CN220730714U

CN220730714U - Integrated radiating computer panel structure

Info

Publication number: CN220730714U
Application number: CN202321758716.9U
Authority: CN
Inventors: 方安定; 林义铭
Original assignee: Jiete Technology Guangdong Co ltd
Current assignee: Jiete Technology Guangdong Co ltd
Priority date: 2023-07-05
Filing date: 2023-07-05
Publication date: 2024-04-05
Anticipated expiration: 2033-07-05

Abstract

The utility model discloses an integrated heat dissipation computer panel structure, which comprises a panel and an eddy current sealing fan, wherein the eddy current sealing fan is arranged at a fluid inlet of the panel, the turbofan is arranged at the position of the fluid inlet, the flow guiding structure is arranged at the inner side of the panel and is provided with air outlets, the air outlets are distributed along the length direction of the panel, the flow guiding structure is provided with flow guiding channels, one ends of the flow guiding channels are matched with the turbofan, and the other ends of the flow guiding channels are matched with the air outlets. Through the integrated design of the turbofan and the flow guide structure in the panel, the use of the fan can be reduced, meanwhile, fluid can be pressurized through the turbofan and conveyed into the chassis through the flow guide structure, the direct cooling of hardware in the chassis computer can be realized, and meanwhile, the fluid through the flow guide structure can be directly discharged out of the chassis through a heat radiation port positioned on the opposite side of the chassis panel; the generation of deflection flow can be avoided through the single turbofan, the fan can not be exposed, and the design of the bladeless fan is realized.

Description

Integrated radiating computer panel structure

Technical Field

The utility model relates to the field of computers, in particular to an integrated heat dissipation computer panel structure.

Background

With the development of computers, the higher the working frequency, the more serious the heat generation, so one of the design directions of the existing computers is how to solve the heat dissipation. At the same time, with the limitation of computer development, the key to how to form differential competition is the design of computer panels.

Most designs are to design a cooling fan on a panel to draw out the hot air flow in the computer or convey the air flow to the inside of the computer, but both designs have exposed fans, have poor appearance design, and cannot realize the whole cooling of the computer (such as easy flow deflection when a plurality of fans are used to influence the unidirectional movement of the fluid).

Disclosure of Invention

The utility model mainly aims to provide an integrated heat-dissipation computer panel structure, which aims to improve the existing heat-dissipation structure and ensure the beautiful design of a chassis panel.

In order to achieve the above object, the present utility model provides an integrated heat dissipation computer panel structure, comprising:

a panel disposed at the fluid inlet of the panel;

a turbofan provided at a position of the fluid inlet;

the air outlet is distributed along the length direction of the panel, the air guide structure is provided with a guide channel, one end of the guide channel is matched with the turbofan, and the other end of the guide channel is matched with the air outlet.

According to the technical scheme, the turbofan and the flow guide structure are integrally designed in the panel, so that the use of the fan can be reduced, meanwhile, fluid can be pressurized through the turbofan and conveyed into the chassis through the flow guide structure, the hardware in the chassis computer can be directly cooled, and meanwhile, the fluid through the flow guide structure can be directly discharged out of the chassis through the heat radiation ports on the opposite side of the chassis panel; the generation of deflection flow can be avoided through the single turbofan, the fan can not be exposed, and the design of the bladeless fan is realized.

Drawings

FIG. 1 is a cross-sectional view of the present utility model;

FIG. 2 is a second cross-sectional view of the present utility model;

FIG. 3 is an exploded view of the present utility model;

FIG. 4 is a second exploded view of the present utility model;

FIG. 5 is a schematic perspective view of the first embodiment of the present utility model;

FIG. 6 is a second perspective view of the present utility model;

fig. 7 is a schematic view of the present utility model after being mounted in a chassis.

In the figure, 1 is a panel, 11 is a fluid inlet, 2 is a turbofan, 21 is a rotating motor, 22 is an impeller, 23 is a blade, 3 is a flow guiding structure, 31 is an air outlet, 32 is a flow guiding channel, 41 is a baffle, 42 is a baffle, 51 is a first chamber, 52 is a second chamber, 61 is a flow guiding cover, and 62 is a flow scratching plate.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and fully with reference to the accompanying drawings, in which it is evident that the embodiments described are only some, but not all embodiments of the utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

It should be noted that, in the embodiment of the present utility model, directional indications (such as up, down, left, right, front, rear, top, bottom, inner, outer, vertical, lateral, longitudinal, counterclockwise, clockwise, circumferential, radial, axial … …) are referred to, and the directional indications are merely used to explain the relative positional relationship, movement conditions, etc. between the components in a specific posture (as shown in the drawings), and if the specific posture is changed, the directional indications are correspondingly changed.

In addition, if there is a description of "first" or "second" etc. in the embodiments of the present utility model, the description of "first" or "second" etc. is only for descriptive purposes, and is not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include at least one such feature. In addition, the technical solutions of the embodiments may be combined with each other, but it is necessary to base that the technical solutions can be realized by those skilled in the art, and when the technical solutions are contradictory or cannot be realized, the combination of the technical solutions should be considered to be absent and not within the scope of protection claimed in the present utility model.

As shown in fig. 1 to 7, a computer panel structure with integrated heat dissipation includes:

a panel 1, a fluid inlet 11 provided in the panel 1;

the turbofan 2 is provided at the position of the fluid inlet 11, preferably inside the panel 1, but may be provided outside the panel 1;

the air guide structure 3, the inboard that the air guide structure 3 located panel 1 just is equipped with air outlet 31, air outlet 31 distributes along the length direction of panel 1, and wherein the air guide structure 3 length can be the half, the third of panel 1 length, the air guide structure 3 is equipped with water conservancy diversion passageway 32, the one end and the turbofan 2 of water conservancy diversion passageway 32 cooperate, and the other end cooperatees with air outlet 31.

Through the integrated design of the turbofan 2 and the flow guide structure 3 in the panel 1, the use of the fan can be reduced, meanwhile, fluid can be pressurized through the turbofan 2 and conveyed into the chassis through the flow guide structure 3, the direct cooling of hardware in the chassis computer can be realized, and meanwhile, the fluid through the flow guide structure 3 can be directly discharged out of the chassis through a heat radiation port positioned on the opposite side of the chassis panel 1; the generation of the turbulent flow can be avoided by the single turbofan 2, the fan can not be exposed, and the design of the bladeless fan is realized.

Specifically, the inner side wall of the panel 1 is provided with a flange 41, the flange 41 is provided with a detachable baffle 42, the flange 41 and the baffle 42 enclose a first chamber 51 and a second chamber 52, the first chamber 51 is used for installing the turbofan 2, the second chamber 52 is a flow guiding structure 3, and the flange 41 formed integrally can reduce the later installation stability of the heat dissipation system, and meanwhile, the installed structure is more stable; that is, the turbo fan compresses the fluid in the first chamber 51 and then enters the second chamber 52.

More specifically, the first chamber 51 is circular, and the turbofan 2 is offset from the center of the first chamber 51, because the fluid generated by the turbofan 2 is in a non-annular shape and flows in one direction, the eccentric design is adopted, so that the generation of deflection flow can be reduced, and the fluid pressure (i.e. the fluid is compressed) can be improved.

In the embodiment of the present utility model, the flow guiding channel 32 is in a "U" shape, and of course, the specific structure may also be composed of a plurality of vertical strip-shaped flow guiding channels 32 arranged at intervals, or a flow guiding channel 32 with a planar structure; other shapes are also possible, the main shape is mainly suitable for actively radiating the whole or partial hardware in the case, such as inverted U-shaped or U-shaped rotated by 90 degrees

Further, the air outlet 31 is provided on the baffle 42.

Further, the first chamber 51 is provided with an inclined air guide sleeve 61, one end of the air guide sleeve 61 is connected with the fluid inlet 11, and the other side is matched with the turbofan, so that the fluid of the turbofan can be more concentrated, and the flow pressure of the fluid can be increased.

In the embodiment of the utility model, the flange 41 is integrally formed with the panel 1 or is mounted separately.

Specifically, the first chamber 51 is provided with a flow-scratching plate 62 at the position of the flow-guiding structure 3, and the flow-scratching plate 62 has the function of blocking the fluid so as to enter the flow-guiding channel 32.

More specifically, the turbofan 2 includes a rotating electric machine 21 and an impeller 22 provided to the rotating electric machine 21, the impeller 22 being composed of a plurality of curved blades 23, by which a better fluid compression effect can be achieved.

In the embodiment of the utility model, the fluid inlet 11 is provided with the dust screen, so that the heat dissipation structure with a larger area of the existing panel 1 can be effectively reduced, and the dust prevention effect in the chassis is affected.

The foregoing description is only of the preferred embodiments of the present utility model, and is not intended to limit the scope of the utility model, but rather, the equivalent structural changes made by the description of the present utility model and the accompanying drawings or the direct/indirect application in other related technical fields are included in the scope of the utility model.

Claims

1. An integrated heat dissipating computer panel structure comprising:

a panel disposed at the fluid inlet of the panel;

a turbofan provided at a position of the fluid inlet;

2. The integrated heat dissipating computer panel structure of claim 1, wherein: the inner side wall of the panel is provided with a flange, the flange is provided with a detachable baffle, the flange and the baffle enclose a first chamber and a second chamber, the first chamber is used for installing the turbofan, and the second chamber is of a flow guiding structure.

3. The integrated heat dissipating computer panel structure of claim 2, wherein: the first chamber is circular, and the turbofan is deviated from the center position of the first chamber.

4. The integrated heat dissipating computer panel structure of claim 1, wherein: the flow guide channel is U-shaped or mouth-shaped.

5. The integrated heat dissipating computer panel structure of claim 2, wherein: the air outlet is arranged on the baffle.

6. The integrated heat dissipating computer panel structure of claim 2, wherein: the first chamber is provided with an inclined guide cover, one end of the guide cover is connected with the fluid inlet, and the other side face of the guide cover is matched with the turbofan.

7. The integrated heat dissipating computer panel structure of claim 2, wherein: the flange and the panel are integrally formed or mounted in a split mode.

8. The integrated heat dissipating computer panel structure of claim 2, wherein: the first chamber is provided with a flow deflection plate at the position of the flow guide structure.

9. The integrated heat dissipating computer panel structure of claim 1, wherein: the turbofan comprises a rotating motor and an impeller arranged on the rotating motor, wherein the impeller consists of a plurality of curved blades.

10. The integrated heat dissipating computer panel structure of claim 1, wherein: the fluid inlet is provided with a dust screen.