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Based on high power battery activation system

A technology for activating the system and high power, applied in primary batteries, primary battery use/maintenance, circuits, etc., can solve the problems of increasing resource allocation, launch time, etc., to save the number of sequences, shorten launch time, and reduce activation power supply current Effect

Active Publication Date: 2022-05-24
BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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  • Abstract
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AI Technical Summary

Problems solved by technology

The current time-sharing activation battery sequence increases the control combination sequence circuit, increases resource allocation and launch time

Method used

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  • Based on high power battery activation system

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Embodiment Construction

[0027] The present invention is further elaborated below in conjunction with an embodiment.

[0028] The present invention provides that when the power of the battery is relatively large, the method of matching a small battery may be employed, by sending a small battery activation timing, thereby achieving the purpose of activating a high-power battery. It can save the number of timing of the control system, reduce the activation supply current, and at the same time be safe and reliable.

[0029] High-power battery-based activation systems, such as Figure 1As shown, specifically, comprising a first motor pump battery, a second motor pump battery, a first small battery, a control system, a third motor pump battery, a fourth motor pump battery and a second small battery; wherein the control system is set in the equipment cabin of the aircraft; the first motor pump battery, the second motor pump battery and the first small battery are set in the front cabin of the aircraft; the third...

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Abstract

The invention relates to an activation system based on a high-power battery, which belongs to the technical field of battery design on bullets; including a first motor pump battery, a second motor pump battery, a first small battery, a control system, a third motor pump battery, and a fourth motor pump battery and the second small battery; wherein, the control system is arranged in the equipment cabin of the aircraft; the first motor pump battery, the second motor pump battery and the first small battery are arranged in the front cabin of the aircraft; the third motor pump battery, the fourth The motor pump battery and the second small battery are arranged in the accessory compartment of the aircraft; wherein, the first small battery is provided with a first pyrotechnic device; the second small battery is provided with a second pyrotechnic device; when the power of the battery is relatively large At this time, the present invention adopts the method of matching a small battery, by sending the activation sequence of the small battery, so as to achieve the purpose of activating the high-power battery. The sequence number of the control system can be saved, the activation power supply current can be reduced, and it is also safe and reliable.

Description

Technical field [0001] The present invention belongs to the field of up-battery design technology, relates to a high-power battery activation system based on. Background [0002] The current on-board control system. Mainly through the combination of bullet control to the small battery to issue activation timing, through the small battery pressure to the motor pump high-power battery activation, and output the control system required power supply for cruise engine flight use. For high-power batteries, the usual practice is to activate the time-sharing by the control combination, powered by the ground power supply, and activate a battery multiple times as needed, which invisibly increases the high-current timing circuit of the control combination and increases the resource configuration. The current time-sharing activates battery timing, increases the control combination timing circuit, and increases the resource allocation and emission time. Contents of the Invention [0003] The...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F42B15/01H01M6/50
CPCF42B15/01H01M6/5088
Inventor 赵茜李海刘江李昕张英兰春云杨哲森
Owner BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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