Modularization reconfigurable method and device based on superconductive magnetic flux pinning connection

Abstract

The invention relates to a modularization reconfigurable method based on superconductive magnetic flux pinning connection and a simulation device applying the method. Particularly, interaction of an II-type high-temperature superconductor with a magnet and the characteristic of controllable magnetic field direction and size are utilized to establish reconfiguration of the modularization structure in a manner of establishing a superconductive magnetic flux pinning connecting interface. The magnetic flux pinning characteristic of the high-temperature superconductor in a superconducting state is fully utilized, the superconductive magnetic flux pinning connecting interface configured under the characteristic has certain rigidity and dampness and can be compared as connection by a spring having certain rigidity, and the superconductor can naturally enter the superconductive state in a space environment so that the reconfigurable method provides brand new developing idea for in-orbit assembly of a modularized spacecraft and has broad application prospect in the field of novel spacecraft development.

Description

technical field [0001] The present invention relates to a modular reconfigurable method based on superconducting magnetic flux pinning connections, and an implementation of a simulation device using the method, which utilizes the interaction between a type II high-temperature superconductor and a magnet, as well as the direction of the magnetic field and The size is controllable, and the reconstruction of the modular structure is completed by establishing a superconducting magnetic flux pinning connection interface. technical background [0002] With the continuous development of aerospace technology, the volume of spacecraft is also increasing, and the carrying capacity of any space vehicle is limited, and many large spacecraft will not be able to be launched into space as a complete independent assembly. Using launch vehicles to carry unassembled structural elements and then assemble them on orbit will be the construction method of many large-scale space agencies. At pres...

AI Technical Summary

Problems solved by technology

At present, the on-orbit assembly methods mainly include deployable structure construction, space forming structure construction, upright structure construction and formation flight construction, etc., but these construction methods have their own limitations.

The deployable structure construction method has complex structure, high failure rate, and high risk; the space forming structure construction method has low reliability in the manufacturing process, and the heat gradient during forming is uncontrollable; the vertical structure construction method involves dangerous artificial space operations or complex robot operations ; The navigation and attitude control of the formation flight construction method is complicated, and the energy consumption is huge, etc.

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