CONDUCTIVE LINE, TRANSFER DEVICE, AND SPACE SOLAR BEAM ENERGY TRANSPORTATION METHOD
[Problem] There has been a problem of addressing laser leakage onto the ground during power/energy transfer from the space to the ground for use in space solar power systems (SSPS) and the like. Further, a problem of lesser charge carriers has been caused in the case of adopting carbon?based material/organic material, which is more lightweight than copper, for conductive lines for the SSPS and the like for use in driving and power transfer in a space craft, a plant, a structure, and an aircraft. [Solution] The present invention provides a system that uses, during the power/energy transfer between the space and the air, photons of UV-C and the like having short wavelengths and being absorbed by molecules or atoms in the air including oxygen, and that comprises a light emitting part 1 and a light receiving part 2 for the photons. Regarding the conductive lines, the present invention proposes conductive lines, electrodes, and batteries which apply a carrier injection/introduction method for electric double layer transistors. The present invention also proposes an idea relating to induction, electric discharge, short-circuiting, and dielectric breakdown of positive/negative electric charges accumulated in the air by using the light emitting part 1 and the conductive lines.
» Number: WO2023228702A1 (A1)
» Publication Date: 30/11/2023
» Applicant: NISHIZAWA KATSUYAĆ¢??[JP]
» Inventor: NISHIZAWA KATSUYAĆ¢??[JP]
This project has received funding from the European Union's Horizon 2020 research and innovation programme under grant agreement Nº 768737