Chassis

Abstract

The utility model discloses a chassis, which relates to the technical field of electronic equipment. The chassis includes: a panel; a flight plug plate, which is arranged opposite to the panel along a first direction; a first side panel, which is respectively connected to the panel and one side of the flight plug plate along the first direction; a plurality of first through slots, which are provided in the first side panel; a second side panel, which is arranged opposite to the first side panel and is respectively connected to one side of the panel and the flight plug plate; a plurality of second through slots, which are provided in the second side panel; a first cover plate, which is respectively connected to the top of the panel, the flight plug plate, the first side panel and the second side panel. The utility model solves the problem in the prior art that the chassis shell is generally designed to be large enough to hide the connector in the shell, which increases the volume and weight of the chassis, and also increases the manufacturing cost, and the heat dissipation effect is not good.

Description

Technical Field

[0001] The utility model relates to the technical field of electronic equipment, in particular to a chassis. Background Art

[0002] In actual applications, the exposed connectors of electronic equipment are subject to collision during transportation or installation. Connectors that are hit by collisions are easily damaged, rendering the electronic equipment unusable. In order to reduce damage to connectors caused by collisions and falls, a protective structure needs to be designed to protect the connectors.

[0003] In the prior art, the chassis shell is generally designed to be large enough to hide the connector inside the shell, which increases the size and weight of the chassis, increases the manufacturing cost, and causes poor heat dissipation. No effective solution has been proposed so far for the above problems. Utility Model Content

[0004] Purpose of the utility model: to provide a chassis to solve the above problems existing in the prior art.

[0005] Technical solution: Chassis, including:

[0006] panel;

[0007] A flight board, arranged opposite to the panel along a first direction;

[0008] A first side plate connected to the panel and one side of the flight plug board respectively along the first direction;

[0009] A plurality of first through slots are formed on the first side plate;

[0010] A second side panel is arranged opposite to the first side panel and is respectively connected to the panel and one side of the flight plug board;

[0011] A plurality of second through slots are formed on the second side plate;

[0012] A first cover plate is connected to the top of the panel, the flight plug plate, the first side plate and the second side plate respectively;

[0013] A second cover plate is arranged opposite to the first cover plate and is respectively connected to the bottom of the panel, the flight plug plate, the first side plate and the second side plate;

[0014] A heat dissipation component, disposed on an outer surface of either the first side plate or the second side plate;

[0015] Among them, a hollow accommodating cavity is formed by enclosing the panel, the aviation plug plate, the first side plate, the second side plate, the first cover plate and the second cover plate, and the heat in the hollow accommodating cavity is directionally dissipated through the first through grooves and the second through grooves by the heat dissipation component.

[0016] Preferably, a plurality of first limiting portions are arranged on the inner wall of the first side plate at intervals along the first direction.

[0017] Preferably, a plurality of second limiting portions are arranged at intervals on the inner wall of the second side plate along the first direction, and the second limiting portions are arranged opposite to the first limiting portions.

[0018] Preferably, the upper end surfaces of the first limiting portion and the second limiting portion located on the same plane are provided with a single-board structure, and the single-board structure is used to assemble and fix each standardized module in the system structure.

[0019] Preferably, the single board structure is connected to the aviation plug board via a backboard.

[0020] Preferably, a heat dissipation boss is provided on the single board structure, and a plurality of heat dissipation teeth are spaced apart above the heat dissipation boss.

[0021] Preferably, a hollow portion is further provided on the single plate structure.

[0022] Preferably, the heat dissipation component comprises: a fan frame, a plurality of fan bases are arranged on the fan frame, and a heat dissipation fan is arranged on the fan base.

[0023] Preferably, a plurality of stoppers are disposed on inner walls of the first side plate and the second side plate respectively.

[0024] Preferably, a third limiting portion is provided on the upper surface of the second cover plate.

[0025] Beneficial effect: In the embodiment of the present application, the structure is optimized and a heat dissipation component is added. The panel, the aviation plug plate, the first side panel, the second side panel, the first cover plate and the second cover plate are used to enclose a hollow accommodating cavity, and the heat in the hollow accommodating cavity is directionally dissipated through the first through grooves and the second through grooves by the heat dissipation component, thereby achieving the purpose of simplifying the structure and heat dissipation, thereby achieving the technical effect of reducing costs and increasing service life, and further solving the problem in the prior art that the chassis shell is generally designed to be large enough to hide the connector in the shell, which increases the volume and weight of the chassis, and also increases the manufacturing cost, as well as the technical problem of poor heat dissipation effect. BRIEF DESCRIPTION OF THE DRAWINGS

[0026] Figure 1It is a schematic diagram of the three-dimensional structure of the chassis of the utility model;

[0027] Figure 2 It is another schematic diagram of the three-dimensional structure of the chassis of the utility model;

[0028] Figure 3 It is a schematic diagram of the internal three-dimensional structure of the chassis of the utility model;

[0029] Figure 4 It is another schematic diagram of the internal three-dimensional structure of the chassis of the utility model;

[0030] Figure 5 is a schematic diagram of the three-dimensional structure of the first side panel of the chassis of the utility model; and

[0031] Figure 6 It is a three-dimensional structural schematic diagram of a single board structure of a chassis of the utility model.

[0032] The accompanying drawings are marked as follows:

[0033] 10. Panel;

[0034] 20. Navigation board;

[0035] 30. first side plate; 301. first through slot; 302. first position limiting portion;

[0036] 40. second side plate; 401. second through slot; 402. second position limiting portion;

[0037] 50. a first cover plate;

[0038] 60. Second cover plate; 601. Third limiting portion;

[0039] 70. heat dissipation component; 701. fan frame; 702. fan base;

[0040] 80, single board structure; 801, heat dissipation boss; 802, heat dissipation teeth; 803, hollow part;

[0041] 90. Back panel;

[0042] 100. Stop block. DETAILED DESCRIPTION

[0043] In order to enable those skilled in the art to better understand the solution of the present application, the technical solution in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by ordinary technicians in this field without creative work should fall within the scope of protection of the present application.

[0044] It should be noted that the terms "first", "second", etc. in the specification and claims of the present application and the above-mentioned drawings are used to distinguish similar objects, and are not necessarily used to describe a specific order or sequential order. It should be understood that the data used in this way can be interchanged where appropriate, so that the embodiments of the present application described here. In addition, the terms "including" and "having" and any of their variations are intended to cover non-exclusive inclusions, for example, a process, method, system, product or device comprising a series of steps or units is not necessarily limited to those steps or units clearly listed, but may include other steps or units that are not clearly listed or inherent to these processes, methods, products or devices.

[0045] In addition, the terms "installed", "set", "provided with", "connected", "connected", and "socketed" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral structure; it can be a mechanical connection, or an electrical connection; it can be a direct connection, or an indirect connection through an intermediate medium, or it can be an internal connection between two devices, elements, or components. For those of ordinary skill in the art, the specific meanings of the above terms in this utility model can be understood according to specific circumstances.

[0046] It should be noted that, in the absence of conflict, the embodiments and features in the embodiments of the present application can be combined with each other. The present application will be described in detail below with reference to the accompanying drawings and in combination with the embodiments.

[0047] like Figure 1-4 As shown, the present application relates to a chassis. The chassis includes: a panel 10; the panel 10 refers to a front panel 10, and by vertically arranging the panel 10, a good protection effect can be achieved, and at the same time, a good coordination effect with other components can be achieved.

[0048] The flight plug board 20 is arranged relative to the panel 10 along a first direction; by arranging the flight plug board 20 and the panel 10 relatively vertically, a good matching effect can be achieved, and at the same time, a good plug-in effect with other components can be achieved, thereby ensuring a stable electrical connection effect between the components. The first direction refers to the horizontal direction.

[0049] The first side panel 30 is connected to one side of the panel 10 and the flight board 20 respectively along the first direction; it can achieve a good side protection effect, and at the same time, can also achieve a good assembly effect with the panel 10 and the flight board 20.

[0050] A plurality of first through slots 301 are provided on the first side panel 30; by providing a plurality of first through slots 301 on the first side panel 30, a good air circulation effect can be ensured, thereby providing a basis for good heat dissipation. Of course, the number and position of the first through slots 301 can be set according to actual usage requirements, and are not limited in the present application.

[0051] The second side plate 40 is arranged opposite to the first side plate 30 and is respectively connected to one side of the panel 10 and the flight plug plate 20; it can achieve a good enclosure effect on both sides, thereby forming a cavity with open ends.

[0052] A plurality of second through slots 401 are provided on the second side panel 40; by providing a plurality of second through slots 401 on the second side panel 40, a good air circulation effect can be ensured, thereby providing a basis for good heat dissipation. Of course, the number and position of the second through slots 401 can be set according to actual usage requirements, and are not limited in the present application.

[0053] The first cover plate 50 is respectively connected to the top of the panel 10, the flight plug plate 20, the first side plate 30 and the second side plate 40, and can achieve a good top covering effect, thereby achieving a good protection effect.

[0054] The second cover plate 60 is arranged opposite to the first cover plate 50, and is respectively connected to the bottom of the panel 10, the flight plug plate 20, the first side plate 30 and the second side plate 40; it can achieve a good bottom covering effect, thereby achieving a good protection effect.

[0055] The heat dissipation assembly 70 is disposed on the outer surface of any one of the first side plate 30 or the second side plate 40 , and can achieve a good heat dissipation effect.

[0056] Among them, a hollow accommodating cavity is formed by enclosing the panel 10, the flight plug plate 20, the first side plate 30, the second side plate 40, the first cover plate 50 and the second cover plate 60, and the heat in the hollow accommodating cavity is directionally dissipated through the first through grooves 301 and the second through grooves 401 respectively by the heat dissipation component 70. By using multiple plates to enclose a hollow accommodating cavity, a good assembly effect can be achieved, and at the same time, a good component protection effect can also be achieved. At the same time, in order to reduce the temperature inside the hollow accommodating cavity to protect its internal components, a heat dissipation component 70 is provided on the outer surface of any first side plate 30 or the second side plate 40, which can ensure a good heat dissipation effect, thereby achieving the effect of reducing the temperature inside the hollow accommodating cavity.

[0057] By adopting the structure of the present application, the weight is reduced and the heat dissipation effect is enhanced. Taking into account both the heat dissipation performance and the overall weight, this hollow design greatly reduces the weight of the whole machine and the single board, and is more suitable for scenes with strict weight requirements.

[0058] From the above description, it can be seen that the present application achieves the following technical effects:

[0059] In the embodiment of the present application, the structure is optimized and a heat dissipation component 70 is added. The panel 10, the aviation plug plate 20, the first side panel 30, the second side panel 40, the first cover plate 50 and the second cover plate 60 are used to enclose a hollow accommodating cavity, and the heat in the hollow accommodating cavity is directionally dissipated through the first through grooves 301 and the second through grooves 401 by the heat dissipation component 70, thereby achieving the purpose of simplifying the structure and heat dissipation, thereby achieving the technical effect of reducing costs and increasing service life, and further solving the problem in the prior art that the chassis shell is generally designed to be large enough to hide the connector in the shell, such a design will increase the size and weight of the chassis, and will also increase the manufacturing cost, as well as the technical problem of poor heat dissipation effect.

[0060] like Figure 5 As shown, the inner wall of the first side plate 30 is provided with a plurality of first limiting portions 302 at intervals along the first direction. It can be understood that a good limiting and fixing effect can be achieved, and at the same time, a good assembly effect with other components can be achieved.

[0061] Furthermore, the inner wall of the second side plate 40 is provided with a plurality of second limiting portions 402 at intervals along the first direction, and the second limiting portions 402 are arranged opposite to the first limiting portions 302. It can be understood that the effect of ensuring stable assembly of other components can be ensured.

[0062] like Figure 6 As shown, the upper end surfaces of the first limiting portion 302 and the second limiting portion 402 located on the same plane are provided with a single plate structure 80, and the single plate structure 80 is used to assemble and fix each standardized module in the system structure. It can be understood that a good assembly effect can be achieved, and at the same time, by adopting the single plate structure 80, a good integration effect can be achieved.

[0063] Specifically, the single board structure 80 is mainly used to assemble and fix each standardized module in the system structure, and plays the role of fixing and heat dissipation. Preferably, the size of the single board structure 80 is 160mm (length) * 100mm (width) * 25.4mm (height); the single board structure 80 is processed by aviation aluminum, and the surface is anodized and gold-plated.

[0064] Furthermore, the single board structure 80 is connected to the flight board 20 via a back board 90. It can be understood that a good electrical connection effect can be achieved, thereby ensuring the effect of stable operation of the components.

[0065] Furthermore, a heat dissipation boss 801 is provided on the single board structure 80, and a plurality of heat dissipation teeth 802 are provided at intervals above the heat dissipation boss 801. It can be understood that a good heat dissipation effect can be achieved, thereby achieving a longer service life and ensuring stable operating performance.

[0066] Specifically, a heat dissipation boss 801 is designed above the device with higher power consumption for heat conduction. A heat dissipation tooth 802 is designed above the heat dissipation boss 801 to increase the heat dissipation area, which is beneficial for quickly dissipating the heat generated by the hardware board into the air, ensuring that the board works normally for a long time, and a leaky design is used where no heat dissipation is required.

[0067] Furthermore, a hollow portion 803 is provided on the single plate structure 80. It can be understood that the effect of simplifying the structure can be achieved.

[0068] Further, the heat dissipation assembly 70 includes: a fan frame 701, a plurality of fan bases 702 are arranged on the fan frame 701, and a heat dissipation fan is arranged on the fan base 702. It can be understood that a good air cooling effect can be achieved, thereby improving the air circulation speed. Preferably, the heat dissipation assembly 70 is assembled in a detachable manner, which can achieve the effect of easy disassembly and assembly.

[0069] Furthermore, a plurality of stoppers 100 are disposed opposite to each other on the inner walls of the first side plate 30 and the second side plate 40. It can be understood that a good limiting and fixing effect can be achieved, thereby preventing the single plate structure 80 from being displaced in the horizontal direction.

[0070] Furthermore, a third limiting portion 601 is disposed on the upper surface of the second cover plate 60. It can be understood that a good limiting matching effect can be achieved.

[0071] The preferred embodiments of the present invention are described in detail above in conjunction with the accompanying drawings; however, the present invention is not limited to the specific details in the above embodiments. Within the technical concept of the present invention, various equivalent transformations can be made to the technical scheme of the present invention, and these equivalent transformations all belong to the protection scope of the present invention.

Claims

1. A chassis, characterized in that: include: panel; A flight board, arranged opposite to the panel along a first direction; A first side plate connected to the panel and one side of the flight plug board respectively along the first direction; A plurality of first through slots are formed on the first side plate; A second side panel is arranged opposite to the first side panel and is respectively connected to the panel and one side of the flight plug board; A plurality of second through slots are formed on the second side plate; A first cover plate is connected to the top of the panel, the flight plug plate, the first side plate and the second side plate respectively; A second cover plate is arranged opposite to the first cover plate and is respectively connected to the bottom of the panel, the flight plug plate, the first side plate and the second side plate; A heat dissipation component is disposed on an outer surface of either the first side plate or the second side plate; Among them, a hollow accommodating cavity is formed by enclosing the panel, the aviation plug plate, the first side plate, the second side plate, the first cover plate and the second cover plate, and the heat in the hollow accommodating cavity is directionally dissipated through the first through grooves and the second through grooves by the heat dissipation component.

2. The chassis according to claim 1, characterized in that: The inner wall of the first side plate is provided with a plurality of first limiting portions at intervals along the first direction.

3. The chassis according to claim 2, characterized in that: A plurality of second limiting portions are arranged at intervals on the inner wall of the second side plate along the first direction, and the second limiting portions are arranged opposite to the first limiting portions.

4. The chassis according to claim 3, characterized in that: The upper end surfaces of the first limiting portion and the second limiting portion located on the same plane are provided with a single board structure, and the single board structure is used to assemble and fix each standardized module in the system structure.

5. The chassis according to claim 4, characterized in that: The single board structure is connected to the flight board via a backboard.

6. The chassis according to claim 4, characterized in that: A heat dissipation boss is arranged on the single board structure, and a plurality of heat dissipation teeth are arranged at intervals above the heat dissipation boss.

7. The chassis according to claim 4, characterized in that: The single board structure is also provided with a hollow portion.

8. The chassis according to claim 1, characterized in that: The heat dissipation component comprises a fan frame, a plurality of fan bases are arranged on the fan frame, and a heat dissipation fan is arranged on the fan base.

9. The chassis according to claim 1, characterized in that: A plurality of stoppers are respectively arranged on the inner walls of the first side plate and the second side plate.

10. The chassis according to claim 1, characterized in that: A third limiting portion is disposed on the upper surface of the second cover plate.

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