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Voltage-controlled current-limiting charging circuit for 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: 2016-03-16
SHANGHAI INST OF SPACE POWER SOURCES
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  • 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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  • Voltage-controlled current-limiting charging circuit for supercapacitor bank

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Embodiment Construction

[0013] The present invention will be further elaborated below in conjunction with the accompanying drawings and specific embodiments. These examples should be understood as only for illustrating the present invention but not for limiting the protection scope of the present invention. After reading the contents 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 voltage-controlled current-limiting charging circuit for a supercapacitor bank of the present invention is as follows figure 1 As shown, it consists of four module circuits: super-buck step-down power module, double-loop control module, charging current reference control module, and constant current and constant voltage control module.

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

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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 in particular relates to a control circuit for a voltage-controlled current-limiting charging circuit of a supercapacitor bank. Background technique [0002] Not adjusting the busbar is an important energy control mode for space vehicles. Its characteristic is that the output current of the solar cell array is directly charged to the battery, and the battery voltage is the busbar voltage. Always changing. [0003] As an auxiliary energy source, a supercapacitor is generally connected in parallel with the battery. The supercapacitor has the ability to output high power instantaneously. Therefore, when there is a large pulse load demand, the supercapacitor will provide most of the energy for the large pulse load. [0004] The importance of supercapacitors is different from that of batteries, and priority should be given to battery charging (battery supplies power to the aircraft p...

Claims

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Application Information

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Patent Type & Authority Applications(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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