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A voltage-controlled current-limiting charging circuit for a supercapacitor bank

A supercapacitor and current-limiting charging technology, which is applied to battery circuit devices, current collectors, circuit devices, etc., can solve the problems of different degrees of importance and limited light period in low rails, etc.

Active Publication Date: 2018-09-18
SHANGHAI INST OF SPACE POWER SOURCES
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The importance of supercapacitors and batteries is different, and battery charging should be given priority (batteries supply power to the aircraft platform). However, due to the limited light period of low-orbit light, it is impossible to wait for the battery to be fully charged before charging the supercapacitor. Therefore, how to solve the problem of supercapacitor charging becomes a problem. Technical Difficulties

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  • A voltage-controlled current-limiting charging circuit for a supercapacitor bank
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  • A voltage-controlled current-limiting charging circuit for a supercapacitor bank

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Embodiment Construction

[0013] The present invention will be further explained below in conjunction with the drawings and specific embodiments. These embodiments should be understood as only used to illustrate the present invention and not to limit the protection scope of the present invention. After reading the content of the present invention, those skilled in the art can make various changes or modifications to the present invention, and these equivalent changes and modifications also fall within the scope defined by the claims of the present invention.

[0014] The electrical principle block diagram of a super capacitor bank voltage-controlled current-limiting charging circuit of the present invention is as follows figure 1 As shown, it is composed of four module circuits: a super-buck step-down power module, a dual-loop control module, a charging current reference control module, and a constant current and constant voltage control module.

[0015] figure 2 It is the super-buck step-down power module...

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Abstract

The invention belongs to a charging control circuit for a supercapacitor based on a non-adjusting-busbar mode of a spacecraft. The circuit can increase the charging current for the supercapacitor with the rise of the busbar voltage; when a constant voltage point of the supercapacitor is achieved, a constant voltage control state is performed. The charging control circuit comprises a super-buck voltage-reduction power module, an electric current loop-voltage loop dual-loop control module, a charging current reference follow-up busbar voltage control module, and a supercapacitor constant-current constant-voltage control module. According to the charging control circuit, the supercapacitor, serving as a backup power, satisfies the power requirement of the busbar preferably; with the increase of excessive energy, the busbar voltage rises gradually, and the charging current is increased gradually; and the charging control circuit is simple in control structure, less in required devices and simple in interface.

Description

Technical field [0001] The invention belongs to the technical field of space power supplies, and specifically relates to a control circuit of a super capacitor bank voltage-controlled current-limiting charging circuit. Background technique [0002] Unregulated bus is an important energy control mode of spacecraft. Its characteristic is to directly charge the battery with the output current of the solar array. The battery voltage is the bus voltage. As the battery voltage changes continuously with the charging and discharging process, when the bus voltage is not adjusted Always changing. [0003] As an auxiliary energy source, the super capacitor is generally connected in parallel with the battery. The super capacitor has the ability to instantly output high power. Therefore, when there is a large pulse load demand, the super capacitor will provide most of the energy for the large pulse load. [0004] Supercapacitors and batteries are of different importance. Priority should be given...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H02J7/00
CPCH02J7/0029H02J7/00304H02J7/345
Inventor 杨华韦云徐军焦宇晟覃思明
Owner SHANGHAI INST OF SPACE POWER SOURCES
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