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Storage battery pack open-circuit failure prevention assembly for spacecraft and control method

A battery pack and battery technology, applied in battery circuit devices, circuits, electrical components, etc., can solve problems such as inapplicability to spacecraft and lack of battery pack application capabilities, achieve simple interfaces, and increase on-orbit applications and service life. , the effect of simple assembly

Pending Publication Date: 2021-03-16
SHANGHAI SATELLITE ENG INST
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  • Description
  • Claims
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Problems solved by technology

[0004] Patent document ZL201610061144.7 discloses an open-circuit monitoring device for battery packs. This patent is mainly aimed at the detection of open-circuit conditions in battery packs used on the ground. On the one hand, it is not suitable for spacecraft and does not have the ability to continue to maintain the use of battery packs; retrieved Application No. CN200720079704.8 for "Single Cell Open Circuit Protection Device for Battery Pack", this patent introduces the open circuit protection device for battery cell of electric locomotive battery pack, which is not suitable for spacecraft

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  • Storage battery pack open-circuit failure prevention assembly for spacecraft and control method

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Embodiment Construction

[0032] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0033] Such as figure 1 According to the present invention, an open-circuit failure prevention assembly for a battery pack for a spacecraft includes: a bidirectional charging and discharging module, an information collection / control module, a data processing / communication module, a power supply module, and a battery pack; the bidirectional charging and discharging module and information The collection / control module is connected; the information collection / control module is connected to the data process...

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Abstract

The invention provides a storage battery pack open-circuit failure prevention assembly for a spacecraft and a control method. The storage battery pack open-circuit failure prevention assembly comprises a bidirectional charging and discharging module, an information acquisition / control module, a data processing / communication module, a power supply module and a storage battery pack, the bidirectional charging and discharging module is connected with the information acquisition / control module; the information acquisition / control module is connected with the data processing / communication module; the power supply module is connected with the bidirectional charging and discharging module, the information acquisition / control module and the data processing / communication module. And the storage battery pack is connected with the bidirectional charging and discharging module and the information acquisition / control module. The storage battery pack open-circuit failure prevention assembly for thespacecraft is simple in interface and relatively independent, charging and discharging of the storage battery pack are not affected when the storage battery pack is normal, and use of a storage battery pack charging and discharging control circuit is not affected when open-circuit faults happen to the single storage battery pack.

Description

technical field [0001] The invention relates to the technical field of battery pack open-circuit failure prevention, in particular to an open-circuit failure prevention component and control method for a battery pack used in spacecraft. Background technique [0002] At present, battery packs are used in each spacecraft as a primary power supply, and each spacecraft is equipped with one or more battery packs. Due to the long-term charge-discharge cycle, the seal fails, and a large amount of monomer electrolyte leaks to cause an open circuit; in addition, it may also be caused by The manufacturing process is not strictly controlled, and the internal welding of the battery is disconnected, resulting in an open circuit. The open circuit is the most serious failure mode of the battery. For the single-pack battery pack plan, the open circuit of the battery pack is a fatal danger. For two or more For the battery pack solution, if one group of batteries fails in open circuit, the di...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02J7/00H01M10/44H02H7/18
CPCH02J7/005H02J7/00036H02J7/0029H02J7/0014H01M10/441H02H7/18Y02E60/10
Inventor 黄小虎张朋松王益军洪平高宇翔邵陈懋王君磊袁双
Owner SHANGHAI SATELLITE ENG INST
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