Unlock instant, AI-driven research and patent intelligence for your innovation.

Lithium battery aging test system capable of simulating high-altitude temperature, humidity and pressure

An aging test, lithium battery technology, applied in closed-circuit television systems, measuring electricity, measuring devices, etc., can solve the problems of inability to apply to aerospace low-voltage environments, inaccurate measurement data, etc., to achieve the effect of convenient connection and accurate data collection

Pending Publication Date: 2022-04-29
CIVIL AVIATION FLIGHT UNIV OF CHINA
View PDF9 Cites 1 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

If you want to obtain accurate test data, you need to place the aging process test cabinet in a designated single environment, but the metering device used to measure the pressure drop change during the aging process works in a single environment, and the measurement data is extremely inaccurate Therefore, the existing technology can only carry out the aging process in a single environment to ensure the normal operation of the metering device
And it is not suitable for the complex environment during high-altitude flight
[0006] Therefore, when the existing test battery aging process is tested, it cannot be applied to the low-voltage environment of aerospace, and its flight environment is a typical environment of lithium variable voltage, variable temperature, low pressure and different humidity

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
  • Lithium battery aging test system capable of simulating high-altitude temperature, humidity and pressure
  • Lithium battery aging test system capable of simulating high-altitude temperature, humidity and pressure

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0030] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0031] see Figure 1-Figure 2 , the present invention provides a technical solution: a lithium battery aging test system that can simulate high-altitude temperature, humidity, and pressure, such as figure 1 As shown, the test system includes a data acquisition system 13, a temperature controller, a humidity controller, a pressure controller and a cycle aging platform module, and the cycle aging platform module includes a vacuum-tight spherical chamber 3, and t...

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 lithium battery aging test system capable of simulating high-altitude temperature, humidity and pressure, the test system comprises a data acquisition system, a temperature controller, a humidity controller, a pressure controller and a circulating aging platform module, the circulating aging platform module comprises a vacuum closed ball cabin, the vacuum sealed ball cabin comprises a circulating charging and discharging platform and a vacuum pump. The test system combines multi-scale coupling environments such as pressure, temperature, humidity and the like according to an actual high-altitude flight environment; a vacuum closed ball cabin is specially designed, a vacuum closed power strip is designed on the right side of the vacuum closed ball cabin to be connected to the outside, so that data acquisition and a rapid interface of a cyclic aging experiment of a battery are carried out, connection is convenient, a closed experiment ball cabin is adopted, insulation treatment is carried out on the closed experiment ball cabin, accuracy and reliability are achieved, and a multi-scale cyclic aging experiment of the battery in a complex environment can be borne; the data acquisition system acquires data accurately and timely without delay.

Description

technical field [0001] The invention relates to the technical field of lithium battery aging testing, in particular to a lithium battery aging testing system capable of simulating high-altitude temperature, humidity and pressure. Background technique [0002] With the continuous depletion of underground energy and the increasingly serious damage to the environment by the products of thermal reactions of existing energy sources, it is extremely urgent for human beings to develop a green, environmentally friendly and high-energy new energy source. Because lithium-ion batteries have the characteristics of long cycle life, high voltage, low memory effect, and high specific energy, they were commercialized once they were developed, and are now widely used in mobile artificial intelligence devices, hybrid and all-electric vehicles, and It has gradually penetrated into the aerospace field, such as: electric aircraft (Ruixiang RXIE) and civil aviation aircraft (such as Airbus A350 a...

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
IPC IPC(8): G01R31/374G01R31/385G01R31/387H04N7/18
CPCG01R31/374G01R31/385G01R31/387H04N7/18
Inventor 孙强刘杭鑫赵晨曦林晏陈现涛
Owner CIVIL AVIATION FLIGHT UNIV OF CHINA