CN207234006U - A kind of integral type aviation head based on lithium battery charger - Google Patents
A kind of integral type aviation head based on lithium battery charger Download PDFInfo
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- CN207234006U CN207234006U CN201720990454.7U CN201720990454U CN207234006U CN 207234006 U CN207234006 U CN 207234006U CN 201720990454 U CN201720990454 U CN 201720990454U CN 207234006 U CN207234006 U CN 207234006U
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- lithium battery
- battery charger
- pedestal
- aviation head
- electrode copper
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Abstract
The utility model discloses a kind of integral type aviation head based on lithium battery charger, including pedestal and back-end device, it is axially in parallel on the pedestal that two electrode copper pipes are installed, one end of two electrode copper pipes is arranged on the inner side of pedestal, the other end of two electrode copper pipes is arranged on the outside of internal plinth and welds together with two output leads of lithium battery charger, and the beneficial effects of the utility model are：1st, electrode copper pipe is connected and is reliably fixed together by this aviation head using integral structure with conducting wire, this entity mounting structure ensure that the good contact performance of electrode copper pipe and conducting wire, occur caused by will not causing plug the problem of loose contact, improve the performance of product.2nd, this aviation head is produced by the way of integral molded plastic through row, improves the automation level and productivity of production, improves the quality of production of product, and insulating properties is strong, it is of low cost the features such as.
Description
Technical field
The utility model is related to a kind of lithium battery charger technical field, be specifically it is a kind of based on lithium battery charger one
Body formula aviation head.
Background technology
Lithium battery charger is the equipment of electric bicycle indispensability.Lithium battery charger can be connect using a variety of output lines
Head, wherein aviation head are the common connectors of one of which.The aviation head front and back end split structure of existing lithium battery charger,
It is installed between electrode needle and conducting wire using welding manner between the inner cavity of front and back end, there are following some problems for it：1st, due to
Aviation head, which often plugs, can cause solder joint loose contact, cause aviation head to damage, it is impossible to normal use；2nd, the housing of aviation head is adopted
It is made, is assembled by 6 components, its cost is higher of zinc alloy material；3rd, it is complete by manual mode using split structure
Produced into installation, its low production efficiency and quality of production is difficult to ensure that.
Utility model content
The technical problem to be solved by the present invention is to provide a kind of integral type aviation head based on lithium battery charger, with
Solve the problems, such as to mention in background technology.
To achieve the above object, the utility model provides following technical solution：
A kind of integral type aviation head based on lithium battery charger, including pedestal and back-end device, it is axial on the pedestal
Parallel to be provided with two electrode copper pipes, one end of two electrode copper pipes is arranged on the inner side of pedestal, two electrode copper pipes it is another
End is arranged on the outside of internal plinth and welds together with two output leads of lithium battery charger, and back-end device is using note
Modeling mode is closely fixed together and by conducting wire cladding in back-end device with pedestal.
Further scheme as the utility model：The positioning parallel with two electrode copper pipes is additionally provided with the pedestal
Hole, one end of the location hole are arranged on the inside of pedestal.
Further scheme as the utility model：The pedestal is circular female seat.
Further scheme as the utility model：The base unit is made of bakelite material.
Further scheme as the utility model：The back-end device is molded for PVC material.
Compared with prior art, the beneficial effects of the utility model are：1st, this aviation head uses integral structure by electrode
Copper pipe is connected with conducting wire to be reliably fixed together, and this entity mounting structure ensure that the good contact of electrode copper pipe and conducting wire
Performance, occurs the problem of loose contact caused by will not causing plug, improves the performance of product.2nd, this aviation head is using overall
The mode of injection is produced through row, improves the automation level and productivity of production, improves the quality of production of product, and absolutely
Edge is strong, it is of low cost the features such as.
Brief description of the drawings
Fig. 1 is the structure diagram of the utility model.
Fig. 2 is the top view of the utility model.
In figure：1- pedestals, 2- back-end devices, 3, two electrode copper pipes of 4-, 5- positioning copper pipe, 6- output leads, 7- conducting wires
Protective case.
Embodiment
The following is a combination of the drawings in the embodiments of the present utility model, and the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are without making creative work
All other embodiments obtained, shall fall within the protection scope of the present invention.
Please refer to Fig.1-2, a kind of integral type aviation head based on lithium battery charger, as shown in Figure 1, including pedestal 1, after
End device 2, pedestal circular female seat made of bakelite material are axially in parallel on pedestal to be provided with two electrode copper pipes 3,4 and
One end of a piece positioning copper pipe 5, two electrode copper pipes and positioning copper pipe, which is arranged on the inside of pedestal, is used to connecting external equipment, two
The other end of electrode copper pipe is arranged on the inner side of internal plinth and is welded on one with two output leads 6 of lithium battery charger
Rise；Back-end device is tightly secured together for PVC material and using Shooting Technique with pedestal, while conducting wire is also covered by rear end
In device, set Wire sheath 7 to protect its inner lead in the outlet of rear end equipment and be connected with lithium battery charger.
Two conducting wires are welded on two electrode copper pipes of pedestal, then by this integral type aviation head first in production
It is placed on dedicated mould and uses PVC material single injection-molded, pedestal and the conducting wire of back-end device and inside is formed one
Structure.
Claims (5)
1. a kind of integral type aviation head based on lithium battery charger, including pedestal and back-end device, it is characterised in that the base
Axially in parallel on seat to be provided with two electrode copper pipes, one end of two electrode copper pipes is arranged on the inner side of pedestal, two electrode coppers
The other end of pipe is arranged on the outside of internal plinth and welds together with two output leads of lithium battery charger, rear end dress
Put and be closely fixed together and by conducting wire cladding in back-end device with pedestal using injection molding manner.
2. a kind of integral type aviation head based on lithium battery charger according to claim 1, it is characterised in that described
The location hole parallel with two electrode copper pipes is additionally provided with pedestal, one end of the location hole is arranged on the inside of pedestal.
3. a kind of integral type aviation head based on lithium battery charger according to claim 1, it is characterised in that described
Pedestal is circular female seat.
4. a kind of integral type aviation head based on lithium battery charger according to claim 1, it is characterised in that described
Base unit is made of bakelite material.
5. a kind of integral type aviation head based on lithium battery charger according to claim 1, it is characterised in that described
Back-end device is molded for PVC material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720990454.7U CN207234006U (en) | 2017-08-09 | 2017-08-09 | A kind of integral type aviation head based on lithium battery charger |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720990454.7U CN207234006U (en) | 2017-08-09 | 2017-08-09 | A kind of integral type aviation head based on lithium battery charger |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207234006U true CN207234006U (en) | 2018-04-13 |
Family
ID=61855710
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720990454.7U Active CN207234006U (en) | 2017-08-09 | 2017-08-09 | A kind of integral type aviation head based on lithium battery charger |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207234006U (en) |
-
2017
- 2017-08-09 CN CN201720990454.7U patent/CN207234006U/en active Active
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