High-frequency and high-voltage electromagnetic microwave antigravity propelling system
A high-frequency high-pressure, propulsion system technology, applied in thrust reversers, using plasma, machines/engines, etc., can solve problems such as inability to generate thrust and anti-gravity effects, limited lifting space, and breakdown of air medium layers.
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Embodiment approach 1
[0049] The start-up operation sequence of the equipment is as follows: First, open the high-voltage controller 9, let the pressure doubler cylinder 8 carry out high-voltage loading on the asymmetrical capacitor composed of the small-area emitting needle 14 and the large-area receiving cavity 10, and let it work in the ion corona Under the discharge mode, and do not break down the air medium therein; then, turn on the cooling fan and the radio frequency controller, let the radio frequency electromagnetic field emitted by the magnetron 5, the transmission of the radio frequency head and the coaxial connector, launch pin 14 in a small area A strong radio frequency electromagnetic field is emitted from the tip, thereby exciting the air in the plasma state, producing a bright plasma flame, and greatly increasing the ion thrust generated by the asymmetric capacitor; finally, by operating and adjusting the radio frequency controller, the magnetron 5 can be changed The intensity of the...
Embodiment approach 2
[0051] By adjusting the current flowing between the two plates of the asymmetrical capacitor, the ejection speed of the plasma and the final thrust output of the thruster 6 can be adjusted and controlled.
[0052] When removing the microwave emitted by the magnetron 5 and only retaining the high voltage of the asymmetric capacitor, the current flowing through the asymmetric capacitor is reduced, while the voltage at both ends of the capacitor can remain constant; when increasing the microwave emitted by the radio frequency source 5 When the intensity, the output voltage of the asymmetric capacitor and other conditions are kept constant, the current flowing through the asymmetric capacitor will increase without causing the high voltage breakdown of the asymmetric capacitor, and finally the ions of the thruster 6 The thrust output increases accordingly.
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