CN103490213A - Novel aviation connector for distribution automation terminal - Google Patents
Novel aviation connector for distribution automation terminal Download PDFInfo
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- CN103490213A CN103490213A CN201310391823.7A CN201310391823A CN103490213A CN 103490213 A CN103490213 A CN 103490213A CN 201310391823 A CN201310391823 A CN 201310391823A CN 103490213 A CN103490213 A CN 103490213A
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- China
- Prior art keywords
- automation terminal
- aviation connector
- plug
- outer cover
- distribution power
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Abstract
The invention discloses a novel aviation connector for a distribution automation terminal. The aviation connector comprises a plug connection assembly and an outer cover assembly. The plug connection assembly comprises an aviation plug and an upper cover, and the aviation plug and the upper cover are fixedly connected. A socket which is matched with a distribution switch connecting base is formed in the upper end of the aviation plug, and a screw hole is formed in the lower end of the upper cover. The outer cover assembly comprises an outer cover which is fixedly connected with the plug connection assembly through the screw hole to form a closed container. By the adoption of the novel aviation connector, the distribution automation terminal can be matched with a high-voltage switch without cable connection and installation tools, therefore, reliability of a whole set of distribution equipment is effectively improved, and cost is reduced.
Description
Technical field
The present invention relates to the power distribution automation field, specifically refer to a kind of novel aviation connector that is applied to distribution power automation terminal.
Background technology
In 10kV power distribution automation field, distribution terminal and outdoor aerial high voltage switch are supporting while realizing the power distribution automation function, and distribution terminal and aerial high-voltage switch interface all are furnished with aviation socket usually, adopt some multicore insulated cables to connect between the two.There is following shortcoming in this kind of connected mode:
1, electric device project installation complexity;
2, stube cable and electric cable accessories processing cost are high;
3, stube cable is arranged between two complete equipments and expose throughout the year outdoor, at aspects such as rainproof, efflorescence prevention, insulation, the processing of cable finished product, require high, once the stube cable annex occurs extremely may causing great power outage.
Summary of the invention
In order to overcome above-mentioned deficiency of the prior art, the invention provides a kind of novel aviation connector that is applied to distribution power automation terminal, it can realize exempting from cable and be connected, exempts from erecting tools when distribution power automation terminal and high-voltage switch gear are supporting, effectively improve the reliability of complete set of distribution, Cost reduction.
The technical solution adopted for the present invention to solve the technical problems is:
A kind of novel aviation connector that is applied to distribution power automation terminal, described aviation connector comprises the plug coupling assembling, it comprises aviation plug and the upper cover be fixedly connected with, wherein said aviation plug upper end is provided with the socket supporting with the panel switches Connection Block, and described upper cover lower end is provided with screw; Cover member, it comprises outer cover, described outer cover is fixedly connected to form a closed container by screw and described plug coupling assembling.
As improvement of the technical scheme, described outer cover lower end is provided with screw thread, by it, is connected with an observation window, and described observation window is airtight window.
As improvement of the technical scheme, described aviation plug lower end is provided with the connecting hole be connected and fixed with upper cover, and described connecting hole and the screw that is arranged at described upper cover lower end all adopt blind hole structure.
As improvement of the technical scheme, between described plug coupling assembling, cover member and observation window, adopt the antiseepage ability of swimming to be tightly connected.
Further, described upper cover, outer cover lower end are provided with the sealing ring mounting groove.
Further, described outer cover upper end-face edge adopts hierarchic structure.
As improvement of the technical scheme, it is conical that described airtight window is, and described closed container is cylindrical.
The beneficial effect that the present invention brings has:
Novel aviation connector of the present invention is fixedly formed by dismountable plug coupling assembling, cover member, it not only can reduce the complexity of electric device project installation, erecting tools is exempted from realization, lifting to the controller switching equipment reliability is also particularly evident, because of its thorough liberation the annexes such as stube cable, realize exempting from cable and connect, make this connector improve to the adaptive capacity of environment, indirectly promote service life of equipment, reduced processing cost simultaneously, there is higher market popularization value.
The accompanying drawing explanation
Below in conjunction with drawings and the specific embodiments, the invention will be further described,
Accompanying drawing 1 is novel aviation connector cross-sectional view of the present invention;
Accompanying drawing 2 is A part partial enlarged drawings in accompanying drawing 1;
Accompanying drawing 3 is B part partial enlarged drawings in accompanying drawing 1.
Embodiment
The novel aviation connector that is applied to distribution power automation terminal of the present invention, it is fixedly formed by dismountable plug coupling assembling, cover member and observation window, using this aviation connector distribution terminal to be docked with any 10kV outdoor aerial high voltage switch when supporting, without annexes such as stube cables, therefore the present invention just do not have the drawbacks such as power distribution automation dysfunction that cause because of the stube cable fault, so can be widely used in the power monitoring field yet.
Concrete, by reference to the accompanying drawings 1 to 3, above-mentioned plug coupling assembling comprises aviation plug 1 and the upper cover 2 be fixedly connected with, wherein the upper end of aviation plug 1 is provided with the socket 11 supporting with the panel switches Connection Block, its lower end is provided with the connecting hole 12 be connected and fixed with upper cover 2, and upper cover 2 screw 21 set by its lower end is fixedly connected with cover member.Cover member mainly comprises outer cover 3 and other relevant connection assemblies, and outer cover 3, with after upper cover 2 is fixedly connected with, can form a cylindrical circular closed container 30, and it can be used to install the distribution power automation terminal core component.
Simultaneously, the lower end of outer cover 3 is provided with screw thread 31, and observation window is fixedly connected with it by this structure, and arranging mainly in order in the situation that covered of observation window, observe directly equipment inner structure, so it is the airtight window 4 that is conic transparent.
In addition, in order to make good looking appearance of the present invention, and keep sealing preferably, above-mentioned connecting hole 12 and screw 21 all adopt the blind hole structure design, in the lower end of upper cover 2 and outer cover 3, are provided with sealing ring mounting groove 5, by sealing ring is installed, can further to its sealing, carry out perfect, in order to make the present invention possess water resistance preferably, improve its adaptive capacity to environment, the upper end-face edge of above-mentioned outer cover 3 adopts hierarchic structure, can effectively prevent that rainwater from infiltrating.
Novel aviation connector of the present invention can be used as a kind of universal power monitoring end product structure, its main body adopts aluminum alloy corrosion resistant to process, the closed container 30 of nonmetal cylinder type adopts the fiber reinforcement type composite plastic, it is had corrosion-resistant, the characteristics such as ageing-resistant, conical observation window adopts the PC+ABS transparent material.Between each parts, closely connect, sealing can reach IP67, and is greater than 10 years useful life.
So novel aviation connector of the present invention, it not only can reduce the complexity of electric device project installation, erecting tools is exempted from realization, the controller switching equipment reliability is had to obvious lifting, simultaneously because of its thorough liberation the annexes such as stube cable, can realize exempting from cable and connect, make this connector to improving in adaptive capacity and the useful life of environment, reduce processing cost simultaneously.
Finally, the above is preferred embodiment of the present invention, and the present invention is not limited to above-mentioned execution mode, as long as it reaches technique effect of the present invention with identical means, within all should belonging to protection scope of the present invention.
Claims (7)
1. a novel aviation connector that is applied to distribution power automation terminal, it is characterized in that: described aviation connector comprises
The plug coupling assembling, it comprises aviation plug (1) and the upper cover (2) be fixedly connected with, and wherein said aviation plug (1) upper end is provided with the socket (11) supporting with the panel switches Connection Block, and described upper cover (2) lower end is provided with screw (21);
Cover member, it comprises outer cover (3), described outer cover (3) is fixedly connected to form a closed container (30) by screw (21) and described plug coupling assembling.
2. a kind of novel aviation connector that is applied to distribution power automation terminal according to claim 1, it is characterized in that: described outer cover (3) lower end is provided with screw thread (31), by it, is connected with an observation window, and described observation window is airtight window (4).
3. a kind of novel aviation connector that is applied to distribution power automation terminal according to claim 1, it is characterized in that: described aviation plug (1) lower end is provided with the connecting hole (12) be connected and fixed with upper cover (2), and described connecting hole (12) and the screw (21) that is arranged at described upper cover (2) lower end all adopt blind hole structure.
4. a kind of novel aviation connector that is applied to distribution power automation terminal according to claim 2, is characterized in that: between described plug coupling assembling, cover member and observation window, adopt the antiseepage ability of swimming to be tightly connected.
5. a kind of novel aviation connector that is applied to distribution power automation terminal according to claim 4, it is characterized in that: described upper cover (2), outer cover (3) lower end are provided with sealing ring mounting groove (5).
6. a kind of novel aviation connector that is applied to distribution power automation terminal according to claim 4, is characterized in that: described outer cover (3) upper end-face edge employing hierarchic structure.
7. a kind of novel aviation connector that is applied to distribution power automation terminal according to claim 2 is characterized in that: described airtight window (4) is conical, and described closed container (30) is cylindrical.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310391823.7A CN103490213A (en) | 2013-09-02 | 2013-09-02 | Novel aviation connector for distribution automation terminal |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310391823.7A CN103490213A (en) | 2013-09-02 | 2013-09-02 | Novel aviation connector for distribution automation terminal |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103490213A true CN103490213A (en) | 2014-01-01 |
Family
ID=49830257
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310391823.7A Pending CN103490213A (en) | 2013-09-02 | 2013-09-02 | Novel aviation connector for distribution automation terminal |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103490213A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2812506Y (en) * | 2005-04-15 | 2006-08-30 | 山东力创科技有限公司 | FTU intelligent electric test control terminal |
| US20110159727A1 (en) * | 2009-12-28 | 2011-06-30 | Matt Howard | Power distribution device |
| CN202796778U (en) * | 2012-07-05 | 2013-03-13 | 山西省电力公司长治供电分公司 | Intelligent integrated 10 kV breaker |
| CN203553446U (en) * | 2013-09-02 | 2014-04-16 | 珠海许继电气有限公司 | Novel aviation connector applied to distribution automation terminals |
-
2013
- 2013-09-02 CN CN201310391823.7A patent/CN103490213A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2812506Y (en) * | 2005-04-15 | 2006-08-30 | 山东力创科技有限公司 | FTU intelligent electric test control terminal |
| US20110159727A1 (en) * | 2009-12-28 | 2011-06-30 | Matt Howard | Power distribution device |
| CN202796778U (en) * | 2012-07-05 | 2013-03-13 | 山西省电力公司长治供电分公司 | Intelligent integrated 10 kV breaker |
| CN203553446U (en) * | 2013-09-02 | 2014-04-16 | 珠海许继电气有限公司 | Novel aviation connector applied to distribution automation terminals |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C12 | Rejection of a patent application after its publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20140101 |