Equipment cabin convenient to install

Abstract

The utility model discloses an equipment compartment convenient to install, and relates to the technical field of equipment compartments, the equipment compartment convenient to install comprises a machine body, an installation assembly is arranged on the machine body and an installation plate, the installation assembly comprises a worm, a grip is fixedly installed on the outer wall of the worm, a rotating rod is arranged on one side of the worm, a worm wheel is fixedly installed on the outer wall of the rotating rod, and a worm wheel is fixedly installed on the worm wheel. A worm is arranged on the handle, a worm gear is arranged on the worm, the worm is in meshed connection with the worm gear, a plurality of pull ropes are wound on the outer wall of the rotating rod, a first inserting rod is fixedly installed at the end, away from the rotating rod, of each pull rope, and a reset spring is arranged outside each first inserting rod. The pull rope is tightened, the first insertion rod is pulled to be separated from the equipment cabin body, taking-down maintenance is facilitated, after maintenance, the grip is loosened, and the reset spring pushes the first insertion rod to fix the equipment cabin body. The mounting assembly enables dismounting to be more convenient, and the working efficiency is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of equipment cabins, in particular to an equipment cabin that is easy to install. Background Art

[0002] The equipment compartment is a compartment dedicated to installing electronic equipment and providing a normal working environment for it. This compartment can be used in a variety of scenarios, such as aircraft, EMUs, base stations, substations, etc. The design of the equipment compartment usually takes into account factors such as equipment protection, installation convenience, maintainability, and optimization of the working environment.

[0003] In the existing technology, workers need to measure the space inside the fuselage, draw it through CAD, carve it with a sinker, splice it into the fuselage, and then fix it with epoxy resin. It takes 3 hours for epoxy resin to be completely fixed at room temperature. The above fixing equipment is too complicated, with too many steps and too long time. The equipment that can be installed is too single and cannot be replaced. Utility Model Content

[0004] The purpose of the utility model is to provide an equipment cabin that is easy to install, so as to solve the problems raised in the above background technology.

[0005] To solve the above technical problems, the utility model provides an equipment cabin that is easy to install, including a fuselage, and installation components are arranged on the fuselage and the mounting plate, and the installation component includes a worm, a handle is fixedly installed on the outer wall of the worm, a rotating rod is arranged on one side of the worm, a worm wheel is fixedly installed on the outer wall of the rotating rod, the worm and the worm wheel are meshingly connected, a plurality of pull ropes are wrapped around the outer wall of the rotating rod, a first plug rod is fixedly installed on the end of the pull rope away from the rotating rod, and a return spring is arranged on the outside of the first plug rod.

[0006] Furthermore, a second limit block is fixedly mounted on the outer wall of the first insertion rod, the return spring is fixedly mounted between the mounting plate and the second limit block, and the rotating rod is rotatably connected to the inner wall of the fuselage.

[0007] Furthermore, a support plate is fixedly mounted on the inner bottom wall of the fuselage, one end of the worm is rotatably connected to the support plate, and the other end is rotatably connected to the fuselage.

[0008] Furthermore, the handle and the support plate are both provided with a plurality of insertion holes, a second insertion rod is inserted into the insertion holes, and a first limiting block is fixedly mounted on one end of the second insertion rod away from the handle.

[0009] Furthermore, a mounting rope is fixedly mounted on one end of the second insertion rod away from the handle, and the other end of the mounting rope is fixedly mounted on the mounting plate.

[0010] Furthermore, one end of the first insertion rod away from the pull rope extends to the interior of the equipment compartment body.

[0011] Furthermore, two slide rails are fixedly mounted on the inner bottom wall of the fuselage, the slide rails are symmetrically arranged, and the equipment compartment body is slidably connected to the slide rails.

[0012] Furthermore, two magnets are fixedly mounted on the side wall of the fuselage, and the two magnets are symmetrically arranged.

[0013] Compared with the prior art, the beneficial effects of the utility model are:

[0014] 1. In the utility model, the staff rotates the handle, and through the meshing of the worm and the worm wheel, drives the rotating rod to rotate, tightens the pull rope and pulls the first plug rod away from the equipment cabin body, which is convenient for removal and maintenance. After maintenance, the handle is released, and the reset spring pushes the first plug rod to fix the equipment cabin body. The installation assembly makes disassembly and assembly more convenient and improves work efficiency.

[0015] 2. In the present invention, the material of the equipment cabin body is iron. When the equipment cabin body is pushed to the inside of the fuselage along the direction of the slide rail, the magnetic force of the magnet will adsorb the equipment cabin body, making the equipment cabin body more stable when installed on the fuselage, reducing the damage to the internal equipment of the equipment cabin body caused by shaking or vibration of the equipment cabin body. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 It is a schematic diagram of the internal structure of the utility model;

[0017] Figure 2 It is a schematic diagram of the connection structure between the fuselage and the magnet in the utility model;

[0018] Figure 3 for Figure 1 A magnified view of the structure at center A;

[0019] Figure 4 for Figure 1 A magnified view of the structure at point B.

[0020] In the figure: 1. fuselage;

[0021] 2. Installation assembly; 201. Handle; 202. Worm; 203. Worm wheel; 204. Rotating rod; 205. Pull rope; 206. First plug rod; 207. Return spring;

[0022] 3. Equipment compartment body; 4. Second plug rod; 5. Socket; 6. First limit block; 7. Installation rope; 8. Support plate; 9. Installation plate; 10. Second limit block; 11. Slide rail; 12. Magnet. DETAILED DESCRIPTION

[0023] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0024] See also Figure 1-Figure 4 , the utility model provides a technical solution:

[0025] See also Figure 1-Figure 4 As shown, an equipment cabin that is easy to install includes a fuselage 1, and an installation component 2 is arranged on the fuselage 1 and the installation plate 9, the installation component 2 includes a worm 202, a handle 201 is fixedly installed on the outer wall of the worm 202, a rotating rod 204 is arranged on one side of the worm 202, a worm wheel 203 is fixedly installed on the outer wall of the rotating rod 204, the worm 202 and the worm wheel 203 are meshingly connected, a plurality of pull ropes 205 are wound around the outer wall of the rotating rod 204, a first plug rod 206 is fixedly installed on the end of the pull rope 205 away from the rotating rod 204, and a return spring 207 is arranged on the outside of the first plug rod 206.

[0026] The staff holds and rotates the handle 201, and the handle 201 drives the worm 202 to rotate, and the worm 202 is meshed with the worm wheel 203. The handle 201 drives the rotating rod 204 to rotate through the worm 202 and the worm wheel 203. When the rotating rod 204 rotates, the pull rope 205 is wrapped around and tightened on the outer wall of the rotating rod 204. At the same time, the pull rope 205 pulls the first plug rod 206 to move in the direction of the rotating rod 204, and the return spring 207 is squeezed and compressed, and the first plug rod 206 is separated from the equipment compartment body 3. At this time, the equipment compartment body 3 can be removed from the fuselage 1 to replace or repair the equipment, and then the equipment compartment body 3 is placed in the interior of the fuselage 1, and the handle 201 is released. The elastic force of the return spring 207 will push the first plug rod 206 toward the equipment compartment body 3 to fix the equipment compartment body 3. The installation component 2 can make the installation and disassembly of the equipment compartment body 3 more convenient and quick, thereby improving work efficiency.

[0027] See also Figure 4 The outer wall of the first plug rod 206 is fixedly mounted with a second limit block 10 , the return spring 207 is fixedly mounted between the mounting plate 9 and the second limit block 10 , and the rotating rod 204 is rotatably connected to the inner wall of the fuselage 1 .

[0028] The second limit block 10 prevents the first insertion rod 206 from passing through the mounting plate 9 when being pulled by the pull rope 205, causing the first insertion rod 206 to move excessively and cannot be used a second time. If it is desired to be used a second time, manual adjustment is required.

[0029] See also Figure 3 A support plate 8 is fixedly installed on the inner bottom wall of the fuselage 1, one end of the worm 202 is rotatably connected to the support plate 8, and the other end is rotatably connected to the fuselage 1.

[0030] One end of the worm 202 is fixed by the support plate 8, and the other end is connected to the body 1. This double support structure can ensure that the worm 202 is more stable during rotation and reduce vibration and shaking.

[0031] See also Figure 3 A plurality of insertion holes 5 are provided on the handle 201 and the support plate 8 , and a second insertion rod 4 is inserted into the insertion hole 5 , and a first limiting block 6 is fixedly installed at one end of the second insertion rod 4 away from the handle 201 .

[0032] After the staff rotates the handle 201 to make the first rod 206 leave the equipment compartment body 3, the second rod 4 is inserted into the appropriate socket 5 to prevent the handle 201 from rotating under the drive of the return spring 207, thereby preventing the first rod 206 from entering the side wall of the equipment compartment body 3 again.

[0033] See also Figure 3 One end of the second insertion rod 4 away from the handle 201 is fixedly mounted with a mounting rope 7 , and the other end of the mounting rope 7 is fixedly mounted on the mounting plate 9 .

[0034] After taking out the second insertion rod 4 from the insertion hole 5, the second insertion rod 4 is relatively small and easily lost. The installation rope 7 prevents the second insertion rod 4 from being lost and allows for easy search when the second insertion rod 4 is to be used again.

[0035] See also Figure 1 One end of the first insertion rod 206 away from the pull rope 205 extends to the interior of the equipment compartment body 3.

[0036] The first plug rod 206 extends into the interior of the equipment compartment body 3 and can cooperate with the slot on the equipment compartment body 3 to achieve the fixing function. This enhances the closing stability of the equipment compartment and prevents accidental opening or loosening.

[0037] See also Figure 2 Two slide rails 11 are fixedly installed on the inner bottom wall of the fuselage 1. The slide rails 11 are symmetrically arranged, and the equipment compartment body 3 is slidably connected to the slide rails 11.

[0038] The symmetrically arranged slide rails 11 provide clear guidance for the equipment compartment body 3, ensuring that it can accurately move along the predetermined track during the sliding process. This can prevent the equipment compartment body 3 from being offset or misaligned during the sliding process, and ensure the alignment and accurate fit between the equipment compartment body 3 and the fuselage 1.

[0039] See also Figure 2Two magnets 12 are fixedly mounted on the side wall of the body 1, and the two magnets 12 are symmetrically arranged.

[0040] The material of the equipment compartment body 3 is iron. When the equipment compartment body 3 is pushed into the interior of the fuselage 1 along the direction of the slide rail 11, the magnetic force of the magnet 12 will adsorb the equipment compartment body 3, making the equipment compartment body 3 installed on the fuselage 1 more stable, reducing the damage to the internal equipment of the equipment compartment body 3 caused by shaking or vibration of the equipment compartment body 3.

[0041] Working principle: the staff holds and rotates the handle 201, the handle 201 drives the worm 202 to rotate, the worm 202 is meshed with the worm wheel 203, and the handle 201 drives the rotating rod 204 to rotate through the worm 202 and the worm wheel 203. When the rotating rod 204 rotates, the pull rope 205 is wrapped around and tightened on the outer wall of the rotating rod 204. At the same time, the pull rope 205 pulls the first plug rod 206 to move in the direction of the rotating rod 204, and the return spring 207 is squeezed and compressed, and the first plug rod 206 is separated from the equipment compartment body 3. At this time, the equipment compartment body 3 can be removed from the fuselage 1 to replace or repair the equipment, and then the equipment compartment body 3 is placed in the interior of the fuselage 1, and the handle 201 is released. The elastic force of the return spring 207 will push the first plug rod 206 toward the equipment compartment body 3 to fix the equipment compartment body 3. The installation component 2 can make the installation and disassembly of the equipment compartment body 3 more convenient and quick, thereby improving work efficiency.

[0042] The material of the equipment compartment body 3 is iron. When the equipment compartment body 3 is pushed into the interior of the fuselage 1 along the direction of the slide rail 11, the magnetic force of the magnet 12 will adsorb the equipment compartment body 3, making the equipment compartment body 3 installed on the fuselage 1 more stable, reducing the damage to the internal equipment of the equipment compartment body 3 caused by shaking or vibration of the equipment compartment body 3.

Claims

1. An equipment cabin that is easy to install, comprising a fuselage (1), characterized in that: The body (1) and the mounting plate (9) are provided with a mounting assembly (2), the mounting assembly (2) comprising a worm (202), a handle (201) being fixedly mounted on the outer wall of the worm (202), a rotating rod (204) being provided on one side of the worm (202), a worm wheel (203) being fixedly mounted on the outer wall of the rotating rod (204), the worm (202) and the worm wheel (203) being meshingly connected, a plurality of pull ropes (205) being wound around the outer wall of the rotating rod (204), a first plug rod (206) being fixedly mounted on one end of the pull rope (205) away from the rotating rod (204), and a return spring (207) being provided on the outside of the first plug rod (206).

2. The equipment cabin that is easy to install as claimed in claim 1, characterized in that: A second limit block (10) is fixedly mounted on the outer wall of the first insertion rod (206), the return spring (207) is fixedly mounted between the mounting plate (9) and the second limit block (10), and the rotating rod (204) is rotatably connected to the inner wall of the fuselage (1).

3. The equipment cabin that is easy to install as claimed in claim 1, characterized in that: A support plate (8) is fixedly mounted on the inner bottom wall of the machine body (1); one end of the worm (202) is rotatably connected to the support plate (8), and the other end is rotatably connected to the machine body (1).

4. The equipment cabin that is easy to install as claimed in claim 1, characterized in that: The handle (201) and the support plate (8) are both provided with a plurality of insertion holes (5), a second insertion rod (4) is inserted into the insertion hole (5), and a first limit block (6) is fixedly mounted on one end of the second insertion rod (4) away from the handle (201).

5. The equipment cabin that is easy to install as claimed in claim 4, characterized in that: A mounting rope (7) is fixedly mounted on one end of the second insertion rod (4) away from the handle (201), and the other end of the mounting rope (7) is fixedly mounted on the mounting plate (9).

6. The equipment cabin that is easy to install as claimed in claim 1, characterized in that: One end of the first insertion rod (206) away from the pull rope (205) extends to the interior of the equipment compartment body (3).

7. The equipment cabin that is easy to install as claimed in claim 6, characterized in that: Two slide rails (11) are fixedly mounted on the inner bottom wall of the fuselage (1), the slide rails (11) are symmetrically arranged, and the equipment cabin body (3) is slidably connected to the slide rails (11).

8. The equipment cabin that is easy to install as claimed in claim 1, characterized in that: Two magnets (12) are fixedly mounted on the side wall of the body (1), and the two magnets (12) are symmetrically arranged.

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