CN216670653U - Computer interface structure - Google Patents

Computer interface structure Download PDF

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Publication number
CN216670653U
CN216670653U CN202123330679.5U CN202123330679U CN216670653U CN 216670653 U CN216670653 U CN 216670653U CN 202123330679 U CN202123330679 U CN 202123330679U CN 216670653 U CN216670653 U CN 216670653U
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China
Prior art keywords
fuselage
interface
computer interface
closing plate
fixedly connected
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CN202123330679.5U
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Chinese (zh)
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吴泉胜
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Nanjing Chengensi Information Technology Co ltd
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Nanjing Chengensi Information Technology Co ltd
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02DCLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
    • Y02D10/00Energy efficient computing, e.g. low power processors, power management or thermal management

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Abstract

The utility model discloses a computer interface structure, which comprises a machine body, wherein a reset mechanism is arranged in the machine body, a fixing mechanism is arranged on the reset mechanism, the fixing mechanism comprises four connecting rods, one end of each connecting rod, which is close to the center of the machine body, is hinged with a fixed block through a hinge shaft, a sealing plate is fixedly connected between the two fixed blocks at the upper end and between the two fixed blocks at the lower end, and the interface can be sealed through the arrangement of the two sealing plates, so that external dust is prevented from entering the interface when the computer interface structure is not used, the interface can be prevented from being damaged by external accidental touch of the interface, the service life of the interface is prolonged, the plug can be clamped by the two sealing plates through the arrangement of compression springs on the two sealing plates when the plug is plugged at the interface, and therefore, workers are prevented from mistakenly touching the plug data line, the plug wire head is pulled out, thereby improving the practicability of the computer.

Description

Computer interface structure
Technical Field
The utility model belongs to the technical field of computers, and particularly relates to a computer interface structure.
Background
The computer has a strong calculation and analysis function, is applied to various industries, is a necessary tool especially for offices, can accelerate office efficiency, for example, for personnel engaged in design, drawings can be drawn through computer design, the computer mainly comprises a host and a display screen, a plurality of interfaces are arranged on the host, and the host and the display screen are mainly connected through a plurality of data lines connected through the interfaces.
However, when the computer is used, a worker easily touches the data line by mistake, so that a plug on the data line is separated from the interface, data loss is caused, the use of the computer is influenced, and when the computer is not used, the interface is in an exposed state, dust is easily accumulated, the interface is also easily damaged by the touch of an external object, and the service life of the interface is influenced.
SUMMERY OF THE UTILITY MODEL
The present invention is directed to a computer interface structure to solve the above problems.
In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides a computer interface structure, includes the fuselage, the inside of fuselage is provided with canceling release mechanical system, the last fixed establishment that is provided with of canceling release mechanical system, fixed establishment includes the connecting rod, the connecting rod is provided with four, four the one end that the connecting rod is close to the fuselage center all articulates through the hinge has the fixed block, two upper ends between the fixed block and two lower extremes equal fixedly connected with closing plate between the fixed block, upper end both ends and lower extreme about the closing plate upper surface the equal fixedly connected with pressure spring in both ends, four about the closing plate lower surface the one end that pressure spring kept away from the fuselage all with the inside fixed connection of fuselage.
Preferably, canceling release mechanical system includes the dead lever, the dead lever bilateral symmetry is provided with two, two the equal fixed mounting of dead lever is in the inside of fuselage, two the dead lever is kept away from the one end surface of closing plate and all is equipped with the slider, two the equal fixedly connected with reset spring of one end that the slider is close to the closing plate, two reset spring overlaps respectively to be established two the surface of dead lever, two reset spring is close to the one end of closing plate all with the inside fixed connection of fuselage.
Preferably, the installation cavity has been seted up to the inside of fuselage, canceling release mechanical system and fixed establishment all set up the inside at the installation cavity.
Preferably, the front surfaces of the two sliding blocks are fixedly connected with moving blocks, and the front surfaces of the two moving blocks are provided with anti-skid grains.
Preferably, the front end of the body is provided with two moving grooves, the two moving grooves are arranged in bilateral symmetry, and the front ends of the two moving blocks penetrate through the two moving grooves respectively and extend to the front end of the body.
Preferably, the lower surface of the upper end sealing plate and the upper surface of the lower end sealing plate are both fixedly provided with rubber pads.
Preferably, the inside fixed mounting of fuselage rear end has the interface, the interface sets up two just the rear of sealing plate.
Compared with the prior art, the utility model has the beneficial effects that:
(1) this computer interface structure, setting through two closing plates, can seal the kneck, thereby avoid external dust to get into the kneck when not using, also can avoid external mistake to touch the interface, cause the damage to the interface, the life of interface has been improved, setting through pressure spring on two closing plates, peg graft when the socket department at the plug, two closing plates can carry out the centre gripping to the plug, thereby the stability of plug has been improved, the staff mistake has been avoided touching plug data line, lead to the plug to be extracted, influence the use of computer, thereby the practicality of computer has been improved.
(2) This computer interface structure, through the canceling release mechanical system who sets up, when not moving the movable block, canceling release mechanical system can further drive two closing plates and move in opposite directions, has improved the centre gripping effect of closing plate then, has strengthened the stability of plug wire head department, and the practicality is higher.
Drawings
FIG. 1 is a schematic perspective view of a fixing mechanism according to the present invention;
FIG. 2 is a front cross-sectional view of the present invention;
FIG. 3 is a left side elevation view of the present invention;
fig. 4 is a top sectional view of the present invention.
In the figure: 1. a body; 2. a reset mechanism; 201. fixing the rod; 202. a slider; 203. a return spring; 3. a fixing mechanism; 301. a connecting rod; 302. a fixed block; 303. a sealing plate; 304. a compression spring; 4. a mounting cavity; 5. a rubber pad; 6. a moving block; 7. a moving groove; 8. and (4) an interface.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1 to 4, the present invention provides a computer interface structure, which includes a main body 1, a reset mechanism 2 is disposed inside the main body 1, a fixing mechanism 3 is disposed on the reset mechanism 2, the fixing mechanism 3 includes four connecting rods 301, the four connecting rods 301 are hinged to fixed blocks 302 through hinge shafts at ends of the four connecting rods 301 close to the center of the main body 1, sealing plates 303 are fixedly connected between the two upper end fixed blocks 302 and between the two lower end fixed blocks 302, compression springs 304 are fixedly connected to left and right ends of the upper surface of the upper end sealing plate 303 and left and right ends of the lower surface of the lower end sealing plate 303, and ends of the four compression springs 304 far from the main body 1 are fixedly connected to the inside of the main body 1.
In this embodiment, preferably, the reset mechanism 2 includes two fixed rods 201, two fixed rods 201 are symmetrically arranged on the left and right sides, two fixed rods 201 are both fixedly installed inside the machine body 1, the surfaces of the ends of the two fixed rods 201 away from the sealing plate 303 are both sleeved with the sliding blocks 202, the ends of the two sliding blocks 202 close to the sealing plate 303 are both fixedly connected with the reset springs 203, the two reset springs 203 are respectively sleeved on the surfaces of the two fixed rods 201, the ends of the two reset springs 203 close to the sealing plate 303 are both fixedly connected with the inside of the machine body 1, the two sliding blocks 202 are moved towards each other, so that the reset springs 203 are compressed, and the connecting rod 301 is driven to move at the same time, so that the connecting rod 301 is buffered to be in a vertical state, and then the two sealing plates 303 are driven to move away from each other, so that the plug wire can be inserted into the machine body 1, when the two sliding blocks 202 are not subjected to the force exerted by a worker, two sliders 202 receive reset spring 203's power back of the body to move mutually then make two closing plates 303 remove in opposite directions, and then fix the plug, improved the stability of plug, when avoiding the plug to produce the mistake and touch, lead to the plug to be extracted, influence the use of computer to the practicality of computer has been improved.
In this embodiment, preferred, installation cavity 4 has been seted up to the inside of fuselage 1, and canceling release mechanical system 2 and fixed establishment 3 all set up in the inside of installation cavity 4, and the setting of installation cavity 4 provides the activity space for canceling release mechanical system 2 and fixed establishment 3, the use of fuselage 1 of being convenient for then.
In this embodiment, preferably, the equal fixedly connected with movable block 6 in front of two sliders 202, the front of two movable blocks 6 all is provided with anti-skidding line, and the setting of movable block 6 is convenient for the staff to drive slider 202 through movable block 6 and remove, and then the slider 202 of being convenient for drives the work of fixed establishment 3, and the frictional force on movable block 6 surface has been increased in the setting of anti-skidding line, takes place the phenomenon of skidding when avoiding the staff to use movable block 6, has improved the practicality when movable block 6 uses.
In this embodiment, preferably, the front end of the body 1 is provided with two moving grooves 7, the two moving grooves 7 are arranged in bilateral symmetry, the front ends of the two moving blocks 6 respectively penetrate through the two moving grooves 7 and extend to the front end of the body 1, and the moving grooves 7 provide a moving space for the moving blocks 6, so that the moving blocks 6 can smoothly drive the sliding block 202 to move horizontally.
In this embodiment, preferably, the rubber pads 5 are fixedly mounted on the lower surface of the upper end sealing plate 303 and the upper surface of the lower end sealing plate 303, and the arrangement of the rubber pads 5 can buffer the extrusion force of the sealing plate 303 to the plug, so as to avoid the damage to the plug caused by the excessive extrusion force of the sealing plate 303, thereby improving the practicability of the machine body 1.
In this embodiment, preferably, the interface 8 is fixedly mounted inside the rear end of the body 1, the interface 8 is arranged right behind the two sealing plates 303, and the plug wire can be smoothly plugged into the interface 8 after the sealing plates 303 are opened, so that subsequent use is facilitated.
The working principle and the using process of the utility model are as follows: when the device uses, at first with two movable blocks 6 remove in opposite directions, thereby drive two sliders 202 and remove in opposite directions, make reset spring 203 compress, drive connecting rod 301 simultaneously and remove, make connecting rod 301 buffering tend to the vertical state, then drive two closing plate 303 and remove back to back, and then make the plug connector insert on fuselage 1's the interface 8, later loosen two movable blocks 6, when two movable blocks 6 do not receive external force, two movable blocks 6 and two sliders 202 receive reset spring 203's power and remove back to back, then make two closing plate 303 remove in opposite directions, and then make two closing plate 303 carry out the centre gripping to the upper and lower both ends of plug connector, the stability of plug connector has been improved, the subsequent use of the computer of being convenient for.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims (7)

1. A computer interface structure, comprising a body (1), characterized in that: the inside of fuselage (1) is provided with canceling release mechanical system (2), be provided with fixed establishment (3) on canceling release mechanical system (2), fixed establishment (3) are including connecting rod (301), connecting rod (301) are provided with four, four connecting rod (301) are close to the one end at fuselage (1) center and all articulate through the hinge and have fixed block (302), two upper ends between fixed block (302) and two lower extremes equal fixedly connected with closing plate (303) between fixed block (302), upper end both ends and lower extreme about closing plate (303) upper surface the equal fixedly connected with pressure spring (304) in both ends about closing plate (303) lower surface, four the inside fixed connection of the one end that fuselage (1) was kept away from in pressure spring (304) all with fuselage (1).
2. A computer interface architecture according to claim 1, wherein: canceling release mechanical system (2) are including dead lever (201), dead lever (201) bilateral symmetry is provided with two, two the inside at fuselage (1) of the equal fixed mounting of dead lever (201), two the one end surface that closing plate (303) were kept away from in dead lever (201) all overlaps and is equipped with slider (202), two the equal fixedly connected with reset spring (203) of one end that slider (202) are close to closing plate (303), two reset spring (203) overlap respectively and establish two the surface of dead lever (201), two reset spring (203) are close to the one end of closing plate (303) all with the inside fixed connection of fuselage (1).
3. A computer interface architecture according to claim 1, wherein: installation cavity (4) have been seted up to the inside of fuselage (1), canceling release mechanical system (2) and fixed establishment (3) all set up the inside in installation cavity (4).
4. A computer interface architecture according to claim 2, wherein: the front surfaces of the two sliding blocks (202) are fixedly connected with moving blocks (6), and the front surfaces of the two moving blocks (6) are provided with anti-skidding threads.
5. A computer interface architecture according to claim 4, wherein: the front end of the machine body (1) is provided with two moving grooves (7), the two moving grooves (7) are arranged in a bilateral symmetry mode, and the front ends of the two moving blocks (6) penetrate through the two moving grooves (7) respectively and extend to the front end of the machine body (1).
6. A computer interface architecture according to claim 1, wherein: the upper end the lower surface of sealing plate (303) and the lower extreme the upper surface of sealing plate (303) all fixed mounting have rubber pad (5).
7. A computer interface architecture according to claim 1, wherein: the inside fixed mounting of fuselage (1) rear end has interface (8), interface (8) set up two sealing plate (303) are just behind.
CN202123330679.5U 2021-12-28 2021-12-28 Computer interface structure Active CN216670653U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202123330679.5U CN216670653U (en) 2021-12-28 2021-12-28 Computer interface structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202123330679.5U CN216670653U (en) 2021-12-28 2021-12-28 Computer interface structure

Publications (1)

Publication Number Publication Date
CN216670653U true CN216670653U (en) 2022-06-03

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ID=81798345

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202123330679.5U Active CN216670653U (en) 2021-12-28 2021-12-28 Computer interface structure

Country Status (1)

Country Link
CN (1) CN216670653U (en)

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