Inter-spacecraft near-field wireless energy transmission system

An energy transmission and near-field wireless technology, which is applied to the power supply system, electrical components, circuit devices and other directions of aerospace vehicles, and can solve the problems of high risk of mechanical interface stuck, exposed electrolytic port, complicated structure and difficult control.

Active Publication Date: 2019-09-27
BEIHANG UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The invention aims at the exposure of the electrolysis port, easy arc emission, high risk of mechanical interface jamming caused by the traditional wired electrical connection, and the complex structure and difficult control in the existing space-borne laser wireless energy transmission technology, which can only transmit energy in one direction and requires alignment accuracy. The shortcomings of high energy transmission efficiency and low overall energy transmission efficiency provide a near-field wireless energy transmission system between spacecraft. Energy transmission also greatly improves energy transmission efficiency, economical, safe, reliable and flexible

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  • Inter-spacecraft near-field wireless energy transmission system

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Embodiment Construction

[0032] The invention relates to a near-field wireless energy transmission system between spacecraft, which includes wireless energy signal terminals respectively arranged in each spacecraft, and the wireless energy transmission process occurs at any two wireless energy signal terminals satisfying a certain space distance Between, and each wireless energy signal terminal has two working states of wireless energy transmission and wireless energy reception;

[0033]The wireless energy signal terminal includes a spacecraft power controller, an inverter / rectifier circuit, and an energy transmitting / receiving circuit that are sequentially connected bidirectionally, and also includes a rectifier circuit that is unidirectionally connected to the inverter / rectifier circuit and the aerospace The voltage regulating circuit between the power supply controllers of the spacecraft. The power supply controller of the spacecraft controls the handshake control of the input and output of the spac...

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Abstract

The invention relates to an inter-spacecraft near-field wireless energy transmission system which comprises wireless energy signal ends arranged in various spacecrafts, wherein each wireless energy signal end has a wireless energy transmission operating state and a wireless energy reception operating state, and includes a spacecraft power controller, an inverter / rectifier circuit and an energy transmitting / receiving circuit which are in successively bidirectional connection and a voltage regulating circuit in unidirectional connection between the rectifier circuit in the inverter / rectifier circuit and the spacecraft power controller. The spacecraft power controller controls the input and output of the spacecraft energy and the handshake control of the energy transmission. The inverter / rectifier circuit inverts the DC power into high-frequency AC power or rectifies the high-frequency AC power into DC power. The energy transmitting / receiving circuit transmits an alternating electromagnetic field or receives the alternating magnetic field. The voltage regulating circuit regulates the voltage of the rectified DC power during energy reception. The system is provided with a structural body for energy transmission and reception to realize bidirectional peer-to-peer wireless energy transmission.

Description

technical field [0001] The invention relates to the technical field of wireless energy transmission, in particular to a near-field wireless energy transmission system between spacecraft. Background technique [0002] With the development of my country's aerospace technology and the deepening exploration of the unknown areas of outer space, the demand for improving the mission capability of spacecraft, ensuring the space safety of spacecraft, prolonging the life of spacecraft, reducing mission costs and failure risks has become increasingly strong. The research and development of space on-orbit service and maintenance technologies such as on-orbit connection, on-orbit assembly, on-orbit repair, replacement or disassembly have put forward urgent requirements. The safety, reliability, and convenience of power transmission between devices (functional modules) have put forward new requirements for the development of space power systems. Traditional technology connects the wired el...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02J50/20B64G1/42
CPCB64G1/42H02J50/20
Inventor 朱立颖刘治钢杨世春张晓峰马亮陈琦闫啸宇何红刘卿君
Owner BEIHANG UNIV
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