Gear broaching machine for roller production

Abstract

The utility model relates to the technical field of gear broaching machines, in particular to a gear broaching machine for roller production, which comprises a machine body. The damping mechanism comprises a mounting plate, and the mounting plate is arranged on the lower surface of the machine body; and the cleaning mechanism comprises a water scraping plate and a sliding groove, and the water scraping plate is arranged on the surface of the observation window. Through the fixed connection of the mounting plate and the elastic metal plate, the fixed connection of the mounting plate and the damping spring, the fixed connection of the damping spring and the base, the fixed connection of the base and the stabilizer bar, the sleeved connection of the stabilizer bar and the lantern ring, and the fixed connection of the lantern ring and the first connecting rod, when a machine body vibrates, the mounting plate can be stressed; the mounting plate compresses the elastic metal plate and the damping spring, and the elastic metal plate and the damping spring can rebound to generate opposite acting force, so that the buffering effect is generated, the damping effect on the fuselage is achieved, the stability of the fuselage is improved, damage caused by vibration of the fuselage to the fuselage is reduced, and noise generated by vibration of the fuselage is weakened.

Description

Technical Field

[0001] The utility model relates to the technical field of gear broaching machines, in particular to a gear broaching machine for roller production. Background Art

[0002] Gear broaching machines are mainly used to manufacture various gears, splines, screws and other components. They remove a certain depth of metal layer on the metal material through the relative movement of the rotating workpiece and the tool to form a tooth-shaped structure.

[0003] With the development of the times and the advancement of science and technology, more and more mechanical equipment have been invented. Most of the mechanical equipment requires components such as gears and screws to maintain operation. As various mechanical equipment enters people's lives, the output of components such as gears and screws has also increased. The production of many of these components requires the use of gear broaching machines. Therefore, the importance of gear broaching machines is self-evident. However, traditional gear broaching machines cannot absorb vibration during operation, which will not only damage the equipment itself, but also generate huge noise, pollute the environment, and harm the workers' health. Utility Model Content

[0004] The purpose of the utility model is to provide a gear broaching machine for roller production, so as to solve the problem proposed in the above background technology that the traditional gear broaching machine cannot absorb vibration during operation, which not only causes damage to the equipment itself, but also generates huge noise, pollutes the environment, and harms the workers' health.

[0005] To achieve the above-mentioned purpose, the present invention provides the following technical solution: a gear broaching machine for roller production, comprising:

[0006] The machine body comprises a fuselage, a control box is fixedly connected to the surface of the fuselage, and an observation window is fixedly connected to the surface of the fuselage;

[0007] The shock-absorbing mechanism includes a mounting plate, the mounting plate being disposed on the lower surface of the fuselage, the lower surface of the mounting plate being fixedly connected to an elastic metal plate, the lower surface of the mounting plate being fixedly connected to a shock-absorbing spring, the surface of the shock-absorbing spring being fixedly connected to a base, the surface of the base being fixedly connected to a stabilizing rod, the surface of the stabilizing rod being sleeved with a collar, and the surface of the collar being fixedly connected to a first connecting rod;

[0008] The cleaning mechanism includes a wiper and a slide. The wiper is arranged on the surface of the observation window, and the slide is opened on the surface of the fuselage. The surface of the wiper is fixedly connected to a second connecting rod, and the surface of the second connecting rod is fixedly connected to a moving rod. The end of the moving rod away from the second connecting rod is threadedly connected to a threaded sleeve.

[0009] Preferably, the mounting plate is in the shape of a plate, the elastic metal plate is in the shape of an arc-shaped plate, and both ends of the shock-absorbing spring are fixedly connected to the mounting plate and the base respectively.

[0010] Preferably, the base is plate-shaped, the stabilizing rod is round rod-shaped, and the collar is annular.

[0011] Preferably, the first connecting rod is in the shape of a round rod, and the mounting plate is slidably connected to the stabilizing rod via the first connecting rod and a collar.

[0012] Preferably, the wiper is in the shape of a long plate, the wiper is slidably connected to the observation window via a second connecting rod, and the slide grooves are distributed in two groups on the surface of the fuselage.

[0013] Preferably, the second connecting rod and the moving rod are both round rod-shaped, and the second connecting rod is slidably connected to the fuselage through the moving rod.

[0014] Preferably, a surface portion of the moving rod is provided with threads, and the threaded sleeve is rotatably connected to the body through the moving rod.

[0015] Compared with the prior art, the beneficial effects of the present invention are:

[0016] 1. Through the fixed connection between the mounting plate and the elastic metal plate, the fixed connection between the mounting plate and the shock-absorbing spring, the fixed connection between the shock-absorbing spring and the base, the fixed connection between the base and the stabilizer bar, the socketing of the stabilizer bar and the collar, and the fixed connection between the collar and the first connecting rod, when the fuselage vibrates, a force is exerted on the mounting plate, causing the mounting plate to compress the elastic metal plate and the shock-absorbing spring. The elastic metal plate and the shock-absorbing spring will rebound to generate a reverse force, thereby producing a buffering effect, reducing the force exerted by the fuselage on the mounting plate, and thereby achieving a shock-absorbing effect on the fuselage, improving the stability of the fuselage, reducing the damage caused by the vibration of the fuselage itself, and reducing the noise generated by the vibration of the fuselage.

[0017] 2. A sliding groove is opened on the surface of the fuselage, the wiper and the second connecting rod are fixedly connected, the second connecting rod and the moving rod are fixedly connected, and the moving rod and the threaded sleeve are threadedly connected. Pulling the moving rod and the threaded sleeve can drive the wiper to slide on the surface of the observation window. When water generated when the fuselage is working splashes onto the observation window, the moving rod and the threaded sleeve can be pulled to make the wiper scrape off the water on the observation window, thereby cleaning the inner glass of the observation window without affecting the workers' observation of the interior of the fuselage. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 This is a frontal perspective schematic diagram of the structure of the present utility model;

[0019] Figure 2 This is a side perspective schematic diagram of the structure of the utility model;

[0020] Figure 3 This is a partial schematic diagram of the structure of the shock absorbing mechanism of the utility model;

[0021] Figure 4 It is a schematic diagram of a three-dimensional partial cross-section of the structure of the wiper blade of the utility model;

[0022] Figure 5 For this utility model Figure 4 Schematic diagram of the enlarged structure at point A in the middle.

[0023] In the figure: 1. fuselage; 11. control box; 12. observation window; 2. mounting plate; 21. elastic metal plate; 22. shock-absorbing spring; 23. base; 24. stabilizer bar; 25. collar; 26. first connecting rod; 3. wiper; 31. slide; 32. second connecting rod; 33. moving rod; 34. threaded sleeve. DETAILED DESCRIPTION

[0024] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0025] See also Figure 1-5 , an embodiment provided by the utility model:

[0026] A gear broaching machine for roller production, comprising:

[0027] The machine body includes a machine body 1, which is used for gear broaching. A control box 11 is fixedly connected to the surface of the machine body 1, and the control box 11 is used to control the machine body 1. An observation window 12 is fixedly connected to the surface of the machine body 1, and the observation window 12 is used for workers to observe the internal conditions of the machine body 1. The machine body 1 and the control box 11 are both existing products and are not technical protection points of this application. No further details are given here.

[0028] The shock absorbing mechanism includes a mounting plate 2, which is arranged on the lower surface of the fuselage 1 and is used to mount the fuselage 1 and the control box 11. The lower surface of the mounting plate 2 is fixedly connected to an elastic metal plate 21, and the lower surface of the mounting plate 2 is fixedly connected to a shock absorbing spring 22. The elastic metal plate 21 and the shock absorbing spring 22 are both used to produce a buffering effect, thereby reducing the force generated by the fuselage 1 on the mounting plate 2, thereby achieving a shock absorbing effect on the fuselage 1. The surface of the shock absorbing spring 22 is fixedly connected to a base 23, which is the base of the entire device and is used to mount a stabilizing rod 24. The surface of the base 23 is fixedly connected to the stabilizing rod 24, and the surface of the stabilizing rod 24 is sleeved with a collar 25. The stabilizing rod 24 and the collar 25 are used in conjunction with each other. The collar 25 slides up and down on the surface of the stabilizing rod 24, so that the fuselage 1 will only produce a small up and down movement and will not shake left and right, thereby improving the stability of the fuselage 1. The surface of the collar 25 is fixedly connected to a first connecting rod 26, which is used to connect the mounting plate 2 and the collar 25;

[0029] The cleaning mechanism includes a wiper 3 and a slide 31. The wiper 3 is arranged on the surface of the observation window 12. The wiper 3 is used to scrape off water on the inner glass of the observation window 12 so as not to affect the workers' observation of the internal situation of the fuselage 1. The slide 31 is opened on the surface of the fuselage 1. The slide 31 is used to move the moving rod 33. The surface of the wiper 3 is fixedly connected with a second connecting rod 32. The second connecting rod 32 is used to connect two sets of wiper blades 3 and is also used to connect the wiper 3 and the moving rod 33. The surface of the second connecting rod 32 is fixedly connected with the moving rod 33. The moving rod 33 is used to pull the wiper 3 up and down. The end of the moving rod 33 away from the second connecting rod 32 is threadedly connected with a threaded sleeve 34. The threaded sleeve 34 is used to lock the wiper 3 in a certain position when the wiper 3 is not in use.

[0030] Furthermore, the mounting plate 2 is in the shape of a plate, and is used to mount the fuselage 1 and the control box 11. The elastic metal plate 21 is in the shape of an arc-shaped plate. The two ends of the shock-absorbing spring 22 are fixedly connected to the mounting plate 2 and the base 23 respectively. The elastic metal plate 21 and the shock-absorbing spring 22 are both used to produce a buffering effect, reducing the force generated by the fuselage 1 on the mounting plate 2, thereby achieving a shock-absorbing effect on the fuselage 1.

[0031] Furthermore, the base 23 is in the shape of a plate. The base 23 is the base of the entire device and is used to install the stabilizing rod 24. The stabilizing rod 24 is in the shape of a round rod, and the ring 25 is in the shape of a circular ring. The stabilizing rod 24 and the ring 25 are used in conjunction with each other. The ring 25 slides up and down on the surface of the stabilizing rod 24, so that the fuselage 1 will only produce a slight up and down movement, and will not shake left and right, thereby improving the stability of the fuselage 1.

[0032] Furthermore, the first connecting rod 26 is in the shape of a round rod, and the mounting plate 2 is slidingly connected to the stabilizing rod 24 via the first connecting rod 26 and the collar 25 . The first connecting rod 26 is used to connect the mounting plate 2 and the collar 25 .

[0033] Furthermore, the wiper 3 is in the shape of a long plate, and is slidably connected to the observation window 12 through a second connecting rod 32. The wiper 3 is used to scrape off water on the inner glass of the observation window 12 so as not to affect the workers' observation of the internal situation of the fuselage 1. The slide grooves 31 are distributed in two groups on the surface of the fuselage 1, and the slide grooves 31 are used to move the moving rod 33.

[0034] Furthermore, the second connecting rod 32 and the moving rod 33 are both round rod-shaped. The second connecting rod 32 is slidingly connected to the fuselage 1 through the moving rod 33. The second connecting rod 32 is used to connect the two sets of wipers 3 and is also used to connect the wipers 3 and the moving rod 33.

[0035] Furthermore, a surface portion of the moving rod 33 is provided with threads, and the moving rod 33 is used to pull the wiper 3 up and down. The threaded sleeve 34 is rotatably connected to the fuselage 1 through the moving rod 33, and the threaded sleeve 34 is used to lock the wiper 3 in a certain position when the wiper 3 is not in use.

[0036] Working principle: When the fuselage 1 vibrates, it will exert force on the mounting plate 2, causing the mounting plate 2 to compress the elastic metal plate 21 and the shock-absorbing spring 22. The elastic metal plate 21 and the shock-absorbing spring 22 will rebound to generate a reverse force, offsetting the force generated by the fuselage 1 on the mounting plate 2, thereby producing a buffering effect, weakening the force generated by the fuselage 1 on the mounting plate 2, and thereby achieving a shock-absorbing effect on the fuselage 1.

[0037] When water generated by the fuselage 1 during operation splashes onto the observation window 12, the movable rod 33 and the threaded sleeve 34 can be pulled to cause the wiper 3 to scrape off the water on the observation window 12, thereby cleaning the inner glass of the observation window 12. When the wiper 3 is not needed, the threaded sleeve 34 can be rotated and tightened to lock the wiper 3 in a certain position.

[0038] It will be apparent to those skilled in the art that the present invention is not limited to the details of the exemplary embodiments described above and that the present invention can be implemented in other specific forms without departing from the spirit or essential characteristics of the present invention. Therefore, the embodiments should be considered in all respects as illustrative and non-restrictive, and the scope of the present invention is defined by the appended claims, not the foregoing description, and all variations within the meaning and range of equivalents of the claims are intended to be encompassed within the present invention. Any reference sign in a claim should not be construed as limiting the claim to which it relates.

Claims

1. A gear broaching machine for roller production, characterized in that: include: The machine body comprises a machine body (1), a control box (11) is fixedly connected to the surface of the machine body (1), and an observation window (12) is fixedly connected to the surface of the machine body (1); A shock-absorbing mechanism comprises a mounting plate (2), the mounting plate (2) being arranged on the lower surface of a fuselage (1), the lower surface of the mounting plate (2) being fixedly connected to an elastic metal plate (21), the lower surface of the mounting plate (2) being fixedly connected to a shock-absorbing spring (22), the surface of the shock-absorbing spring (22) being fixedly connected to a base (23), the surface of the base (23) being fixedly connected to a stabilizing rod (24), the surface of the stabilizing rod (24) being sleeved with a collar (25), and the surface of the collar (25) being fixedly connected to a first connecting rod (26); The cleaning mechanism comprises a wiper (3) and a chute (31), wherein the wiper (3) is arranged on the surface of an observation window (12), and the chute (31) is opened on the surface of a machine body (1); the surface of the wiper (3) is fixedly connected to a second connecting rod (32), the surface of the second connecting rod (32) is fixedly connected to a moving rod (33), and one end of the moving rod (33) away from the second connecting rod (32) is threadedly connected to a threaded sleeve (34).

2. The gear broaching machine for roller production according to claim 1, characterized in that: The mounting plate (2) is plate-shaped, the elastic metal plate (21) is arc-shaped, and the two ends of the shock-absorbing spring (22) are fixedly connected to the mounting plate (2) and the base (23) respectively.

3. The gear broaching machine for roller production according to claim 1, characterized in that: The base (23) is plate-shaped, the stabilizing rod (24) is round-rod-shaped, and the collar (25) is annular.

4. The gear broaching machine for roller production according to claim 1, characterized in that: The first connecting rod (26) is in the shape of a round rod, and the mounting plate (2) is slidably connected to the stabilizing rod (24) via the first connecting rod (26) and the collar (25).

5. The gear broaching machine for roller production according to claim 1, characterized in that: The wiper (3) is in the shape of a long plate and is slidably connected to the observation window (12) via a second connecting rod (32). The slide grooves (31) are distributed in two groups on the surface of the fuselage (1).

6. The gear broaching machine for roller production according to claim 1, characterized in that: The second connecting rod (32) and the moving rod (33) are both in the shape of round rods, and the second connecting rod (32) is slidably connected to the fuselage (1) via the moving rod (33).

7. The gear broaching machine for roller production according to claim 1, characterized in that: The surface portion of the moving rod (33) is provided with threads, and the threaded sleeve (34) is rotatably connected to the body (1) through the moving rod (33).

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