CN217721864U - Splicing processor easy to dissipate heat - Google Patents

Abstract

The utility model relates to a concatenation treater technical field just discloses an easy heat dissipation type's concatenation treater, which comprises a bod, the front end fixed mounting of fuselage has the connector, the fixed chamber of the equal fixedly connected with in the left and right sides of fuselage, the one end joint that the fuselage was kept away from to fixed chamber has the dust screen, the center that fixed chamber is close to fuselage one end is rotated and is connected with the fan, the upper and lower both ends of fixed intracavity portion all set up flutedly, the equal sliding connection in the left and right sides of recess portion has the slider, and this easy heat dissipation type's concatenation treater is opened the back through the drive fan and is accelerated inside and external circulation of air speed of fuselage, and then cools down to the inside of fuselage, can avoid the dust to get into the inside of fixed chamber and fuselage through the dust screen that sets up, and then avoids the dust to pile up and influence the heat dissipation, can make the telescopic link not be with the slider joint through pressing the push rod, and then can dismantle the dust screen so that the washing.

Description

Splicing processor easy to radiate heat

Technical Field

The utility model relates to a concatenation treater technical field specifically is a concatenation treater of easy heat dissipation type.

Background

The splicing processor is to cut apart video signal into a plurality of display element all the way, display element signal output after will cutting apart to a plurality of display terminal to accomplish and constitute a complete image with a plurality of display screen concatenations, splicing processor is various at present, but can not be better dispel the heat in the use, can lead to because splicing processor inner assembly temperature is overheated, and then the unable normal operating's of splicing processor condition appears.

SUMMERY OF THE UTILITY MODEL

For the purpose that realizes above-mentioned being convenient for dispel the heat and clear up the concatenation treater, the utility model provides a following technical scheme: the utility model provides a concatenation treater of easy heat dissipation type, includes the fuselage, the front end fixed mounting of fuselage has the connector, the fixed chamber of the equal fixedly connected with in the left and right sides of fuselage, the one end joint that the fuselage was kept away from to fixed chamber has the dust screen, the center that fixed chamber is close to fuselage one end is rotated and is connected with the fan, the upper and lower both ends of fixed intracavity portion are all seted up flutedly, the equal sliding connection in the left and right sides of recess inside has the slider, the draw-in groove has been seted up on the top of slider, two the one end fixed mounting that the slider was kept away from each other has the push rod, two the one end fixedly connected with reset spring that the slider is close to each other, the dust screen is close to the one end fixed mounting of fixed intracavity portion and has the telescopic link, the equal fixed mounting in upper and lower both ends of telescopic link has the kelly.

As optimization, the through holes with even intervals are formed in one end, close to the machine body, of the fixed cavity and communicated with the machine body, so that air in the fixed cavity and the machine body can circulate to dissipate heat in the machine body.

As optimization, the end of the fixed cavity, which is far away from the machine body, is provided with a notch, the dust screen is fixedly installed at the edge of the notch, and the outer edge surface of the dust screen is flush with the outer surface of the fixed cavity.

As an optimization, the fan is electrically connected with an external power supply, and the fan is connected with a remote controller through signals, so that the switch of the fan can be conveniently controlled.

Preferably, the push rod penetrates through the fixed cavity and extends to the outside of the fixed cavity, and the push rod can be pushed to drive the sliding block to move at the outside.

Preferably, the telescopic rod is formed by combining a hollow rod fixedly connected with the dust screen, solid rods slidably connected to the upper side and the lower side inside the hollow rod and a spring connecting the two solid rods.

As the optimization, the size and the draw-in groove looks adaptation of kelly, kelly and draw-in groove are in same horizontal direction, but the kelly joint in the inside of draw-in groove and then fix the inside at fixed chamber with the dust screen, kelly and draw-in groove are close to the outside one end of fuselage and all are provided with the hypotenuse of looks adaptation, can promote the kelly to remove in vertical direction when the draw-in groove horizontal direction removes.

The utility model has the advantages that: this concatenation treater of easy heat dissipation type opens the back through the drive fan and accelerates the inside and external circulation of air speed of fuselage, and then cools down to the inside of fuselage, can avoid the dust to get into the inside of fixed chamber and fuselage through the dust screen that sets up, and then avoids the dust to pile up and influence the heat dissipation, can make the telescopic link not be in with the slider joint through pressing the push rod, and then can dismantle the dust screen so that wash.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic view of the internal structure of the fixing cavity of the present invention;

fig. 3 is a schematic side view of the cross-sectional structure of the present invention.

In the figure: 1. a body; 2. a connecting port; 3. a fixed cavity; 4. a dust screen; 5. a fan; 6. a groove; 7. a slider; 8. a card slot; 9. a push rod; 10. a return spring; 11. a telescopic rod; 12. and (7) clamping the rod.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts all belong to the protection scope of the present invention.

Please refer to fig. 1-2, an easy heat dissipation type's concatenation treater, including fuselage 1, the front end fixed mounting of fuselage 1 has connector 2, the equal fixed chamber 3 of fixedly connected with in the left and right sides of fuselage 1, the one end that fixed chamber 3 is close to fuselage 1 has seted up the even through-hole in interval and has communicated with fuselage 1, make the inside air energy circulation of fixed chamber 3 and fuselage 1 so that dispel the heat to the inside of fuselage 1, the one end joint that fixed chamber 3 kept away from fuselage 1 has dust screen 4, the opening has been seted up to the one end that fixed chamber 3 kept away from fuselage 1, dust screen 4 fixed mounting is in the edge of opening, the outside face of dust screen 4 flushes with the surface in fixed chamber 3, the center that fixed chamber 3 is close to fuselage 1 one end rotates and is connected with fan 5, fan 5 electricity is connected with external power supply, fan 5 signal connection has the remote controller, can be convenient control the switch to fan 5, recess 6 has all been seted up at the inside upper and lower both ends in fixed chamber 3.

Please refer to fig. 2-3, the inside equal sliding connection in the left and right sides of recess 6 has slider 7, draw-in groove 8 has been seted up on the top of slider 7, the one end fixed mounting that two sliders 7 kept away from each other has push rod 9, push rod 9 runs through fixed chamber 3 and extends to the outside of fixed chamber 3, can promote push rod 9 externally and drive slider 7 and remove, the one end fixedly connected with reset spring 10 that two sliders 7 are close to each other, dust screen 4 is close to the inside one end fixed mounting of fixed chamber 3 has telescopic link 11, telescopic link 11 is by the hollow rod with dust screen 4 fixed connection, sliding connection is formed at the inside solid pole of the inside upper and lower both sides of hollow rod and the spring combination of connecting two solid poles, the equal fixed mounting in both ends has kelly 12 in the upper and lower both ends of telescopic link 11, the size and the draw-in groove 8 looks adaptation of kelly 12, kelly 12 and draw-in groove 8 are in same horizontal direction, kelly 12 can promote the hypotenuse that the draw-in that the vertical direction removed that dust screen 4 was fixed chamber 3 in draw-in the inside of draw-in groove 8, kelly 12 and draw-in the outside of fuselage 1.

When the dust-proof device is used, the remote controller is controlled to open the fan 5, the air circulation speed inside the machine body 1 and the air circulation speed outside the machine body 1 are accelerated through the rotation of the fan 5, further, the cooling speed inside the machine body 1 is accelerated, dust outside the surface can effectively enter the inside of the fixed cavity 3 through the dust-proof net 4 clamped inside the fixed cavity 3, further, the problem that the heat dissipation speed of the electronic component inside the machine body 1 is influenced due to the fact that dust is accumulated on the surface of the electronic component is avoided, when a large amount of dust needs to be cleaned, the two push rods 9 are pressed towards the inside of the machine body 1, the push rods 9 push the clamping rods 12 to move upwards, the clamping rods 12 are not limited with the push rods 9, at the moment, the telescopic rods 11 fixedly connected with the clamping rods 12 are not limited by the sliding blocks 7, therefore, the dust-proof net 4 fixedly connected with the telescopic rods 11 is not limited, and therefore the dust-proof net 4 can be taken out and cleaned.

To sum up, this concatenation treater of easy heat dissipation type, the inside and external circulation of air speed of fuselage 1 after drive fan 5 opens, and then cools down to the inside of fuselage 1, can avoid the dust to get into the inside of fixed chamber 3 and fuselage 1 through the dust screen 4 that sets up, and then avoids the dust to pile up and influence the heat dissipation, can make telescopic link 11 not with slider 7 joint through pressing push rod 9, and then can dismantle dust screen 4 so that wash.

In the description of the present invention, unless expressly stated or limited otherwise, the terms "disposed," "mounted," "connected," and "fixed" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral part; can be mechanically or electrically connected; they may be directly connected or indirectly connected through intervening media, or may be connected through the use of two elements or the interaction of two elements. The specific meaning of the above terms in the present invention can be understood as a specific case by those skilled in the art.

The utility model discloses the standard parts that use all can purchase from the market, and dysmorphism piece all can be customized according to the record of the description with the drawing.

Above, only be the embodiment of the preferred of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the design of the present invention, equivalent replacement or change should be included in the protection scope of the present invention.

Claims (7)

1. The utility model provides a concatenation treater of easy heat dissipation type, includes fuselage (1), its characterized in that: the front end fixed mounting of fuselage (1) has connector (2), the equal fixedly connected with fixed chamber (3) in the left and right sides of fuselage (1), the one end joint that fuselage (1) was kept away from in fixed chamber (3) has dust screen (4), the center that fixed chamber (3) is close to fuselage (1) one end is rotated and is connected with fan (5), recess (6) have all been seted up at the upper and lower both ends of fixed chamber (3) inside, the equal sliding connection in the left and right sides of recess (6) inside has slider (7), draw-in groove (8) have been seted up on the top of slider (7), two the one end fixed mounting that slider (7) kept away from each other has push rod (9), two the one end fixedly connected with reset spring (10) that slider (7) are close to each other, dust screen (4) are close to the inside one end fixed mounting of fixed chamber (3) have telescopic link (11), the equal fixed mounting in upper and lower both ends of telescopic link (11) has kelly (12).

2. The splicing processor of claim 1, wherein the splicing processor comprises: and through holes with uniform intervals are formed in one end, close to the machine body (1), of the fixed cavity (3) and are communicated with the machine body (1).

3. The splicing processor of claim 1, wherein: an opening is formed in one end, far away from the machine body (1), of the fixed cavity (3), the dust screen (4) is fixedly installed at the edge of the opening, and the outer side face of the dust screen (4) is flush with the outer surface of the fixed cavity (3).

4. The splicing processor of claim 1, wherein: the fan (5) is electrically connected with an external power supply, and the fan (5) is connected with a remote controller in a signal mode.

5. The splicing processor of claim 1, wherein the splicing processor comprises: the push rod (9) penetrates through the fixing cavity (3) and extends to the outside of the fixing cavity (3).

6. The splicing processor of claim 1, wherein: the telescopic rod (11) is formed by combining a hollow rod fixedly connected with the dust screen (4), solid rods slidably connected to the upper side and the lower side inside the hollow rod and springs connecting the two solid rods.

7. The splicing processor of claim 1, wherein: the size and the draw-in groove (8) looks adaptation of kelly (12), kelly (12) and draw-in groove (8) are in same horizontal direction, kelly (12) and draw-in groove (8) are close to the outside one end of fuselage (1) and all are provided with the hypotenuse of looks adaptation.

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