Ground charging method and system for satellite lithium battery

A ground charging and lithium battery technology, which is applied in secondary battery charging/discharging, battery disconnection circuit, battery circuit device, etc., can solve the problems of shortened service life of the battery pack, battery capacity attenuation, failure to fully charge the lithium battery, etc. Achieve the effect of avoiding leakage and burning and ensuring safety

Active Publication Date: 2019-09-06
CHINA ACADEMY OF SPACE TECHNOLOGY
View PDF5 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The traditional satellite nickel-hydrogen battery charging method is to use constant current charging, but this method is directly applied to lithium batteries, and there will be a problem that the lithium battery cannot be fully charged. In order to meet the requirements of a certain test item, it can only be charged multiple times.
[0004] Since lithium batteries must be connected in series in order to meet the requirements of the operating voltage, there is inconsistency between the individual batteries in the battery pack, and the difference caused by continuous charge and discharge cycles will accelerate the capacity decay of some individual batteries. The capacity of the battery pack is determined by the minimum capacity of the single battery, so these differences will shorten the service life of the battery pack

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Ground charging method and system for satellite lithium battery
  • Ground charging method and system for satellite lithium battery
  • Ground charging method and system for satellite lithium battery

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0044] Take the method of the present invention applied to the charging of a certain type of satellite before launch as an example.

[0045] In this embodiment, N=4 and M=2. In this embodiment, the satellite has two lithium battery packs, each lithium battery pack has an initial voltage of 3.3V and an upper limit voltage of 4.1V.

[0046] At the beginning, the voltage of each lithium battery pack is less than 3.3V, using such as Figure 5The shown system charges the lithium battery pack. The charging method is that the control system first controls the charging power supply to output 1.35A (C / 100) current to pre-charge the lithium battery pack. The control system collects the temperature and voltage of the satellite lithium battery pack. When After the voltage reaches 3.3V (monomer), control the charging power supply to output a constant current (C / 10). After charging to 4.1V, switch to constant voltage mode and step down charging. The step is 0 and the charging is terminated....

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention discloses a ground charging method and system for a lithium battery used for a satellite. According to the ground charging method, the lithium battery is pre-charged by trickle current to enable the voltage of the lithium battery to reach the initial voltage; then the lithium battery is charged by constant current until the upper limit voltage is reached; the process of decreasing the charging current and continuously charging the lithium battery until the upper limit voltage is reached is implemented for multiple times; and the charging process is finished when the current is decreased to the trickle current value and the upper limit voltage of the lithium battery is achieved through continuous charging. The system for implementing the ground charging method comprises a power supply, a charging power supply, a switch and a controller, wherein the controller controls the power supply and the charging power supply to supply power to the lithium battery. By adoption of the method and the system provided by the invention, the lithium battery can be fully charged; multiple times of charging for a certain test project can be avoided; and the risk of shortening the service life of the battery is greatly lowered.

Description

technical field [0001] The invention relates to a ground charging method and system for satellite lithium batteries, which are suitable for ground charging of satellite lithium batteries. Background technique [0002] Lithium-ion batteries have high weight / volume ratio energy, which can increase the load ratio of satellite platforms and reduce launch costs. At the same time, lithium-ion batteries have the advantages of small thermal effect, small self-discharge, and easy modularization. They have obvious advantages in aerospace applications. It has become the third generation of aerospace energy storage power after nickel-cadmium and nickel-hydrogen batteries. [0003] Projects such as the satellite full-star test, pyrotechnic program control function test, and three-system joint test all require lithium batteries to supply power, especially before the satellite is about to be launched. The battery needs to be fully charged. The traditional satellite nickel-hydrogen battery...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Patents(China)
IPC IPC(8): H01M10/44H02J7/00
CPCH01M10/441H02J7/0013H02J7/0031Y02E60/10
Inventor 谢华魏强张斯明李明峰戴萌余文涛杜磊
Owner CHINA ACADEMY OF SPACE TECHNOLOGY
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products