CN209088117U - The Aviation Connector of the full glass sintering of eight cores - Google Patents
The Aviation Connector of the full glass sintering of eight cores Download PDFInfo
- Publication number
- CN209088117U CN209088117U CN201821796383.8U CN201821796383U CN209088117U CN 209088117 U CN209088117 U CN 209088117U CN 201821796383 U CN201821796383 U CN 201821796383U CN 209088117 U CN209088117 U CN 209088117U
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- China
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- connector
- external surface
- cylinder
- side external
- glass sintering
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Abstract
The utility model discloses the Aviation Connectors of the full glass sintering of eight cores, including main connector, one side external surface of the main connector is fixedly installed with No.1 screwed ring, the side of the main connector is provided with cylinder, the other side of the main connector is provided with annulus, one side external surface of the annulus is fixedly installed with rubber ring, one side external surface of middle part of the annulus is fixedly installed with No. two screwed rings, one side external surface of middle part of the cylinder is fixedly installed with rubber ring, the cylinder is internally provided with secondary connector, one side external surface of the pair connector is fixedly installed with round conductor, the main connector is internally provided with conductor.The Aviation Connector of the full glass sintering of eight cores described in the utility model is equipped with main connector, rubber ring and rubber ring, can enhance airtight effect, moreover it is possible to which banding conducting wire prevents it from surprisingly falling off, and can also improve ring network cabinet sealing effect, brings better prospect of the application.
Description
Technical field
The utility model relates to air-tightness field of connectors, the in particular to Aviation Connectors of the full glass sintering of eight cores.
Background technique
The Aviation Connector of the full glass sintering of eight cores is a kind of connector with gas seal property, is used for eight core ring network cabinets
With external electrical connection inside gas tank, there is good sealing effect；There is certain disadvantage when in use in existing connector
End, firstly, in use, air-tightness is poor, substantially there is showing for chronic leakage more than 0.1 atmospheric pressure
As, secondly, conducting wire is difficult to connect fastening, it is easy to fall off, in addition, air-tightness is lower at gap when being installed on ring network cabinet outer wall, tool
There have to be certain unfavorable, certain adverse effect is brought to the use process of people, for this purpose, it is proposed that the full glass sintering of eight cores
Aviation Connector.
Utility model content
The main purpose of the utility model is to provide the Aviation Connectors of the full glass sintering of eight cores, 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:
The Aviation Connector of the full glass sintering of eight cores, including main connector, the fixed peace of a side external surface of the main connector
Equipped with No.1 screwed ring, the side of the main connector is provided with cylinder, and the other side of the main connector is provided with annulus, institute
The side external surface for stating annulus is fixedly installed with rubber ring, and one side external surface of middle part of the annulus is fixedly installed with No. two screw threads
Ring, one side external surface of middle part of the cylinder are fixedly installed with rubber ring, and the cylinder is internally provided with secondary connector, described
One side external surface of secondary connector is fixedly installed with round conductor, and the main connector is internally provided with conductor, the conductor
A side external surface be fixedly connected with glass sintering, a side external surface of the glass sintering is fixedly connected with contact pin, the glass
The outer peripheral surface of glass sintering is fixedly installed with glass ring, and the side of the cylinder is provided with conducting wire.
There are eight groups of perforation on secondary connector construction, respectively correspond eight groups of contact pins, insertion type is installed to the one of main connector
End.
The inner ring diameter of rubber ring should be less than diameter of wire, when conducting wire passes through, rubber ring stress stretcher strain, can banding lead
Line prevents it from surprisingly falling off.
Preferably, one end outer surface of the conducting wire is through the middle part of rubber ring and one side external surface of middle part of round conductor
It is fixedly connected.
Preferably, one end outer surface of the contact pin is through a side external surface of glass sintering and one end outer surface of conductor
It is fixedly connected, the quantity of the contact pin is eight groups, and the quantity of the conductor is eight groups.
Preferably, No.1 seccotine is provided between the rubber ring and annulus, a side external surface of the rubber ring is logical
No.1 seccotine is crossed to be fixedly connected with a side external surface of annulus.
Preferably, No.1 screw thread is provided between the cylinder and No.1 screwed ring, one end inner surface of the cylinder is logical
It crosses No.1 screw thread to be flexibly connected with the outer surface of No.1 screwed ring, is provided with No. two between the main connector and No. two screwed rings
One end inner surface of screw thread, the main connector is flexibly connected by No. two screw threads with the outer surface of No. two screwed rings.
Preferably, No. two seccotines are provided between the rubber ring and cylinder, the outer surface of the rubber ring passes through two
It is fixedly connected in the middle part of number seccotine and cylinder.
Compared with prior art, the utility model has the following beneficial effects: the Aviation Connector of the full glass sintering of eight cores,
By the main connector of setting, glass sintering itself has through-hole structure at eight, and eight groups of contact pins, in contacting in through-hole, pass through with conductor
1000 degree of high-temperature vacuum sinter bondeds, by 1,000 degree of high-temperature vacuum sintering in conjunction with glass ring, glass ring passes through glass sintering
1000 degree of high-temperature vacuums are sintered to fix inside main connector, formed an air-tightness by force with the overall structure that is completely embedded, with
This makes air-tightness connector be able to bear the pressure of 6 atmospheric pressure or more, and by the rubber ring of setting, rubber ring is fixed on cylinder
Opening, when conducting wire passes through, can banding conducting wire, can effectively prevent from conducting wire connection not enough fastening is unexpected to fall off, rubber ring
Setting, when annulus is bonded ring network cabinet inner wall, No. two screwed rings pass through ring network cabinet preformed hole and the side of main connector connects, knob
When fastening, rubber ring stress deformation can block gap at ring network cabinet preformed hole, and leakproofness is stronger, be conducive to people and use, entirely
The Aviation Connector structure of the full glass sintering of eight cores is simple, easy to operate, and the effect used is more preferable relative to traditional approach.
Detailed description of the invention
Fig. 1 is the overall structure diagram of the Aviation Connector of the full glass sintering of eight core of the utility model.
Fig. 2 is the exploded view of Fig. 1 of the Aviation Connector of the full glass sintering of eight core of the utility model.
Fig. 3 is the structural schematic diagram of secondary connector 5 in Fig. 2 of the Aviation Connector of the full glass sintering of eight core of the utility model.
Fig. 4 is the structural schematic diagram of conductor 7 in Fig. 2 of the Aviation Connector of the full glass sintering of eight core of the utility model.
Fig. 5 is the structural schematic diagram of cylinder 2 in Fig. 2 of the Aviation Connector of the full glass sintering of eight core of the utility model.
In figure: 1, main connector；2, cylinder；3, annulus；4, conducting wire；5, secondary connector；6, No.1 screwed ring；7, conductor；
8, No. two screwed rings；9, rubber ring；10, round conductor；11, glass ring；12, contact pin；13, glass sintering；14, rubber ring.
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. 1-5, the Aviation Connector of the full glass sintering of eight cores, including main connector 1, outside the side of main connector 1
Surface is fixedly installed with No.1 screwed ring 6, and the side of main connector 1 is provided with cylinder 2, and the other side of main connector 1 is provided with
Annulus 3, a side external surface of annulus 3 are fixedly installed with rubber ring 9, and one side external surface of middle part of annulus 3 is fixedly installed with No. two
Screwed ring 8, one side external surface of middle part of cylinder 2 are fixedly installed with rubber ring 14, and cylinder 2 is internally provided with secondary connector 5, pair
One side external surface of connector 5 is fixedly installed with round conductor 10, and main connector 1 is internally provided with conductor 7, and the one of conductor 7
Side external surface is fixedly connected with glass sintering 13, and a side external surface of glass sintering 13 is fixedly connected with contact pin 12, glass sintering
13 outer peripheral surface is fixedly installed with glass ring 11, and the side of cylinder 2 is provided with conducting wire 4.
One end outer surface of conducting wire 4 is through the middle part of rubber ring 14 and the fixed company of one side external surface of middle part of round conductor 10
Connect, rubber ring 14 can banding conducting wire 4, prevent it from surprisingly falling off；The side of glass sintering 13 is run through in one end outer surface of contact pin 12
Outer surface is fixedly connected with one end outer surface of conductor 7, and the quantity of contact pin 12 is eight groups, and the quantity of conductor 7 is eight groups, contact pin 12
Across the side of glass sintering 13, conductor 7 passes through the other side of glass sintering 13, in the interior contact of glass sintering 13, passes through
After high-temperature vacuum sintering, the overall structure being completely embedded can be formed；No.1 seccotine, rubber are provided between rubber ring 9 and annulus 3
One side external surface of rubber ring 9 is fixedly connected by No.1 seccotine with a side external surface of annulus 3, and rubber ring 9 is made to be fixed on circle
The side of ring 3；No.1 screw thread is provided between cylinder 2 and No.1 screwed ring 6, one end inner surface of cylinder 2 passes through No.1 screw thread
It is flexibly connected with the outer surface of No.1 screwed ring 6, No. two screw threads, main connection is provided between main connector 1 and No. two screwed rings 8
One end inner surface of device 1 is flexibly connected by No. two screw threads with the outer surface of No. two screwed rings 8, easy disassembly；Rubber ring 14 with
No. two seccotines are provided between cylinder 2, the outer surface of rubber ring 14 connects by the way that the middle part of No. two seccotines and cylinder 2 is fixed
It connects, rubber ring 14 is made to be fixed on the middle part of cylinder 2.
It should be noted that the utility model is the Aviation Connector of the full glass sintering of eight cores, in use, our first knobs are twisted
No. two screwed rings 8 of 3 side of annulus are passed through the preformed hole of ring network cabinet inner wall by lower annulus 3, then by No. two screwed rings 8 and main company
One end knob connection fastening for connecing device 1, can be such that overall structure is fixed in ring network cabinet, wherein a side surface of annulus 3 is equipped with
Rubber ring 9, when connection fastens, 9 stress deformation of rubber ring can block the gap at preformed hole, inside ring network cabinet, by route
It is separately connected with eight groups of conductors 7, secondary connector 5 and cylinder 2 are two groups of structures, by eight groups of perforation alignment pins of secondary connector 5
12 are inserted in, and 14 middle part of rubber ring that conducting wire 4 passes through 2 side of cylinder is connect with round conductor 10, and knob cylinder 2 is connected to main connection
One end of device 1 can limit the scope of activities of secondary connector 5, separate it can not with contact pin 12 after knob fastening, more practical.
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. the Aviation Connector of the full glass sintering of eight cores, including main connector (1), it is characterised in that: the one of the main connector (1)
Side external surface is fixedly installed with No.1 screwed ring (6), and the side of the main connector (1) is provided with cylinder (2), the main connection
The other side of device (1) is provided with annulus (3), and a side external surface of the annulus (3) is fixedly installed with rubber ring (9), the circle
One side external surface of middle part of ring (3) is fixedly installed with No. two screwed rings (8), and one side external surface of middle part of the cylinder (2) is fixed
It is equipped with rubber ring (14), the cylinder (2) is internally provided with secondary connector (5), the side appearance of the pair connector (5)
Face is fixedly installed with round conductor (10), and the main connector (1) is internally provided with conductor (7), the side of the conductor (7)
Outer surface is fixedly connected with glass sintering (13), and a side external surface of the glass sintering (13) is fixedly connected with contact pin (12),
The outer peripheral surface of the glass sintering (13) is fixedly installed with glass ring (11), and the side of the cylinder (2) is provided with conducting wire
(4)。
2. the Aviation Connector of the full glass sintering of eight cores according to claim 1, it is characterised in that: the one of the conducting wire (4)
End outer surface is fixedly connected through the middle part of rubber ring (14) with one side external surface of middle part of round conductor (10).
3. the Aviation Connector of the full glass sintering of eight cores according to claim 1, it is characterised in that: the one of the contact pin (12)
A side external surface of the end outer surface through glass sintering (13) is fixedly connected with one end outer surface of conductor (7), the contact pin
(12) quantity is eight groups, and the quantity of the conductor (7) is eight groups.
4. the Aviation Connector of the full glass sintering of eight cores according to claim 1, it is characterised in that: the rubber ring (9) with
No.1 seccotine is provided between annulus (3), a side external surface of the rubber ring (9) passes through No.1 seccotine and annulus (3)
A side external surface be fixedly connected.
5. the Aviation Connector of the full glass sintering of eight cores according to claim 1, it is characterised in that: the cylinder (2) and one
No.1 screw thread is provided between number screwed ring (6), one end inner surface of the cylinder (2) passes through No.1 screw thread and No.1 screwed ring
(6) outer surface is flexibly connected, and No. two screw threads, the main company are provided between the main connector (1) and No. two screwed rings (8)
One end inner surface for connecing device (1) is flexibly connected by No. two screw threads with the outer surface of No. two screwed rings (8).
6. the Aviation Connector of the full glass sintering of eight cores according to claim 1, it is characterised in that: the rubber ring (14) with
No. two seccotines are provided between cylinder (2), the outer surface of the rubber ring (14) passes through in No. two seccotines and cylinder (2)
Portion is fixedly connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821796383.8U CN209088117U (en) | 2018-11-02 | 2018-11-02 | The Aviation Connector of the full glass sintering of eight cores |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821796383.8U CN209088117U (en) | 2018-11-02 | 2018-11-02 | The Aviation Connector of the full glass sintering of eight cores |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209088117U true CN209088117U (en) | 2019-07-09 |
Family
ID=67122111
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821796383.8U Active CN209088117U (en) | 2018-11-02 | 2018-11-02 | The Aviation Connector of the full glass sintering of eight cores |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209088117U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109473806A (en) * | 2018-11-02 | 2019-03-15 | 南京纬度电力科技有限公司 | The Aviation Connector of the full glass sintering of eight cores |
-
2018
- 2018-11-02 CN CN201821796383.8U patent/CN209088117U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109473806A (en) * | 2018-11-02 | 2019-03-15 | 南京纬度电力科技有限公司 | The Aviation Connector of the full glass sintering of eight cores |
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