature. When the inner diameter of the capillary increases from 1 mm to 3 mm, the ablation mass decreases significantly, and then the equivalent ablation mass remains approximately unchanged as the inner diameter of the cavity increases further; the ablation mass continues to increase as the capillary length increases, while the ablation mass per unit area continues to decrease. The impulse bit depends on the ablation mass and plasma plume velocity, and the difference in ablation characteristic further affects the plasma in the cavity. The density and equivalent pressure determine the plasma electrothermal acceleration process. The continuous increase in the diameter and length of the capillary cavity will induce the acceleration process to lag behind the discharge and ablation process. And the decrease of the deposited energy impedes the electrothermal acceleration process, which results in the decrease of the impulse bit, specific impulse, and the overall efficiency. Furthermore, the overall efficiency transfer model analysis indicates the influence of the capillary inner diameter on thruster efficiency is mainly reflected in the energy transfer efficiency, and the capillary length change mainly affects the electrothermal acceleration efficiency. The overall efficiency optimization of the thruster needs to start from increasing both energy deposition efficiency and acceleration efficiency.
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