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Fixing seat for aviation storage battery

A technology for aviation batteries and fixing bases, which is applied to battery pack parts, circuits, electrical components, etc., can solve the problems of insufficient firmness and strength of convex and concave structures, no double safety protection measures, and insufficient structural strength and reliability, and achieve large The effect of safety and reliability, simple structure and easy processing

Inactive Publication Date: 2016-06-01
CHINA ELECTRONIC TECH GRP CORP NO 18 RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, the fixing seat developed by domestic manufacturers relies on the front and rear sides of the battery box to be designed as a convex-concave structure, and then is installed and positioned by extrusion with screws or even pins. There are no double safety protection measures, and the structural strength and reliability are insufficient, such as loose pins. Then the box will be thrown out, and the firmness and strength of the convex-concave structure are not enough, and there are hidden dangers in terms of safety.

Method used

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  • Fixing seat for aviation storage battery
  • Fixing seat for aviation storage battery
  • Fixing seat for aviation storage battery

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0041] The mode of work and the manufacture method of this design invention:

[0042] Such as figure 2 As shown, in order to ensure high reliability and safety, this design invention adopts box flash and figure 1 The sliding way of the fixed seat is fitted and disassembled through the locking mechanism of the spring lock lever, which constitutes a double safety assembly relationship and is convenient for operation, use and maintenance.

[0043] Under the premise of ensuring the reliability and rationality of the structure, this design invention mainly adopts the overall milling process to remove the remaining material for the processing of the base of the part 1. On the premise of ensuring sufficient strength, the part 1 is designed as followsfigure 1 The structure shown is the multi-directional symmetrical and simple structural design of the layered and frame-cooperated slideway. Specifically, through the three-layer design, the bottom of the 8 mounting holes is designed wi...

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PUM

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Abstract

The invention discloses a fixing seat for an aviation storage battery. The fixing seat comprises a fixing seat body, a spring lock rod locking mechanism and a press plate mechanism, wherein the fixing seat body comprises a base, a slipway connected with a box body is arranged on the upper surface of the base, the spring lock rod locking mechanism comprises two lock rods, two springs, a handle and a bent plate, the lock rods are arranged at the two ends of the bent plate, the two springs are connected to the lock rods in a sleeving way, the two ends of the bent plate are fixedly connected with the two ends of the handle by fastening elements, a locking groove is arranged at the end part of each lock rod, the press plate mechanism comprises a strip-shaped press plate, a locking tongue is arranged at each of the two ends of the strip-shaped press plate, the distance between the locking tongues is equal to the distance between the two locking grooves, a locking hole is formed in one end of the base, the two ends of the bent plate are fixedly connected with the end surface of the base by fastening elements, a fastening element is arranged at the middle of the strip-shaped press plate and fixedly connected with the base, the locking hole comprises two openings perpendicular to each other, the locking groove goes through one of the openings, and the locking tongue goes through the other opening.

Description

technical field [0001] The invention relates to the technical field of aviation storage batteries, in particular to a fixing seat for aviation storage batteries. Background technique [0002] The demand and market of aviation battery packs, which are necessary for national defense and civil aircraft, develop with the development of the national economy and the political needs of national defense, and have broad market prospects. [0003] The structure of the aviation battery pack used by the aircraft is different, and the structure of the corresponding fixing seat or mounting frame is also different. At present, the fixing seat developed by domestic manufacturers relies on the front and rear sides of the battery box to be designed as a convex-concave structure, and then is installed and positioned by extrusion with screws or even pins. There are no double safety protection measures, and the structural strength and reliability are insufficient, such as loose pins. Then the b...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01M2/10H01M50/244H01M50/249H01M50/264
CPCH01M50/256H01M50/20Y02E60/10
Inventor 郭琦苏晓倩
Owner CHINA ELECTRONIC TECH GRP CORP NO 18 RES INST
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