CN214755260U

CN214755260U - Comprehensive wiring device in comprehensive wiring system

Info

Publication number: CN214755260U
Application number: CN202120944210.1U
Authority: CN
Inventors: 胡亚林; 未胜利; 于晓奔
Original assignee: Hefei Jingxin Electronic Technology Co ltd
Current assignee: Hefei Jingxin Electronic Technology Co ltd
Priority date: 2021-05-06
Filing date: 2021-05-06
Publication date: 2021-11-16
Anticipated expiration: 2031-05-06

Abstract

The utility model relates to a comprehensive wiring system technical field just discloses a comprehensive wiring device among comprehensive wiring system, which comprises a bod, the forceful electric power opening has been seted up to the side of fuselage, the spout has been seted up to the side of fuselage, the side slidable mounting of spout has the stopper, the nut hole has been seted up to the side of stopper. The utility model discloses a, it slides from top to bottom in the spout to drive the slider through the handle, thereby make and hold the thing board and can carry out elevating movement, remove the stopper in the spout simultaneously, when holding the thing board and reaching the assigned position, and then make the stopper block the slider, put in the drier through the inside at the storage tank, thereby make the inside of fuselage can keep dry, can not be moist, and the exhaust hole makes the bottom of strong electric wire have the circulation of air, and then can not influenced by water when having reached the wiring, can effectually prevent that the electric wire from damaging, and can carry out the regulation of height to the electric wire, the mesh of the electric wire electric leakage condition can not appear.

Description

Comprehensive wiring device in comprehensive wiring system

Technical Field

The utility model relates to a comprehensive wiring system technical field specifically is a comprehensive wiring device among comprehensive wiring system.

Background

The comprehensive wiring system is a wiring system specially designed for complying with development requirements, for modern buildings, such as nerves in the body, a series of high-quality standard materials are adopted, voice, data, images and part of control signal systems are integrated by a unified transmission medium in a modularized combination mode, and are integrated in a standard wiring system through a unified planning design, so that three major subsystems of the modern building are organically connected, and a wiring device is required to be used for wiring work so as to perform better wiring.

Present wiring device is when laying wire, and the inside of fuselage is wet easily to lead to the power cord to meet water, and can not carry out the regulation of height to the power cord, and then lead to the power cord the condition of electric leakage to appear, and forceful electric power line and weak current line interfere with each other easily, lead to losing and disorderly of circuit signal, for this reason, the utility model provides a comprehensive wiring device among the comprehensive wiring system.

SUMMERY OF THE UTILITY MODEL

The utility model provides a not enough to prior art, the utility model provides a comprehensive wiring device among comprehensive wiring system possesses comprehensive wiring system and can not influenced by water when the wiring, can effectually prevent that the electric wire from damaging, can carry out the regulation of height to the electric wire, the condition of electric wire electric leakage can not appear, and the condition of interference can not appear between forceful electric power line and the light current line, can effectually prevent losing and disorderly advantage of circuit signal, has solved the problem of mentioning among the background art.

The utility model provides a following technical scheme: the utility model provides an integrated wiring device among integrated wiring system, includes the fuselage, the forceful electric power opening has been seted up to the side of fuselage, the spout has been seted up to the side of fuselage, the side slidable mounting of spout has the stopper, the nut hole has been seted up to the side of stopper, the inside slidable mounting of spout has the slider, the side welding of slider has the handle, the side welding of slider has the bracing piece, the last skin weld of bracing piece has the thing board of holding, the side welding of holding the thing board has the protective block, the upper surface of holding the thing board has seted up the exhaust hole, the inside of fuselage is provided with deposits the jar.

Preferably, the lower surface of the inside of the machine body is welded with a blocking plate, the side face of the blocking plate is provided with an anti-static film, the side face of the machine body is provided with a weak current opening, the lower surface of the inside of the machine body is provided with a storage tank, and the lower surface of the inside of the machine body is welded with a fixing box.

Preferably, the limiting block is arranged in a U shape, the upper surface area of the limiting block is smaller than that of the sliding block, a plurality of nut holes are uniformly arranged on the side face of the machine body, and the nut holes are not in contact with the sliding grooves.

Preferably, the support rod is arranged in an inverted triangle, the plane of the support rod is parallel to the lower surface of the object bearing plate, and the sliding grooves are respectively formed in the side face of the machine body and the side face of the blocking plate.

Preferably, the exhaust holes are a plurality of, and a plurality of exhaust holes are uniformly arranged on the upper surface of the object bearing plate, and the protection block is arranged in an arc shape.

Preferably, the storage tank has a plurality of, and a plurality of storage tank is in the inside align to grid setting of fuselage, a plurality of the inside of storage tank all is provided with the carbon powder.

Compared with the prior art, the utility model discloses possess following beneficial effect:

1. the comprehensive wiring device in the comprehensive wiring system drives the sliding block to slide up and down in the sliding groove through the handle, so that the object bearing plate can move up and down, the limiting block moves in the sliding groove, when the object bearing plate reaches a specified position, the limiting block is fixed with the side surface of the machine body through the nut hole, and the limiting block can block the sliding block, so that the sliding block cannot slide down, because the supporting rod is arranged in an inverted triangle, the object bearing plate cannot be in direct contact with the lower surface inside the machine body, a strong current wire penetrates into the machine body through the strong current opening, the abrasion of the strong current wire is reduced through the protective block, excessive damage cannot occur, through throwing the drying agent in the storage tank, the inside of the machine body can be kept dry all the time through the use of the exhaust holes, and the inside of the machine body is in a dry environment for a long time when wiring is achieved, the inside of effectual preventing is dampened, and can carry out the regulation of height to the electric wire, the mesh that the electric wire electric leakage condition can not appear.

2. This synthesize integrated wiring device among wiring system, divide into two parts through the inside of barrier plate with the fuselage, one is the forceful electric power line space, another is the light current line space, thereby can tentatively prevent mutual interference between the electric current, because the side of barrier plate is provided with the antistatic film, and then can further prevent static mutual interference, penetrate the fuselage through the light current opening with the light current line in, pass fixed box simultaneously, because fixed box is rectangle cavity setting, thereby make the light current not have the inside of large tracts of land at the fuselage, the inside carbon dust of storage tank can be electrolyzed simultaneously, and then can absorb free electron, thereby reached and prevented strong electric wire and light current case mutual interference, prevent circuit signal loss and disorderly purpose.

Drawings

FIG. 1 is a sectional view of the overall structure of the present invention;

FIG. 2 is a side sectional view of the fuselage structure of the present invention;

fig. 3 is an enlarged schematic view of the structure at a position a of the present invention.

In the figure: 1. a body; 2. a strong current opening; 3. a chute; 4. a limiting block; 5. a nut hole; 6. a slider; 7. a handle; 8. a support bar; 9. an object bearing plate; 10. a protection block; 11. an exhaust hole; 12. a storage tank; 13. a blocking plate; 14. an antistatic film; 15. a weak current opening; 16. a storage tank; 17. and (5) fixing the box.

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 work belong to the protection scope of the present invention.

Referring to fig. 1-3, an integrated wiring device in an integrated wiring system comprises a body 1, a strong current opening 2 is formed on the side surface of the body 1, a sliding groove 3 is formed on the side surface of the body 1, a limiting block 4 is slidably mounted on the side surface of the sliding groove 3, a nut hole 5 is formed on the side surface of the limiting block 4, the limiting block 4 is in a U-shaped arrangement, the upper surface area of the limiting block 4 is smaller than the upper surface area of the sliding block 6, a plurality of nut holes 5 are uniformly arranged on the side surface of the body 1, the nut holes 5 are not in contact with the sliding groove 3, the sliding block 6 is slidably mounted inside the sliding groove 3, a handle 7 is welded on the side surface of the sliding block 6, a support rod 8 is welded on the side surface of the support rod 8, an object bearing plate 9 is welded on the upper surface of the object bearing plate 9, a protection block 10 is welded on the side surface of the object bearing plate 9, an exhaust hole 11 is formed on the upper surface of the object bearing plate 9, and a plurality of exhaust holes 11 are formed, a plurality of vent holes 11 are uniformly arranged on the upper surface of the object bearing plate 9, a protective block 10 is arranged in an arc shape, a storage tank 12 is arranged in the machine body 1, a barrier plate 13 is welded on the lower surface in the machine body 1, a support rod 8 is arranged in an inverted triangle, the plane of the support rod 8 is parallel to the lower surface of the object bearing plate 9, sliding chutes 3 are respectively arranged on the side surface of the machine body 1 and the side surface of the barrier plate 13, an antistatic film 14 is arranged on the side surface of the barrier plate 13, a weak current opening 15 is arranged on the side surface of the machine body 1, a plurality of storage tanks 16 are arranged on the lower surface in the machine body 1, the plurality of storage tanks 16 are uniformly arranged in the machine body 1, carbon powder is arranged in the plurality of storage tanks 16, a fixing box 17 is welded on the lower surface in the machine body 1, a slider 6 is driven by a handle 7 to slide up and down in the sliding chute 3, thereby enabling the object bearing plate 9 to carry out lifting motion, simultaneously moving the limit block 4 in the sliding groove 3, when the object bearing plate 9 reaches a designated position, fixing the limit block 4 with the side surface of the machine body 1 through the nut hole 5, further enabling the limit block 4 to block the sliding block 6, further enabling the sliding block 6 not to slide downwards, because the support rod 8 is arranged in an inverted triangle, further enabling the object bearing plate 9 not to be in direct contact with the lower surface inside the machine body 1, enabling a strong current wire to penetrate into the machine body 1 through the strong current opening 2, reducing the abrasion of the strong current wire through the protection block 10, avoiding excessive damage, and enabling the interior of the machine body 1 to keep dry through throwing a drying agent in the storage tank 12, avoiding moisture, and enabling the bottom of the strong current wire to have air circulation through the exhaust hole 11, further avoiding water influence when wiring is achieved, can effectively prevent the electric wire from being damaged, can adjust the height of the electric wire, can not generate the electric leakage of the electric wire, the interior of the body 1 is divided into two parts, one is a strong current space and the other is a weak current space, by the barrier plate 13, so that mutual interference between currents can be prevented preliminarily, because the side of the blocking plate 13 is provided with the anti-static film 14, the mutual interference of static electricity can be further prevented, the weak current is passed through the weak current opening 15 into the body 1, and simultaneously passed through the fixing box 17, because the fixing box 17 is arranged in a rectangular hollow manner, the weak wire is not arranged in the machine body 1 in a large area, and carbon powder in the storage tank 16 can be electrolyzed, and then can absorb free electron to reach and prevented that strong wire and weak current case fox from interfering, prevent that the circuit limit number from losing and disorderly purpose.

The theory of operation, penetrate the inside of fuselage 1 through forceful electric power opening 2 with the forceful electric power line, the forceful electric power line is placed in the top that holds thing board 9, the bottom of bracing piece 8 and the inside lower surface contact of fuselage 1, the forceful electric power line and the inside lower surface contactless of fuselage 1, drive slider 6 through handle 7 and remove in spout 3, slider 6 drives and holds thing board 9 and carries out the elevating movement, stopper 4 removes in spout 3, fix through nut hole 5, the inside drier of holding vessel 12 is dry to fuselage 1 inside, penetrate the inside of fuselage 1 through weak current opening 15 with the weak current line, the weak current line passes fixed box 17, antistatic film 14 prevents that static from passing barrier plate 13, the carbon powder in the inside storing vessel 16 absorbs the ionization in the air can.

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 invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. An integrated wiring device in an integrated wiring system, characterized in that: including fuselage (1), forceful electric power opening (2) have been seted up to the side of fuselage (1), spout (3) have been seted up to the side of fuselage (1), the side slidable mounting of spout (3) has stopper (4), nut hole (5) have been seted up to the side of stopper (4), the inside slidable mounting of spout (3) has slider (6), the side welding of slider (6) has handle (7), the side welding of slider (6) has bracing piece (8), the last surface welding of bracing piece (8) has and holds thing board (9), the side welding that holds thing board (9) has protection piece (10), exhaust hole (11) have been seted up to the upper surface that holds thing board (9), the inside of fuselage (1) is provided with deposits jar (12).

2. The integrated wiring device in an integrated wiring system according to claim 1, wherein: the anti-static electricity machine is characterized in that a blocking plate (13) is welded on the lower surface of the interior of the machine body (1), an anti-static film (14) is arranged on the side surface of the blocking plate (13), a weak electricity opening (15) is formed in the side surface of the machine body (1), a storage tank (16) is arranged on the lower surface of the interior of the machine body (1), and a fixing box (17) is welded on the lower surface of the interior of the machine body (1).

3. The integrated wiring device in an integrated wiring system according to claim 1, wherein: stopper (4) are the setting of U type, and the upper surface area of stopper (4) is less than the upper surface area of slider (6), a plurality of nut hole (5) have been seted up to the side align to grid of fuselage (1), and a plurality of nut hole (5) and spout (3) contactless.

4. The integrated wiring device in an integrated wiring system according to claim 1, wherein: the bracing piece (8) are the reverse triangle setting, and the plane of bracing piece (8) is parallel arrangement with the lower surface that holds thing board (9), spout (3) are seted up respectively in the side of fuselage (1) and the side of barrier plate (13).

5. The integrated wiring device in an integrated wiring system according to claim 1, wherein: the exhaust holes (11) are provided with a plurality of exhaust holes (11) which are uniformly arranged on the upper surface of the object bearing plate (9), and the protection block (10) is arranged in an arc shape.

6. The integrated wiring device in an integrated wiring system according to claim 2, characterized in that: the storage tank (16) is provided with a plurality of storage tanks (16) which are uniformly arranged in the machine body (1), and the storage tanks (16) are all provided with carbon powder.