CN210444680U - Mounting structure that aviation was inserted and switch board thereof - Google Patents
Mounting structure that aviation was inserted and switch board thereof Download PDFInfo
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- CN210444680U CN210444680U CN201920935945.0U CN201920935945U CN210444680U CN 210444680 U CN210444680 U CN 210444680U CN 201920935945 U CN201920935945 U CN 201920935945U CN 210444680 U CN210444680 U CN 210444680U
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- aviation
- support
- mounting structure
- aviation plug
- board
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Abstract
The utility model provides a mounting structure that aviation was inserted and switch board thereof, this mounting structure that aviation was inserted are suitable for and insert the internal at the internal of cabinet of switch board with aviation, and the internal perpendicular roof beam and the skeleton that have mutual parallel arrangement of cabinet, and the mounting structure that aviation was inserted includes: the aviation plug board comprises two supports, an aviation plug board and a fastener, wherein one support is arranged on a vertical beam, and the other support is arranged on a framework; the aviation plug board is provided with two flanges and a plurality of jacks suitable for connecting aviation plugs, and the two flanges extend downwards from two opposite edges of the aviation plug board in a one-to-one correspondence manner; the two flanges are hinged on the two supports in a one-to-one correspondence manner; the fastening piece is connected with the aviation plug board and the support so as to fasten the aviation plug board on the support. The flexible wiring operation that this mounting structure was convenient for the aviation to insert, the aviation of being convenient for operate is inserted, space in the reducible switch board.
Description
Technical Field
The utility model relates to an electric field, in particular to mounting structure that aviation was inserted and switch board thereof.
Background
At present, connectors such as an aviation plug and an aviation socket are adopted to play waterproof and dustproof roles in order to ensure the reliability of a circuit in a control cabinet. However, in the related art, the aviation plug is fixed in the control cabinet, so that the aviation plug is inconvenient to wire and operate and occupies space in the control cabinet.
SUMMERY OF THE UTILITY MODEL
The utility model discloses aim at solving one of the technical problem in the above-mentioned technique to a certain extent at least, even if be convenient for the nimble wiring operation that the aviation inserted, the aviation of being convenient for is inserted, reduces the space in the switch board. Therefore, the first objective of the present invention is to provide an aviation plug mounting structure.
A second object of the present invention is to provide a control cabinet.
In order to achieve the above object, the utility model discloses an installation structure that aviation was inserted is provided to the first aspect, is suitable for to insert the aviation at the internal of the cabinet of switch board, the internal perpendicular roof beam and the skeleton that have mutual parallel arrangement of cabinet, the installation structure that the aviation was inserted includes:
one support is arranged on the vertical beam, and the other support is arranged on the framework;
the aviation plug board is provided with two flanges and a plurality of jacks suitable for being connected with aviation plugs, and the two flanges extend downwards from two opposite edges of the aviation plug board in a one-to-one correspondence manner; the two flanges are hinged on the two supports in a one-to-one correspondence manner;
and the fastener is connected with the aviation plug board and the support so as to fasten the aviation plug board on the support.
According to the utility model discloses an installation structure of aviation plug, through the setting of turn-ups, turn-ups and support articulated, aviation plug board and support pass through fastener fastening connection; make when loosening the fastener, the turn-ups can be rotatory on the support, and then drives the aviation picture peg rotatory, and the aviation of being convenient for easily operate is inserted and is carried out nimble wiring operation, also can reduce the space in the switch board simultaneously.
In addition, according to the utility model discloses the mounting structure that aviation was inserted that above-mentioned embodiment provided can also have following additional technical characteristics:
according to the utility model discloses an embodiment, the support has first extension board, second extension board and third extension board, first extension board laminating is in erect the roof beam or on the skeleton, the second extension board is on a parallel with first extension board setting and laminating are in on the aviation picture peg, the third extension board laminating in the turn-ups and perpendicular connection first extension board with the second extension board.
According to an embodiment of the present invention, the flange is hinged to the third support plate; the fastener is connected with the aviation flashboard and the second supporting board.
According to the utility model discloses an embodiment, the fastener includes screw rod and nut, the screw rod connects soon the support with on the aviation picture peg and follow the aviation picture peg is worn out, the nut locking is in the screw rod is followed on the tip that the aviation picture peg was worn out, with the aviation picture peg fastening is in on the support.
According to the utility model discloses an embodiment, the turn-ups with the support passes through the bolt hinge.
In a second aspect of the present invention, the present invention provides a control cabinet, which includes the above-mentioned aviation plug-in mounting structure. From this, through the mounting structure that this aviation was inserted, can easily operate the aviation in the switch board and insert and carry out nimble wiring operation, also can reduce the space in the switch board simultaneously.
Drawings
Fig. 1 is a schematic view of an installation structure of an aviation plug according to an embodiment of the present invention;
fig. 2 is an exploded schematic view of an aerial pod mounting structure according to an embodiment of the present invention;
fig. 3 is a schematic structural diagram of a control cabinet according to an embodiment of the present invention;
description of reference numerals: the control cabinet 10, the cabinet body 11, the vertical beam 12, the framework 13, the support 14, the first support plate 141, the second support plate 142, the third support plate 143, the aviation flashboard 15, the flanging 151, the jack 152, the fastener 16, the screw 161, the nut 162 and the bolt 17.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary and intended to be used for explaining the present invention, and should not be construed as limiting the present invention.
In order to better understand the above technical solutions, exemplary embodiments of the present invention will be described in more detail below with reference to the accompanying drawings. While exemplary embodiments of the invention are shown in the drawings, it should be understood that the invention can be embodied in various forms and should not be limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art.
The following describes a mounting structure of an aviation plug according to an embodiment of the present invention with reference to the drawings.
As shown in fig. 1-3, according to the utility model discloses mounting structure that aviation was inserted is suitable for inserting the aviation and installs in the cabinet body 11 of switch board 10, has mutual parallel arrangement's perpendicular roof beam 12 and skeleton 13 in the cabinet body 11, and this mounting structure that aviation was inserted includes: two supports 14, an aviation flashboard 15 and a fastener 16.
Specifically, one of the two supports 14 is disposed on the vertical beam 12, and the other support is disposed on the framework 13; the aviation plug board 15 is provided with two flanges 151 and a plurality of jacks 152 suitable for being connected with aviation plugs, and the two flanges 151 extend downwards from two opposite edges of the aviation plug board 15 in a one-to-one correspondence manner; the two flanges 151 are hinged on the two supports 14 in a one-to-one correspondence manner; the fastener 16 connects the aircraft insert panel 15 and the support base 14 to fasten the aircraft insert panel 15 to the support base 14.
That is, the support 14 is fixed on the vertical beam 12 or the framework 13 in the cabinet 11, and the aviation flashboard 15 is hinged on the support 14 through the flanging 151 and is fastened on the support 14 through the fastening piece 16. Therefore, through the arrangement of the flanging 151, the flanging 151 is hinged with the support 14, and the aviation plug board 15 is tightly connected with the support 14 through the fastening piece 16; when the fastening piece 16 is loosened, the flanging 151 can rotate on the support 14, so that the aviation plugboard 15 is driven to rotate, aviation plugboards can be easily operated, flexible wiring operation can be conveniently carried out, and meanwhile, the space in the control cabinet can be reduced. It should be understood that the support 14 of the present invention is not limited to the vertical beam 12 or the frame 13 disposed in the cabinet 11, and may be installed at other positions in the cabinet 11. In addition, in the present embodiment, the support 14 is fixed to the vertical beam 12 or the framework 13 by screws.
In some examples, the support 14 is generally zigzag-shaped, the support 14 has a first support plate 141, a second support plate 142, and a third support plate 143, the first support plate 143 is attached to the vertical beam 12 or the framework 13, the second support plate 142 is disposed parallel to the first support plate 141 and is attached to the aircraft insertion panel 15, and the third support plate 143 is attached to the flange 151 and vertically connects the first support plate 141 and the second support plate 142. That is, the first support plate 141 and the second support plate 142 are respectively vertically engaged with two opposite sides of the third support plate 143; the first support plate 141 can be fixed on the vertical beam 12 or the framework 13 through screws, so that the support 14 is arranged on the vertical beam 12 or the framework 13, the second support plate 142 is attached to the aviation insertion plate 15, and the third support plate 143 is attached to the flange 151, so that the aviation insertion plate 15 is arranged on the support 14.
Further, the turned-over edge 151 is hinged with the third support plate 143, and the fastener 16 connects the aviation plug board 15 with the second support plate 142. That is, the turned-over edge 151 is attached to and hinged to the third support plate 143; the aviation plug board 15 is attached to the second support plate 142 and connected through the fastener 16, so that when the fastener 16 fastens the aviation plug board 15 and the second support plate 142, the aviation plug board 15 is firmly installed on the support 14, and when the fastener 16 is unscrewed, the aviation plug board 15 can rotate relative to the support 14, so that an operator can operate the aviation plug board conveniently, and wiring operation is facilitated.
In some examples, the fastener 16 may include a threaded rod 161 and a nut 162, the threaded rod 161 being threaded onto the support 14 and the aircraft insert panel 15 and extending out of the aircraft insert panel 15, the nut 162 being tightened onto the end of the threaded rod 161 extending out of the aircraft insert panel 15 to secure the aircraft insert panel 15 to the support 14. That is, the screw 161 is screwed at the position where the second support plate 142 and the aviation plug board 15 are jointed, and penetrates out of the aviation plug board 15 to be locked with the nut 162, so as to tightly connect the second support plate 142 and the aviation plug board 15. The screw 161 may be fixed on the opposite surface of the second support plate 142 facing the aviation plug board 15, and the nut 162 may be a nut structure with a nut, so as to facilitate screwing in or screwing out the screw 161.
In some examples, the flange 151 is hingedly connected to the support 14 by bolts 17. Specifically, the flange 151 is hinged to the third support plate 143 through the bolt 17, and is hinged through the bolt 17, so that when the fastener 16 is loosened, the aviation plug board 15 can rotate along the rotation point of the bolt 17, and aviation plug operation and flexible wiring operation are facilitated.
In a second aspect of the present invention, the present invention provides a control cabinet 10, which includes the above-mentioned aviation plug mounting structure. Therefore, the aviation plug can be easily operated and flexible wiring operation can be carried out in the control cabinet 10 through the aviation plug mounting structure, and meanwhile, the space in the control cabinet can be reduced.
Other components within the control cabinet 10 according to embodiments of the present invention are components within existing control cabinets and will not be described in detail herein.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and to simplify the description, but do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore should not be construed as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically limited otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
In the present disclosure, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact between the first and second features, or may comprise contact between the first and second features not directly. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above should not be understood to necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, various embodiments or examples described in this specification can be combined and combined by those skilled in the art.
Although embodiments of the present invention have been shown and described, it is understood that the above embodiments are exemplary and should not be construed as limiting the present invention, and that variations, modifications, substitutions and alterations can be made to the above embodiments by those of ordinary skill in the art without departing from the scope of the present invention.
Claims (6)
1. The utility model provides a mounting structure that aviation was inserted, is suitable for inserting the aviation and installs the internal at the cabinet of switch board, a serial communication port, the internal perpendicular roof beam and the skeleton that have mutual parallel arrangement of cabinet, mounting structure that the aviation was inserted includes:
one support is arranged on the vertical beam, and the other support is arranged on the framework;
the aviation plug board is provided with two flanges and a plurality of jacks suitable for being connected with aviation plugs, and the two flanges extend downwards from two opposite edges of the aviation plug board in a one-to-one correspondence manner; the two flanges are hinged on the two supports in a one-to-one correspondence manner;
and the fastener is connected with the aviation plug board and the support so as to fasten the aviation plug board on the support.
2. The aircraft insert mounting structure according to claim 1, wherein the seat has a first leg plate, a second leg plate and a third leg plate, the first leg plate being attached to the vertical beam or the framework, the second leg plate being disposed parallel to the first leg plate and being attached to the aircraft insert plate, the third leg plate being attached to the flange and perpendicularly connecting the first leg plate and the second leg plate.
3. The aviation plug mounting structure of claim 2, wherein said flange is hingedly connected to said third strip; the fastener is connected with the aviation flashboard and the second supporting board.
4. An aircraft insert mounting structure according to claim 1, wherein the fastener comprises a threaded rod and a nut, the threaded rod is screwed onto and out of the carrier and the aircraft insert plate, and the nut is locked onto the end of the threaded rod that is out of the aircraft insert plate to fasten the aircraft insert plate to the carrier.
5. The aircraft insert mounting structure of claim 1 wherein said flange is bolted to said support.
6. A control cabinet, characterized by comprising an aviation plug mounting structure according to any one of claims 1 to 5.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920935945.0U CN210444680U (en) | 2019-06-20 | 2019-06-20 | Mounting structure that aviation was inserted and switch board thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920935945.0U CN210444680U (en) | 2019-06-20 | 2019-06-20 | Mounting structure that aviation was inserted and switch board thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210444680U true CN210444680U (en) | 2020-05-01 |
Family
ID=70403690
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920935945.0U Active CN210444680U (en) | 2019-06-20 | 2019-06-20 | Mounting structure that aviation was inserted and switch board thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210444680U (en) |
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2019
- 2019-06-20 CN CN201920935945.0U patent/CN210444680U/en active Active
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