Engineering mechanical equipment anti-collision early warning device mounting mechanism convenient to disassemble and assemble

Abstract

The utility model relates to the technical field of anti-collision early warning of mechanical equipment, in particular to an anti-collision early warning device mounting mechanism for engineering mechanical equipment, which is convenient to disassemble and assemble, and solves the technical problems that when the engineering mechanical equipment is used, an anti-collision early warning device needs to be mounted at a visual blind area of the equipment; however, most engineering mechanical equipment anti-collision early warning device installation mechanisms can only fixedly install early warning aircrafts of the same model and size, and are inconvenient to disassemble and assemble, so that the use flexibility of the devices is influenced. According to the technical scheme, the engineering mechanical equipment anti-collision early warning device mounting mechanism convenient to disassemble and assemble comprises a mounting assembly, an adjusting assembly, an early warning assembly and a fixing assembly; compared with a traditional installation mechanism for the anti-collision early warning device of the engineering mechanical equipment, the anti-collision early warning device can be stably fixed to the equipment in an adjustable clamping and fixing mode according to the actual size of the device, the operation of installing the device is optimized, and the practical value of the device is enhanced.

Description

Technical Field

[0001] The utility model relates to the technical field of anti-collision warning for mechanical equipment, and in particular to an installation mechanism for an anti-collision warning device for engineering mechanical equipment which is convenient to assemble and disassemble. Background Art

[0002] Engineering machinery and equipment refers to various mechanized equipment used in the fields of construction, civil engineering, mining, road construction, water conservancy projects, etc. The main functions of these equipment are to improve work efficiency, reduce labor intensity, and ensure project quality and safety. Engineering machinery and equipment are divided into many categories according to specific engineering projects, working environments, construction requirements, etc. The operating production environment of such equipment often hides many dangerous factors, and the equipment may also have some blind spots. Therefore, it is necessary to add anti-collision warning devices to the equipment, which are mainly used to improve the safety of the construction site. It can monitor and warn of potential collision risks, thereby reducing the possibility of accidents. The application of anti-collision warning devices can significantly improve the safety of the construction site and reduce human errors and equipment damage. However, most engineering machinery and equipment anti-collision warning device installation mechanisms are inconvenient to disassemble, replace and release the collision machine. Utility Model Content

[0003] In order to overcome the installation mechanism of the anti-collision warning device of most engineering machinery equipment, most of them can only fix the early warning machine of the same model and size, and it is inconvenient to disassemble and assemble, which affects the flexibility of the device.

[0004] The technical solution of the utility model is: an installation mechanism for an anti-collision warning device of engineering machinery equipment which is easy to disassemble and assemble, comprising a base, a mounting assembly, a warning assembly, a first adjustment assembly, a first fixing assembly, a second adjustment assembly and a second fixing assembly; a mounting assembly is arranged on the bottom surface of the base, a warning assembly is arranged on one side of the base, a first adjustment assembly is arranged on one side of the base, a first fixing assembly is arranged on one side of the first adjustment assembly, two groups of the first fixing assembly are arranged, a second adjustment assembly is also arranged on one side of the base, two groups of the second adjustment assembly are arranged, and a second fixing assembly is arranged on one side of the second adjustment assembly.

[0005] Preferably, the base is installed and fixed at a specified position of the mechanical equipment by setting an installation component, the first adjustment component is fixed by the base, the first adjustment component is used to drive the first fixed component to move, the first fixed component is used to clamp and fix the warning component from the vertical direction, and then, the second adjustment component is used to drive the second fixed component to move, the second fixed component is used to clamp and fix the warning component from the horizontal direction, and the warning component is used to perform anti-collision warning operations, thereby achieving stable fixation of the device to the equipment according to its actual size, optimizing the operation effect of the installation device, and enhancing the practical value of the device.

[0006] Preferably, the mounting assembly includes a mounting plate, mounting holes and bolts; a mounting plate is provided on the bottom surface of the base, mounting holes are provided on one side of the mounting plate, multiple groups of mounting holes are provided, bolts are provided on the inner sides of the mounting holes, and the bolts and the mounting holes are threadedly connected to each other; the base is connected and fixed by the mounting plate, the mounting holes are used to clearly define the bolt installation and fixing position, and the bolts are rotated in the mounting holes, thereby achieving the effect of stably fixing the mounting plate to the specified installation position of the mechanical equipment.

[0007] Preferably, the early warning component includes an early warning aircraft body, a positioning groove and a positioning column; the early warning aircraft body is arranged on one side of the base, a positioning groove is opened on the bottom surface of the early warning aircraft body, and there are two groups of positioning grooves; a positioning column is arranged on one side of the base, and there are two groups of positioning columns, and the positioning column and the positioning groove are interlocked with each other; the early warning aircraft body is used to perform specific anti-collision warning operations, and the positioning column is embedded in the positioning groove, so as to clarify the installation and placement position of the early warning aircraft body.

[0008] Preferably, the first adjustment component includes a bidirectional adjustment screw and a first motor; a bidirectional adjustment screw is arranged on one side of the base, and a first motor is arranged on the other side of the base, and the output end of the first motor is interconnected with the bidirectional adjustment screw; the bidirectional adjustment screw is driven to rotate by the first motor, and the bidirectional adjustment screw is rotated to flexibly adjust the spacing between the two groups of first fixed components.

[0009] Preferably, the first fixing component includes a first fixing block, a first fixing column and a first fixing groove; a first fixing block is arranged on the outside of the two-way adjustment screw rod, the first fixing block is arranged in two groups, a first fixing column is arranged on one side of the first fixing block, a first fixing groove is opened on one side of the early warning aircraft body, the first fixing groove is opened in two groups, and the first fixing column and the first fixing groove are interlocked with each other; the first fixing column is connected and fixed by the first fixing block, and the first fixing column is embedded in the first fixing groove, so that it is installed and fixed in the vertical direction according to the actual size of the early warning aircraft body.

[0010] Preferably, the second adjusting component includes a second screw rod and a second motor; a second screw rod is arranged on one side of the base, and two groups of second screw rods are arranged; a second motor is arranged on the other side of the base, and the output end of the second motor is connected to the second screw rod; the second screw rod is driven to rotate by the second motor, and the spacing between the two groups of second fixed components can be flexibly adjusted by rotating the second screw rod.

[0011] Preferably, the second fixing assembly includes a second fixing block, a second fixing column and a second fixing groove; a second fixing block is arranged on the outside of the second screw rod, a second fixing column is arranged on one side of the second fixing block, a second fixing groove is opened on one side of the early warning aircraft body, two groups of second fixing grooves are opened, and the second fixing column and the second fixing groove are interlocked with each other; the second fixing column is connected and fixed by the second fixing block, and the second fixing column is embedded in the second fixing groove, so that it is installed and fixed in the horizontal direction according to the actual size of the early warning aircraft body.

[0012] Beneficial effects of the utility model:

[0013] 1. Compared with the traditional installation mechanism of anti-collision warning device for engineering machinery, most of them use bolts to fix the warning device to the specified position of the equipment, which can only fix the warning machine of the same model and size, and it is inconvenient to disassemble and assemble. Through the adjustable clamping and fixing method, it can be stably fixed to the equipment according to the actual size of the device, optimize the operation of the installation device, and enhance the practical value of the device;

[0014] 2. When fixing the device, place the main body of the early warning machine on the surface of the base, embed the positioning column into the positioning groove, and drive the bidirectional adjustment screw rod to rotate by the first motor to adjust the distance between the two sets of first fixing blocks, and embed the first fixing column into the first fixing groove. Then, drive the second screw rod to rotate by the second motor to adjust the distance between the two sets of second fixing blocks, and embed the second fixing column into the second fixing groove, so as to solve the problem that most of the installation mechanisms of the anti-collision early warning device are inconvenient to disassemble and replace the anti-collision machine, and enhance the flexibility of the device;

[0015] 3. Before installing the main body of the early warning machine, clarify the actual warning requirement position of the mechanical equipment, place the mounting plate at the specified installation position of the equipment, then align the bolt with the mounting hole, turn the bolt in the mounting hole, and turn the bolt to stably install and fix the mounting plate at the corresponding position of the equipment, so as to stably and fixedly install the base at the specified early warning point. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 Shown is a three-dimensional structural schematic diagram of an installation mechanism of an anti-collision warning device for engineering machinery equipment that is easy to disassemble and assemble according to the utility model;

[0017] Figure 2 Shown is a three-dimensional structural diagram of an installation component of an installation mechanism of an anti-collision warning device for engineering machinery and equipment that is easy to disassemble and assemble according to the utility model;

[0018] Figure 3 Shown is a three-dimensional structural schematic diagram of a warning component of an installation mechanism of an anti-collision warning device for engineering machinery and equipment that is easy to disassemble and assemble according to the utility model;

[0019] Figure 4 Shown is a schematic diagram of the three-dimensional structure of the second fixing component of the installation mechanism of the anti-collision warning device for engineering machinery equipment which is easy to disassemble and assemble according to the utility model.

[0020] Explanation of the accompanying drawings: 1. base; 2. mounting assembly; 3. early warning assembly; 4. first adjustment assembly; 5. first fixing assembly; 6. second adjustment assembly; 7. second fixing assembly; 201. mounting plate; 202. mounting hole; 203. bolt; 301. early warning aircraft body; 302. positioning groove; 303. positioning column; 401. bidirectional adjustment screw rod; 402. first motor; 501. first fixing block; 502. first fixing column; 503. first fixing groove; 601. second screw rod; 602. second motor; 701. second fixing block; 702. second fixing column; 703. second fixing groove. DETAILED DESCRIPTION

[0021] The utility model is further described below in conjunction with the accompanying drawings and embodiments.

[0022] See also Figure 1 The utility model provides an embodiment: an installation mechanism for an anti-collision warning device of engineering machinery equipment with convenient disassembly and assembly, comprising a base 1, a mounting component 2, a warning component 3, a first adjustment component 4, a first fixing component 5, a second adjustment component 6 and a second fixing component 7; the bottom surface of the base 1 is provided with the mounting component 2, one side of the base 1 is provided with the warning component 3, one side of the base 1 is provided with the first adjustment component 4, one side of the first adjustment component 4 is provided with the first fixing component 5, two groups of the first fixing component 5 are provided, one side of the base 1 is also provided with the second adjustment component 6, two groups of the second adjustment component 6 are provided, and one side of the second adjustment component 6 is provided with the second fixing component 7.

[0023] See also Figure 2-3 In this embodiment, the mounting assembly 2 includes a mounting plate 201, a mounting hole 202 and a bolt 203; the bottom surface of the base 1 is provided with a mounting plate 201, one side of the mounting plate 201 is provided with a mounting hole 202, and the mounting hole 202 is provided with multiple groups, and the inner side of the mounting hole 202 is provided with a bolt 203, and the bolt 203 and the mounting hole 202 are threadedly connected to each other, and the base 1 is connected and fixed by the mounting plate 201, and the mounting hole 202 is used to clarify the installation and fixing position of the bolt 203, and the bolt 203 is rotated in the mounting hole 202, so as to realize the stable fixing of the mounting plate 201 to the mechanical equipment. The effect of fixing the installation position; the early warning component 3 includes an early warning machine body 301, a positioning groove 302 and a positioning column 303; the early warning machine body 301 is arranged on one side of the base 1, and the bottom surface of the early warning machine body 301 is provided with a positioning groove 302, and the positioning groove 302 is provided with two groups, and the positioning column 303 is arranged on one side of the base 1, and the positioning column 303 is provided with two groups, and the positioning column 303 and the positioning groove 302 are mutually embedded, and the early warning machine body 301 is used to perform specific anti-collision warning operations, and the positioning column 303 is embedded in the positioning groove 302, so as to clarify the installation and placement position of the early warning machine body 301;

[0024] The first adjustment component 4 includes a bidirectional adjustment screw 401 and a first motor 402; a bidirectional adjustment screw 401 is provided on one side of the base 1, and a first motor 402 is provided on the other side of the base 1, and the output end of the first motor 402 is connected to the bidirectional adjustment screw 401, and the bidirectional adjustment screw 401 is driven to rotate by the first motor 402, and the bidirectional adjustment screw 401 is rotated to flexibly adjust the distance between the two groups of first fixed components 5; the first fixed component 5 includes a first fixed block 501, a first fixed column 502 and a first fixed groove 503; the bidirectional adjustment screw 4 01 is provided with a first fixing block 501 on the outside, and the first fixing block 501 is provided with two groups. A first fixing column 502 is provided on one side of the first fixing block 501, and a first fixing groove 503 is provided on one side of the early warning aircraft body 301, and the first fixing groove 503 is provided with two groups. The first fixing column 502 and the first fixing groove 503 are interlocked with each other, and the first fixing column 502 is connected and fixed by the first fixing block 501, and the first fixing column 502 is embedded in the first fixing groove 503, so that the early warning aircraft body 301 is installed and fixed in the vertical direction according to the actual size of the early warning aircraft body 301.

[0025] See also Figure 4 In this embodiment, the second adjustment component 6 includes a second screw rod 601 and a second motor 602; a second screw rod 601 is provided on one side of the base 1, and two groups of second screw rods 601 are provided. A second motor 602 is provided on the other side of the base 1, and the output end of the second motor 602 is connected to the second screw rod 601. The second motor 602 drives the second screw rod 601 to rotate, and the second screw rod 601 is rotated to flexibly adjust the spacing between the two groups of second fixing components 7; the second fixing component 7 includes a second fixing block 701, a second fixing column 702 and a second Fixed groove 703; a second fixed block 701 is arranged on the outside of the second screw rod 601, a second fixed column 702 is arranged on one side of the second fixed block 701, a second fixed groove 703 is opened on one side of the early warning aircraft body 301, and two groups of second fixed grooves 703 are opened. The second fixed column 702 and the second fixed groove 703 are interlocked with each other, and the second fixed column 702 is connected and fixed by the second fixed block 701, and the second fixed column 702 is embedded in the second fixed groove 703, so that the early warning aircraft body 301 is installed and fixed in the horizontal direction according to the actual size of the early warning aircraft body 301.

[0026] Before installing the early warning machine body 301, place the mounting plate 201 at the designated installation position of the equipment, turn the bolt 203 in the mounting hole 202, and turn the bolt 203 to stably install and fix the mounting plate 201 at the corresponding position of the equipment;

[0027] When the device is fixed vertically, the main body 301 of the early warning aircraft is placed on the surface of the base 1, so that the positioning column 303 is embedded in the positioning groove 302, and then the bidirectional adjustment screw rod 401 is driven to rotate by the first motor 402, and the bidirectional adjustment screw rod 401 is rotated to adjust the distance between the two groups of first fixing blocks 501, and the first fixing column 502 is embedded in the first fixing groove 503;

[0028] When the device is fixed horizontally, the second motor 602 drives the second screw rod 601 to rotate, and the second screw rod 601 is rotated to flexibly adjust the distance between the two groups of second fixing blocks 701, and the second fixing column 702 is embedded in the second fixing groove 703, so as to stably install and fix the early warning aircraft body 301.

[0029] Through the above steps, the base 1 is installed and fixed at the specified position of the mechanical equipment by setting the installation component 2, the first adjustment component 4 is fixed by the base 1, the first adjustment component 4 is used to drive the first fixing component 5 to move, the first fixing component 5 is used to clamp and fix the warning component 3 from the vertical direction, and then, the second adjustment component 6 is used to drive the second fixing component 7 to move, the second fixing component 7 is used to clamp and fix the warning component 3 from the horizontal direction, and the warning component 3 is used to perform anti-collision warning operations.

[0030] The embodiments of the present invention are described in detail above in conjunction with the accompanying drawings, but the present invention is not limited to the above embodiments, and various changes can be made within the knowledge scope of those skilled in the art without departing from the purpose of the present invention.

Claims

1. A convenient installation and disassembly mechanism for an anti-collision warning device for engineering machinery, comprising a base (1); characterized in that: The invention also comprises a mounting assembly (2), an early warning assembly (3), a first adjustment assembly (4), a first fixing assembly (5), a second adjustment assembly (6) and a second fixing assembly (7); the mounting assembly (2) is arranged on the bottom surface of the base (1); the early warning assembly (3) is arranged on one side of the base (1); the first adjustment assembly (4) is arranged on one side of the base (1); the first fixing assembly (5) is arranged on one side of the first adjustment assembly (4); two groups of the first fixing assembly (5) are arranged; a second adjustment assembly (6) is also arranged on one side of the base (1); two groups of the second adjustment assembly (6) are arranged; and a second fixing assembly (7) is arranged on one side of the second adjustment assembly (6).

2. According to the installation mechanism of the anti-collision warning device for engineering machinery equipment with convenient assembly and disassembly according to claim 1, it is characterized by: The mounting assembly (2) comprises a mounting plate (201), mounting holes (202) and bolts (203); the mounting plate (201) is arranged on the bottom surface of the base (1); mounting holes (202) are provided on one side of the mounting plate (201); the mounting holes (202) are provided in multiple groups; bolts (203) are provided inside the mounting holes (202); the bolts (203) and the mounting holes (202) are threadedly connected to each other.

3. According to the installation mechanism of the anti-collision warning device for engineering machinery and equipment with convenient assembly and disassembly as claimed in claim 1, it is characterized by: The early warning component (3) comprises an early warning machine body (301), a positioning groove (302) and a positioning column (303); the early warning machine body (301) is arranged on one side of the base (1); the bottom surface of the early warning machine body (301) is provided with a positioning groove (302); the positioning groove (302) is provided in two groups; the positioning column (303) is arranged on one side of the base (1); the positioning column (303) is provided in two groups; the positioning column (303) and the positioning groove (302) are mutually engaged.

4. According to claim 3, the installation mechanism of the anti-collision warning device for engineering machinery equipment with convenient assembly and disassembly is characterized in that: The first adjustment component (4) comprises a bidirectional adjustment screw (401) and a first motor (402); the bidirectional adjustment screw (401) is arranged on one side of the base (1), and the first motor (402) is arranged on the other side of the base (1); the output end of the first motor (402) is interconnected with the bidirectional adjustment screw (401).

5. According to claim 4, the installation mechanism of the anti-collision warning device for engineering machinery equipment with convenient assembly and disassembly is characterized in that: The first fixing assembly (5) comprises a first fixing block (501), a first fixing column (502) and a first fixing groove (503); the first fixing block (501) is arranged outside the bidirectional adjustment screw rod (401), the first fixing block (501) is arranged in two groups, a first fixing column (502) is arranged on one side of the first fixing block (501), a first fixing groove (503) is opened on one side of the early warning aircraft body (301), the first fixing groove (503) is opened in two groups, and the first fixing column (502) and the first fixing groove (503) are interlocked.

6. The installation mechanism of the anti-collision warning device for engineering machinery and equipment with convenient assembly and disassembly according to claim 4 is characterized in that: The second adjustment component (6) comprises a second screw rod (601) and a second motor (602); the second screw rod (601) is arranged on one side of the base (1), and two groups of the second screw rod (601) are arranged; the second motor (602) is arranged on the other side of the base (1), and the output end of the second motor (602) is connected to the second screw rod (601).

7. The installation mechanism of the anti-collision warning device for engineering machinery and equipment with convenient assembly and disassembly according to claim 6 is characterized by: The second fixing assembly (7) comprises a second fixing block (701), a second fixing column (702) and a second fixing groove (703); a second fixing block (701) is arranged outside the second screw rod (601), a second fixing column (702) is arranged on one side of the second fixing block (701), a second fixing groove (703) is opened on one side of the early warning aircraft body (301), two groups of second fixing grooves (703) are opened, and the second fixing column (702) and the second fixing groove (703) are interlocked.

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