CN209088107U - Aviation Connector of the 26 core rectangles from short circuit - Google Patents
Aviation Connector of the 26 core rectangles from short circuit Download PDFInfo
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- CN209088107U CN209088107U CN201821796407.XU CN201821796407U CN209088107U CN 209088107 U CN209088107 U CN 209088107U CN 201821796407 U CN201821796407 U CN 201821796407U CN 209088107 U CN209088107 U CN 209088107U
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- connector
- fixedly installed
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- side external
- link
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Abstract
The utility model discloses the Aviation Connectors of oneself short circuit of 26 core rectangles, including main connector, the lower end of the main connector is provided with secondary connector, one side external surface of the pair connector is fixedly installed with No.1 side plate, another side external surface of the pair connector is fixedly installed with No. two side plates, one side external surface of upper center of No. two side plates is fixedly installed with current transformer, the upper end outer surface of No. two side plates is fixedly installed with jack module, the lower end outer surface of the main connector is fixedly installed with contact pin, the upper end outer surface of the contact pin is fixedly installed with leather sheath, iron plate is provided in the middle part of the contact pin.26 core rectangle described in the utility model is equipped with side plate, link block and iron plate, can facilitate installation from the Aviation Connector of short circuit, main connector can also be made to be directly connected to fasten with secondary connector, it can also realize from short circuit, prevent circuit secondary back from bringing unexpected harm, bring better prospect of the application.
Description
Technical field
The utility model relates to smart grid Communication Control field, in particular to Aviation Connector of the 26 core rectangles from short circuit.
Background technique
Connector is a kind of tool that can be connected inside enclosed construction with external structure, be can be realized inside enclosed construction
With the intercommunications such as external structure data, electric current, not only structure is simple for it, and easy to operate；Existing connector is deposited when in use
In certain drawbacks, firstly, secondary current circuit, which disconnects, can generate high pressure when connector disconnects, there is safety to operator
Hidden danger, while current transformer may be damaged, it is not easy to install when secondly, connector is inside enclosed construction, in addition, main company
It connects when device is connect with secondary connector and not enough fastens, easy accident falls off, and certain unfavorable shadow is brought to the use process of people
It is loud, for this purpose, it is proposed that the Aviation Connector of oneself short circuit of 26 core rectangles.
Utility model content
The main purpose of the utility model is to provide 26 core rectangles from the Aviation Connector of short circuit, can effectively solve background
The problems in technology.
To achieve the above object, the technical solution that the utility model is taken are as follows:
26 core rectangles are provided with secondary connection from short-circuit Aviation Connector, including main connector, the lower end of the main connector
Device, a side external surface of the pair connector are fixedly installed with No.1 side plate, and another side external surface of the pair connector is fixed
No. two side plates are installed, one side external surface of upper center of No. two side plates is fixedly installed with current transformer, and described No. two
The upper end outer surface of side plate is fixedly installed with jack module, and the lower end outer surface of the main connector is fixedly installed with contact pin, institute
The upper end outer surface for stating contact pin is fixedly installed with leather sheath, and iron plate, the iron plate and main connector are provided in the middle part of the contact pin
Between be fixedly connected with spring, one side external surface of front end of the main connector is fixedly installed with No.1 link block, the main company
Another side external surface in front end for connecing device is fixedly installed with No. two link blocks, the fixed peace of one side external surface of rear end of the main connector
Equipped with No. three link blocks, another side external surface in the rear end of the main connector is fixedly installed with No. four link blocks.
Leather sheath is plastic material, has insulation characterisitic, and positioned at one end of contact pin, iron plate is conductor, and main connector and pair are even
When connecing device connection, iron plate is pushed at leather sheath, and short-circuit condition stops, and when main connector and secondary connector disconnect, spring pushes iron
Piece is directly contacted with contact pin, makes 26 groups of contact pin circuit connections, forms short-circuit condition.
Preferably, No.1 fixed block, the side of the No.1 side plate are provided between the No.1 side plate and secondary connector
Outer surface is fixedly connected by No.1 fixed block with a side external surface of secondary connector, between No. two side plates and secondary connector
It is provided with No. two fixed blocks, the other side appearance that a side external surface of No. two side plates passes through No. two fixed blocks and secondary connector
Face is fixedly connected.
Preferably, the No.1 link block, No. two be provided with No. three fixed blocks between link block and main connector, described one
Number link block, No. two link blocks upper end outer surface pass through No. three fixed blocks and two side external surface of front end of main connector is fixed
Connection, No. three link blocks, No. four be provided with No. four fixed blocks between link block and main connector, No. three link blocks,
The upper end outer surface of No. four link blocks passes through No. four fixed blocks and is fixedly connected with the rear end sides outer surface of main connector.
Preferably, two side external surfaces of the iron plate pass through the fixed company of two side external surface of lower end of spring and main connector
It connects, the quantity of the spring is two groups.
Preferably, No.1 bolt, the No.1 are provided between the No.1 link block, No. two link blocks and secondary connector
Link block, No. two link blocks lower end outer surface pass through No.1 bolt and the two side external surface activity of front end of secondary connector connects
It connects, is provided with No. two bolts, No. three link blocks, No. four between No. three link blocks, No. four link blocks and secondary connector
The lower end outer surface of link block passes through No. two bolts and is flexibly connected with the rear end sides outer surface of secondary connector.
Preferably, the quantity of the jack module is 26 groups, and the quantity of the contact pin is 26 groups.
Compared with prior art, the utility model has the following beneficial effects: the 26 core rectangle from short circuit Aviation Connector,
, can be firm in being installed on horizontal plane or vertical plane by overall structure by two groups of side plates of setting, pass through the iron plate of setting, iron
Skin offers 26 groups of through-holes, corresponding with contact pin position, and when main connector is connect with secondary connector, spring stress is shunk, iron
Piece is pushed to contact pin upper end, contacts with leather sheath, and when main connector is separated with secondary connector, iron plate is pushed into insert by recoil of spring
Needle lower end, iron plate is directly contacted with contact pin at this time, and iron plate is conductor, is formed short circuit with 26 groups of contact pins, can be prevented connector
When disconnection, secondary current circuit, which disconnects, generates high pressure, causes contingency to operator, while may damage Current Mutual Inductance
Four groups of link blocks when main connector is connect with secondary connector, are connect by device, the setting of four groups of link blocks with pair respectively using bolt
Device is fixed, and main connector can be made to connect fastening with secondary connector, is conducive to people and is used, the aviation of entire 26 core rectangle from short circuit connects
Header structure is simple, easy to operate, and the effect used is more preferable relative to traditional approach.
Detailed description of the invention
Fig. 1 is overall structure diagram of the 26 core rectangle of the utility model from short-circuit Aviation Connector.
Fig. 2 is the structural schematic diagram of 26 core rectangle of the utility model secondary connector 2 from Fig. 1 of the Aviation Connector of short circuit.
Fig. 3 is structural schematic diagram of the 26 core rectangle of the utility model from main connector 1 in Fig. 1 of the Aviation Connector of short circuit.
Fig. 4 be 26 core rectangle of the utility model from short circuit Aviation Connector Fig. 3 bottom view.
In figure: 1, main connector；2, secondary connector；3, No.1 side plate；4, No. two side plates；5, current transformer；6, jack
Module；7, contact pin；8, leather sheath；9, No.1 link block；10, No. two link blocks；11, No. three link blocks；12, No. four link blocks；13,
Iron plate；14, spring.
Specific embodiment
To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below
In conjunction with specific embodiment, the utility model is further described.
As shown in Figs 1-4,26 core rectangles are set from short-circuit Aviation Connector, including main connector 1, the lower end of main connector 1
It is equipped with secondary connector 2, a side external surface of secondary connector 2 is fixedly installed with No.1 side plate 3, the other side appearance of secondary connector 2
Face is fixedly installed with No. two side plates 4, and one side external surface of upper center of No. two side plates 4 is fixedly installed with current transformer 5, and No. two
The upper end outer surface of side plate 4 is fixedly installed with jack module 6, and the lower end outer surface of main connector 1 is fixedly installed with contact pin 7, inserts
The upper end outer surface of needle 7 is fixedly installed with leather sheath 8, and the middle part of contact pin 7 is provided with iron plate 13, between iron plate 13 and main connector 1
It is fixedly connected with spring 14, one side external surface of front end of main connector 1 is fixedly installed with No.1 link block 9, before main connector 1
Another side external surface is held to be fixedly installed with No. two link blocks 10, one side external surface of rear end of main connector 1 is fixedly installed with No. three
Link block 11, another side external surface in the rear end of main connector 1 are fixedly installed with No. four link blocks 12.
No.1 fixed block is provided between No.1 side plate 3 and secondary connector 2, a side external surface of No.1 side plate 3 passes through one
Number fixed block is fixedly connected with a side external surface of secondary connector 2, be provided between No. two side plates 4 and secondary connector 2 No. two it is solid
Determine block, a side external surface of No. two side plates 4 is fixedly connected with another side external surface of secondary connector 2 by No. two fixed blocks, is led to
It crosses No.1 side plate 3 and No. two side plates 4 can facilitate will be integrally fastened to horizontal plane or vertical plane；9, No. two link blocks of No.1 link block
No. three fixed blocks are provided between 10 and main connector 1, the upper end outer surface of 9, No. two link blocks 10 of No.1 link block passes through
No. three fixed blocks are fixedly connected with two side external surface of front end of main connector 1,11, No. four link blocks 12 of No. three link blocks and main company
It connects and is provided with No. four fixed blocks between device 1, the upper end outer surface of 11, No. four link blocks 12 of No. three link blocks passes through No. four fixations
Block is fixedly connected with the rear end sides outer surface of main connector 1；Two side external surfaces of iron plate 13 pass through spring 14 and main connection
Two side external surface of lower end of device 1 is fixedly connected, and the quantity of spring 14 is two groups, influence iron plate 13 can by spring 14 and movable；
No.1 bolt, 9, No. two link blocks of No.1 link block are provided between 9, No. two link blocks 10 of No.1 link block and secondary connector 2
10 lower end outer surface passes through No.1 bolt and is flexibly connected with two side external surface of front end of secondary connector 2, No. three link blocks 11,
No. two bolts, the lower end appearance of 11, No. four link blocks 12 of No. three link blocks are provided between No. four link blocks 12 and secondary connector 2
Face passes through No. two bolts and is flexibly connected with the rear end sides outer surface of secondary connector 2, can make main connector 1 and secondary connector 2
Stable connection；The quantity of jack module 6 is 26 groups, and the quantity of contact pin 7 is 26 groups.
It should be noted that the utility model is Aviation Connector of the 26 core rectangles from short circuit, using making, by main connector 1
It is placed in the top of secondary connector 2, the position insertion of 7 alignment receptacles module of contact pin, 6 aperture can be completed connection, use later
Bolt is tight by secondary connector 2 and 11, No. four 12 knobs of link block of link block of link block 10, three of No.1 link block 9, two respectively
Gu, it is ensured that it connects and fastens between main connector 1 and secondary connector 2, can prevent main connector 1 from surprisingly falling off with secondary connector 2,
The two sides of secondary connector 2 are separately installed with No.1 side plate 3 and No. two side plates 4, pass through No.1 side plate 3 and No. two side plates using screw
It at 4 perforation, fastens, overall structure can be pacified in horizontal plane or vertical plane then at knob at the preformed hole of vertical plane or horizontal plane
Dress is firm, and when main connector 1 is connect with secondary connector 2, iron plate 13 is pushed to the upper end of leather sheath 8, main connector 1 and secondary connector
When 2 disconnection, spring 14 is sprung back, and pushes iron plate 13 to contact with contact pin 7,7 circuit intercommunication of contact pin 7 and 26 group contact pin, with this reality
It is more practical now from short circuit.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above.Current row
The technical staff of industry is described in above embodiments and description it should be appreciated that the present utility model is not limited to the above embodiments
Only illustrate the principles of the present invention, on the premise of not departing from the spirit and scope of the utility model, the utility model is also
It will have various changes and improvements, these various changes and improvements fall within the scope of the claimed invention.The utility model
Claimed range is defined by the appending claims and its equivalent thereof.
Claims (6)
1.26 core rectangles short-circuit Aviation Connector, including main connector (1) certainly, it is characterised in that: under the main connector (1)
End is provided with secondary connector (2), and a side external surface of the pair connector (2) is fixedly installed with No.1 side plate (3), and the pair is even
Another side external surface for connecing device (2) is fixedly installed with No. two side plates (4), the upper center side appearance of No. two side plates (4)
Face is fixedly installed with current transformer (5), and the upper end outer surface of No. two side plates (4) is fixedly installed with jack module (6), institute
The lower end outer surface for stating main connector (1) is fixedly installed with contact pin (7), and the upper end outer surface of the contact pin (7) is fixedly installed with
Leather sheath (8) is provided with iron plate (13) in the middle part of the contact pin (7), is fixedly connected between the iron plate (13) and main connector (1)
Have spring (14), one side external surface of front end of the main connector (1) is fixedly installed with No.1 link block (9), the main connection
Another side external surface in front end of device (1) is fixedly installed with No. two link blocks (10), the rear end side appearance of the main connector (1)
Face is fixedly installed with No. three link blocks (11), and another side external surface in rear end of the main connector (1) is fixedly installed with No. four companies
Connect block (12).
2. the Aviation Connector of oneself short circuit of 26 core rectangle according to claim 1, it is characterised in that: the No.1 side plate (3)
Be provided with No.1 fixed block between secondary connector (2), a side external surface of the No.1 side plate (3) by No.1 fixed block with
One side external surface of secondary connector (2) is fixedly connected, and No. two are provided between No. two side plates (4) and secondary connector (2) admittedly
Determine block, a side external surface of No. two side plates (4) is fixed by No. two fixed blocks and another side external surface of secondary connector (2)
Connection.
3. the Aviation Connector of oneself short circuit of 26 core rectangle according to claim 1, it is characterised in that: the No.1 link block
(9), No. three fixed blocks, the No.1 link block (9), No. two companies are provided between No. two link blocks (10) and main connector (1)
The upper end outer surface for connecing block (10) passes through No. three fixed blocks and is fixedly connected with two side external surface of front end of main connector (1), institute
It states and is provided with No. four fixed blocks between No. three link blocks (11), No. four link blocks (12) and main connector (1), No. three connections
Block (11), No. four link blocks (12) upper end outer surface pass through the rear end sides appearance of No. four fixed blocks Yu main connector (1)
Face is fixedly connected.
4. the Aviation Connector of oneself short circuit of 26 core rectangle according to claim 1, it is characterised in that: the two of the iron plate (13)
Side external surface passes through spring (14) and is fixedly connected with two side external surface of lower end of main connector (1), the number of the spring (14)
Amount is two groups.
5. the Aviation Connector of oneself short circuit of 26 core rectangle according to claim 1, it is characterised in that: the No.1 link block
(9), No.1 bolt, the No.1 link block (9), No. two connections are provided between No. two link blocks (10) and secondary connector (2)
The lower end outer surface of block (10) passes through No.1 bolt and is flexibly connected with two side external surface of front end of secondary connector (2), and described three
No. two bolts, No. three link blocks are provided between number link block (11), No. four link blocks (12) and secondary connector (2)
(11), the lower end outer surface of No. four link blocks (12) passes through No. two bolts and the rear end sides outer surface of secondary connector (2) is living
Dynamic connection.
6. the Aviation Connector of oneself short circuit of 26 core rectangle according to claim 1, it is characterised in that: the jack module (6)
Quantity be 26 groups, the quantity of the contact pin (7) is 26 groups.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821796407.XU CN209088107U (en) | 2018-11-02 | 2018-11-02 | Aviation Connector of the 26 core rectangles from short circuit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821796407.XU CN209088107U (en) | 2018-11-02 | 2018-11-02 | Aviation Connector of the 26 core rectangles from short circuit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209088107U true CN209088107U (en) | 2019-07-09 |
Family
ID=67122163
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821796407.XU Active CN209088107U (en) | 2018-11-02 | 2018-11-02 | Aviation Connector of the 26 core rectangles from short circuit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209088107U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109510010A (en) * | 2018-11-02 | 2019-03-22 | 南京纬度电力科技有限公司 | Aviation Connector of the 26 core rectangles from short circuit |
-
2018
- 2018-11-02 CN CN201821796407.XU patent/CN209088107U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109510010A (en) * | 2018-11-02 | 2019-03-22 | 南京纬度电力科技有限公司 | Aviation Connector of the 26 core rectangles from short circuit |
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