CN213278308U - Airplane buckle for fixing JAE connector - Google Patents
Airplane buckle for fixing JAE connector Download PDFInfo
- Publication number
- CN213278308U CN213278308U CN202021977657.0U CN202021977657U CN213278308U CN 213278308 U CN213278308 U CN 213278308U CN 202021977657 U CN202021977657 U CN 202021977657U CN 213278308 U CN213278308 U CN 213278308U
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- China
- Prior art keywords
- inserted bar
- jae
- connecting piece
- airplane
- elastic plug
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
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- Insertion Pins And Rivets (AREA)
Abstract
The utility model discloses an aircraft for fixing JAE connector is buckled, including elastic plug, separation blade and connecting piece, elastic plug is that the inserted bar bottom is connected in the middle of the V type inserted bar, and the cavity constitutes extrusion die cavity between inserted bar inner wall and the inserted bar, and the separation blade is connected on the inserted bar top, and the connecting piece is located the separation blade another side, is equipped with the draw-in groove with JAE connector joint on the connecting piece. Only a round hole is formed in the fixing plate, the elastic plug connector is clamped and pressed in the round hole, and the JAE connector is clamped on the connecting piece. The utility model discloses supplementary fixed JAE connector in assembling lithium ion battery, only need open a round hole on the fixed plate can, convenient operation is swift, and JAE connector also can be dismantled simultaneously.
Description
Technical Field
The utility model relates to a lithium ion battery assembly field, more specifically say, it relates to an aircraft knot for fixing JAE connector.
Background
The lithium ion battery comprises a battery cell and a protection circuit board, wherein the battery cell level is led out and connected with the protection circuit board through a terminal and a collection line, and a JAE connector is a connector from the collection line to the circuit board. The JAE connector does not hang during assembly, otherwise the JAE connector is easy to fall off by bumping and vibration during vehicle running at a later period. The convenience and rapidness of the fixation of the JAE connector is also part of improving the efficiency of battery assembly.
SUMMERY OF THE UTILITY MODEL
Not enough to prior art exists, the utility model aims to provide a solve the aircraft that is used for fixed JAE connector of above-mentioned problem and detain, supplementary JAE connector convenient and fast is fixed, and JAE connector also can conveniently be dismantled, improves battery packaging efficiency.
In order to achieve the above purpose, the utility model provides a following technical scheme:
a aircraft is detained for fixed JAE connector, including elastic plug, separation blade and connecting piece, the elastic plug is that the inserted bar bottom is connected in the middle of the V type inserted bar, and the cavity constitutes extrusion die cavity between inserted bar inner wall and the inserted bar, and the separation blade is connected on the inserted bar top, and the connecting piece is located the separation blade another side, is equipped with the draw-in groove with JAE connector joint on the connecting piece. Only a round hole is formed in the fixing plate, the elastic plug connector is clamped and pressed in the round hole, and the JAE connector is clamped on the connecting piece.
The utility model discloses further improve technical scheme and be, the bottom surface of the eye-splice is the arcwall face to the corner and the surface broad width that make progress. The inserting buckle is convenient to press into the round hole arranged on the fixing plate.
The utility model discloses further improve technical scheme and be, the inboard backplate that extends in both sides arm top of eye-splice, backplate and side arm top surface form L type step. The eye-splice card is gone into the fixed plate round hole, and the inner wall of round hole leans on the backplate, avoids direct contact inserted bar, prevents to grind off the inserted bar.
The utility model discloses further improve technical scheme be, the inserted bar is the long board of upper portion rectangle, lower part shape of falling trapezoidal. The slope surface of the inserted rod is easier to be inserted into the round hole of the fixed plate.
The utility model discloses further improve technical scheme and be, the separation blade is the both sides to the crooked arc of elastic plug. The arc-shaped plate has certain elasticity, and the card is tighter.
The utility model discloses further improve technical scheme and be, elastic plug, separation blade and connecting piece are a body structure. The integrated structure is more firm and durable.
The utility model discloses beneficial effect:
utilize the utility model discloses supplementary fixed JAE connector only need open on the fixed plate a round hole can, during the elastic plug pressed the insertion round hole, the draw-in groove and the JAE connector joint of another connecting piece, convenient operation is swift, and JAE connector also can be dismantled simultaneously.
Drawings
Fig. 1 is a perspective view of the present invention;
fig. 2 is a sectional view of the present invention.
Detailed Description
As shown in fig. 1 and fig. 2, the utility model discloses an elastic plug 1 of a body structure, separation blade 2 and connecting piece 3, elastic plug 1 comprises inserted bar 11 and V type eye-splice 12, inserted bar 11 is the upper portion rectangle, the long board of trapezoidal form is fallen to the lower part, 11 bottoms of inserted bar are connected in the middle of V type eye-splice 12, the cavity constitutes extrusion pressure die cavity 13 between 12 inner walls of eye-splice and the inserted bar 11, separation blade 2 is connected on 11 tops of inserted bar, separation blade 2 is the crooked arc of both sides to elastic plug, connecting piece 3 is located the 2 another sides of separation blade, be equipped with the draw-in groove 31 with JAE connector joint on the connecting piece 3.
For the convenience of insertion, the bottom surface of the insert buckle 12 is provided with an upward corner and the outer surface is provided with an arc-shaped surface 14.
The inner sides of the tops of the two side arms 15 of the inserting buckle 12 extend upwards to form a protective plate 16, and the protective plate 16 and the top surfaces of the side arms 15 form an L-shaped step.
It is above only the utility model discloses a preferred embodiment, the utility model discloses a scope of protection does not only confine above-mentioned embodiment, the all belongs to the utility model discloses a technical scheme under the thinking all belongs to the utility model discloses a scope of protection. It should be noted that, for those skilled in the art, various modifications and decorations can be made without departing from the principle of the present invention, and these modifications and decorations should also be regarded as the protection scope of the present invention.
Claims (6)
1. An aircraft buckle for fixing JAE connector, its characterized in that: including elastic plug (1), separation blade (2) and connecting piece (3), elastic plug (1) is that inserted bar (11) bottom is connected in the middle of V type eye-splice (12), and the cavity constitutes extrusion pressure die cavity (13) between eye-splice (12) inner wall and inserted bar (11), and separation blade (2) are connected on inserted bar (11) top, and connecting piece (3) are located separation blade (2) another side, are equipped with draw-in groove (31) with JAE connector joint on connecting piece (3).
2. An airplane clasp for securing a JAE connector according to claim 1, wherein: the upper corner and the outer surface width of the bottom surface of the insert buckle (12) are arc surfaces (14).
3. An airplane clasp for securing a JAE connector according to claim 1, wherein: the inner sides of the tops of the arms (15) on the two sides of the inserting buckle (12) extend upwards to form a protective plate (16), and the protective plate (16) and the top surfaces of the side arms (15) form an L-shaped step.
4. An airplane clasp for securing a JAE connector according to claim 1, wherein: the inserted bar (11) is a long plate with a rectangular upper part and an inverted trapezoidal lower part.
5. An airplane clasp for securing a JAE connector according to claim 1, wherein: the blocking piece (2) is an arc-shaped plate with two sides bent towards the elastic plug.
6. An airplane clasp for securing a JAE connector according to any one of claims 1 to 5, wherein: the elastic plug (1), the baffle (2) and the connecting piece (3) are of an integrated structure.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202021977657.0U CN213278308U (en) | 2020-09-11 | 2020-09-11 | Airplane buckle for fixing JAE connector |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202021977657.0U CN213278308U (en) | 2020-09-11 | 2020-09-11 | Airplane buckle for fixing JAE connector |
Publications (1)
Publication Number | Publication Date |
---|---|
CN213278308U true CN213278308U (en) | 2021-05-25 |
Family
ID=75940569
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202021977657.0U Active CN213278308U (en) | 2020-09-11 | 2020-09-11 | Airplane buckle for fixing JAE connector |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN213278308U (en) |
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2020
- 2020-09-11 CN CN202021977657.0U patent/CN213278308U/en active Active
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