Experimental device for controlling strong dissipative plasma in black barrier area of spacecraft by pulsed magnetic field
A pulsed magnetic field and plasma technology, which can be used in instruments, teaching models, educational appliances, etc., can solve the problems of high power consumption, relieve the high quality of communication black-barrier systems, and poor communication reliability, and achieve high power utilization efficiency and small size. , the effect of simple device structure
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Embodiment 1
[0027] Embodiment one: if figure 1 As shown, an experimental device for controlling a strong dissipative plasma in a black barrier area of a spacecraft by a pulsed magnetic field involved in this embodiment includes a controllable power supply, a pulsed magnet, a casing, magnet leads, a magnet support structure and a plasma source, The outer surface of the shell and the plasma source are in the vacuum chamber, the inside of the shell is in the air, the pulse magnet and the supporting structure are located inside the shell, the end of the shell is a flange, and the flange is connected with the vacuum chamber, and the shell's The abdomen is fixed to the vacuum chamber through supporting feet; the magnet support structure is composed of a rod and a support block. The rod loads the magnet support structure into the shell and controls the rotation of the support structure. The rotating support is rotated; the magnet leads of the pulse magnet are drawn out from the support block a...
Embodiment 2
[0029] Embodiment two: if figure 1 , 3 As shown in and 4, a pulsed magnetic field involved in the present embodiment regulates an experimental device for controlling a strong dissipative plasma in a black barrier area of a spacecraft, the housing is a simulated spacecraft, and its structure is a cylindrical hollow structure, and The head is conical.
Embodiment 3
[0030] Embodiment three: as figure 1 , 6 As shown in and 7, a pulsed magnetic field involved in this embodiment regulates an experimental device for strongly dissipating plasma in the black barrier area of a spacecraft. The cross section of the pulse magnet is arched, the conductor cross section of the pulse magnet is rectangular, and the pulse magnet is wound with a multi-turn conductor.
[0031] The structure of the pulse magnet is similar to the racetrack structure, which is composed of two parallel conductors and two ring-shaped end conductors. The purpose is to generate a uniform magnetic field at a certain distance on the surface of the shell, such as Image 6 As shown, the cross-section of the pulse magnet is arched, such as Image 6 and 7 As we know, the conductor cross section of the pulse magnet (that is, the left view of the pulse conductor) is rectangular.
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