CN213225087U - Machine head installation guide mechanism of machine tool - Google Patents

Machine head installation guide mechanism of machine tool Download PDF

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Publication number
CN213225087U
CN213225087U CN202021532838.2U CN202021532838U CN213225087U CN 213225087 U CN213225087 U CN 213225087U CN 202021532838 U CN202021532838 U CN 202021532838U CN 213225087 U CN213225087 U CN 213225087U
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Prior art keywords
screw
machine
spring
reference column
guide mechanism
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CN202021532838.2U
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Chinese (zh)
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徐雅鹏
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Melkat Machinery Wuxi Co ltd
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Melkat Machinery Wuxi Co ltd
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Abstract

The utility model discloses a aircraft nose installation guiding mechanism of lathe, concretely relates to lathe technical field, including reference column, screw machine, screw, spring, the top surface fixed mounting of reference column has the handle, and one side movable mounting of reference column has the shock attenuation board, and the inner chamber fixed mounting of shock attenuation board has the spring, and one side laminating of shock attenuation board has the acoustic baffle, and the bottom surface fixedly connected with of slide bears the dish, bears one side of dish and passes through roller bearing demountable installation and have the carriage release lever, and one side movable mounting of reference column has the screw, and the surface of screw and the inner wall looks joint of reference column. The utility model discloses a set up spring and acoustic baffle, the spring has the effect of fine shock attenuation buffering, in the aircraft nose installation of lathe, produces the amplitude, and the spring can carry out corresponding slowing down to protect the internals of whole lathe equipment, make the part of each position can not be because of the amplitude is not hard up or the frame that loosens, and the effect of acoustic baffle is the partial noise that produces when just adsorbing the installation.

Description

Machine head installation guide mechanism of machine tool
Technical Field
The utility model relates to a lathe technical field, more specifically say, the utility model relates to a aircraft nose installation guiding mechanism of lathe.
Background
Machine tools are machines for manufacturing machines, also called machine tools or machine tools, and are conventionally called machine tools for short, and are generally divided into metal cutting machine tools, forging machine tools, woodworking machine tools and the like, and many methods for processing machine parts in modern machine manufacturing are provided: in addition to cutting, casting, forging, welding, stamping, extruding and the like are also available, but parts with high precision requirements and fine surface roughness requirements generally need to be finally machined by cutting on a machine tool, and the machine tool plays an important role in national economy and modernization construction.
However, in practical use, there still exist some disadvantages, such as:
one, many lathe on the market can produce noise and vibrations in the process of aircraft nose installation, and the vibrations of small amplitude can lead to the installation deviation, and uses for a long time down, and vibrations can lead to the inside part of whole lathe loose impaired, leads to scattered frame even, has the potential safety hazard, but the emergence of accident is all kept away in the lack of specific damping device of most erection equipment.
Second, the reference column of current lathe aircraft nose erection equipment, poor stability, the contractility is limited, and mounting structure is insecure, and life is short, and a lot of equipment all is fixed unmovable, when meetting double-end lathe, can not disposable installation, but need install in proper order, not only wastes time but also consumes the manpower.
It is therefore desirable to provide a machine tool head mounting guide mechanism.
SUMMERY OF THE UTILITY MODEL
In order to overcome the above-mentioned defect of prior art, the embodiment of the utility model provides a aircraft nose installation guiding mechanism of lathe, through spring and acoustic baffle, the spring has the effect of fine shock attenuation buffering, in the aircraft nose installation of lathe, produce the amplitude, the spring can carry out corresponding slowing down, thereby protect the internals of whole lathe equipment, make the part of each position can not be because of the amplitude is not hard up or scattered frame, and the effect of acoustic baffle is the partial noise that produces when just adsorbing the installation, in order to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a aircraft nose installation guiding mechanism of lathe, includes reference column, screw machine, screw, spring, the top surface fixed mounting of reference column has the handle, one side movable mounting of reference column has the shock attenuation board, the inner chamber fixed mounting of shock attenuation board has the spring, one side laminating of shock attenuation board has the acoustic baffle, the bottom demountable installation of acoustic baffle has the roller bearing, the slide is installed to the bottom of reference column is inlayed, the bottom surface fixedly connected with of slide bears the dish, one side of bearing the dish has the carriage release lever through roller bearing demountable installation, the bottom surface demountable installation who bears the dish has the gyro wheel, the inner chamber swing joint of gyro wheel has the wheel core, one side swing joint of gyro wheel has the stationary blade, one side movable mounting of reference column has the screw, the surface of screw and the inner wall looks joint of reference column.
In a preferred embodiment, the inner cavity of the sliding seat is provided with a plurality of screw holes, and the distance between the screw holes is three to five centimeters.
In a preferred embodiment, the upper end and the lower end of the spring are respectively and fixedly connected with an upper gasket and a lower gasket, and the spring is movably sleeved with a guide post.
In a preferred embodiment, the surface of the screw is threaded, a screw cap is fixedly connected to the top surface of the screw, a drill point is fixedly mounted at the top end of the screw, and the screw is made of a metal component.
In a preferred embodiment, a screw machine is movably mounted on the top surface of the moving rod, and the surface of the moving rod is provided with anti-skid threads.
In a preferred embodiment, a connecting rod is fixedly installed at one side of the screw machine, a handle is fixedly installed at one end of the connecting rod, and a sponge ring is adhered to the surface of the handle.
In a preferred embodiment, an anti-drop box is fixedly connected to one side of the screw machine, and a drill body is fixedly mounted on the surface of the anti-drop box.
In a preferred embodiment, the surface of the sound absorption plate is attached with sound absorption materials, and the sound absorption plate is rectangular.
The utility model discloses a technological effect and advantage:
1. the utility model discloses a set up spring and acoustic baffle, the spring has the effect of fine shock attenuation buffering, in the aircraft nose installation of lathe, produces the amplitude, and the spring can carry out corresponding slowing down to protect the internals of whole lathe equipment, make the part of each position can not be because of the amplitude is not hard up or the frame that loosens, and the effect of acoustic baffle is the partial noise that produces when just adsorbing the installation.
2. The utility model discloses a set up the stationary blade, fix the gyro wheel that bears set bottom, prevent the displacement, aim at the aircraft nose both sides with whole installation device after that, the inner wall that keeps the reference column keeps certain distance with the aircraft nose, and operating personnel holds the handle after that, slightly does the effort and nudges the reference column, closely laminates until the inner wall of reference column and the outer wall of aircraft nose, carries out corresponding installation through the set screw at last, has improved work efficiency.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention.
Fig. 2 is a schematic sectional view of the present invention.
Fig. 3 is the schematic diagram of the damping plate structure of the present invention.
Fig. 4 is a schematic view of the screw structure of the present invention.
Fig. 5 is an enlarged schematic view of the screw machine of the present invention.
The reference signs are: 1. a positioning column; 2. a damper plate; 3. a handle; 4. a sound absorbing panel; 5. a carrier tray; 6. A screw eye; 7. a slide base; 8. a screw; 9. a fixing sheet; 10. a screw machine; 11. a handle; 12. a travel bar; 13. a roller; 14. a wheel core; 15. a screw cap; 16. a thread; 17. drilling a tip; 18. an upper gasket; 19. a spring; 20. a lower gasket; 21. a guide post; 22. a connecting rod; 23. an anti-drop box; 24. a drill body; 25. and (4) rolling shafts.
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.
As shown in the attached figures 1-5, the machine head installation guide mechanism of a machine tool comprises a positioning column 1, a screw machine 10, a screw 8 and a spring 19, wherein a handle 3 is fixedly installed on the top surface of the positioning column 1, a damping plate 2 is movably installed on one side of the positioning column 1, the spring 19 is fixedly installed in the inner cavity of the damping plate 2, a sound absorbing plate 4 is attached to one side of the damping plate 2, a rolling shaft 25 is detachably installed at the bottom of the sound absorbing plate 4, a sliding seat 7 is embedded at the bottom of the positioning column 1, a bearing disc 5 is fixedly connected to the bottom surface of the sliding seat 7, a moving rod 12 is detachably installed on one side of the bearing disc 5 through the rolling shaft 25, a roller 13 is detachably installed on the bottom surface of the bearing disc 5, a wheel core 14 is movably connected to the inner cavity of the roller 13, a fixing piece 9 is movably connected to one side of, a plurality of screw holes 6 have been seted up to the inner chamber of slide 7, and the interval value of screw hole 6 is three to five centimetres, screw thread 16 has been seted up on the surface of screw 8, the top surface fixedly connected with screw cap 15 of screw 8, and the top fixed mounting of screw 8 has drill point 17, the material of screw 8 adopts the metal material component, one side fixed mounting of screw machine 10 has connecting rod 22, the one end fixed mounting of connecting rod 22 has handle 11, and the surface bonding of handle 11 has the sponge circle, one side fixedly connected with anticreep box 23 of screw machine 10, and the fixed surface of anticreep box 23 installs drill body 24.
Referring to the attached fig. 3 of the specification specifically, the upper end and the lower end of the spring 19 are fixedly connected with an upper gasket 18 and a lower gasket 20 respectively, and the spring 19 is movably sleeved with a guide post 21.
The implementation mode is specifically as follows: the upper gasket 18 and the lower gasket 20 can fix the upper top end and the lower top end of the guide post 21 and the spring 19, so that the spring 19 is prevented from sliding off, and the damping and buffering effects are prevented from being influenced.
Referring to the attached fig. 2, the screw machine 10 is movably mounted on the top surface of the moving rod 12, and the surface of the moving rod 12 is provided with anti-slip threads.
The implementation mode is specifically as follows: the screw machine 10 is placed on the surface of the movable rod 12, and the anti-slip threads formed on the surface of the movable rod 12 are used for increasing the friction force between the bottom surface of the screw machine 10 and the surface of the movable rod 12 and preventing the screw machine 10 from accidentally falling off to hurt workers.
Referring to the attached fig. 2 of the specification, a sound absorbing material is attached to the surface of the sound absorbing plate 4, and the sound absorbing plate 4 is rectangular.
The implementation mode is specifically as follows: the sound absorption plate 4 can adsorb the noise that produces in the lathe aircraft nose installation, and the sound absorption plate 4 also can play the effect of a secondary protection simultaneously, and the protection reference column 1 is not damaged.
The utility model discloses the theory of operation:
the first step is as follows: the operator first assembles the various components of the device normally and then starts the device normally.
The second step is that: firstly, an operator moves the installation equipment of the machine head of the whole machine tool to the machine head to be installed, pulls out the fixing piece 9, fixes the roller 13 at the bottom of the bearing disc 5 to prevent displacement, then aligns the whole installation device to two sides of the machine head, keeps a certain distance between the inner wall of the positioning column 1 and the machine head, then holds the handle 3 by hand, slightly pushes the positioning column 1 until the inner wall of the positioning column 1 is tightly attached to the outer wall of the machine head, then pushes and pulls the moving rod 12 provided with the screw machine 10 to one side of the bearing disc 5, installs the screw 8 into the corresponding screw eye 6 by using the electric screw machine 10, the specific position of the screw eye 6 is determined according to the situation, after the screw 8 is fixed, the operator starts to assemble each part of the machine head, returns the moving rod 12 provided with the screw machine 10 to the original position after the assembly is finished, if the screw machine 10 is not needed, can pack up screw machine 10 to also pack up carriage release lever 12 through roller 25, laminate it in one side of acoustic baffle 4 simultaneously, save working space, unscrew screw 8 at last, return the reference column 1 normal position, be convenient for next use can.
The third step: the operator first closes the device normally, then checks whether the fixity between the various components of the device is normal, and then replaces and repairs the more aged and worn parts inside the device.
The points to be finally explained are: first, in the description of the present application, it should be noted that, unless otherwise specified and limited, the terms "mounted," "connected," and "connected" should be understood broadly, and may be a mechanical connection or an electrical connection, or a communication between two elements, and may be a direct connection, and "upper," "lower," "left," and "right" are only used to indicate a relative positional relationship, and when the absolute position of the object to be described is changed, the relative positional relationship may be changed;
secondly, the method comprises the following steps: in the drawings of the disclosed embodiments of the present invention, only the structures related to the disclosed embodiments are referred to, and other structures can refer to the common design, and under the condition of no conflict, the same embodiment and different embodiments of the present invention can be combined with each other;
and finally: the above description is only for the preferred embodiment of the present invention and should not be taken as limiting the invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (8)

1. The utility model provides a aircraft nose installation guiding mechanism of lathe, includes reference column (1), screw machine (10), screw (8), spring (19), its characterized in that: the top surface fixed mounting of reference column (1) has handle (3), one side movable mounting of reference column (1) has shock attenuation board (2), the inner chamber fixed mounting of shock attenuation board (2) has spring (19), one side laminating of shock attenuation board (2) has acoustic baffle (4), the bottom demountable installation of acoustic baffle (4) has roller bearing (25), the bottom of reference column (1) is inlayed and is installed slide (7), the bottom surface fixedly connected with of slide (7) bears dish (5), one side of bearing dish (5) has carriage release lever (12) through roller bearing (25) demountable installation, the bottom surface demountable installation of bearing dish (5) has gyro wheel (13), the inner chamber swing joint of gyro wheel (13) has wheel core (14), one side swing joint of gyro wheel (13) has stationary blade (9), one side movable mounting of reference column (1) has screw (8), the surface of the screw (8) is clamped with the inner wall of the positioning column (1).
2. The machine head installation guide mechanism of a machine tool according to claim 1, wherein: the inner cavity of the sliding seat (7) is provided with a plurality of screw holes (6), and the distance value of the screw holes (6) is three to five centimeters.
3. The machine head installation guide mechanism of a machine tool according to claim 1, wherein: the upper end and the lower end of the spring (19) are respectively fixedly connected with an upper gasket (18) and a lower gasket (20), and the spring (19) is movably sleeved with a guide post (21).
4. The machine head installation guide mechanism of a machine tool according to claim 1, wherein: screw thread (16) are seted up on the surface of screw (8), the top surface fixedly connected with screw cap (15) of screw (8), just the top fixed mounting of screw (8) has drill point (17), the material of screw (8) adopts the metal material component.
5. The machine head installation guide mechanism of a machine tool according to claim 1, wherein: the top surface of the moving rod (12) is movably provided with a screw machine (10), and the surface of the moving rod (12) is provided with anti-skid grains.
6. The machine head installation guide mechanism of a machine tool according to claim 1, wherein: one side fixed mounting of screw machine (10) has connecting rod (22), the one end fixed mounting of connecting rod (22) has handle (11), just the surface bonding of handle (11) has the sponge circle.
7. The machine head installation guide mechanism of a machine tool according to claim 1, wherein: one side fixedly connected with anticreep box (23) of screw machine (10), just the fixed surface of anticreep box (23) installs and bores body (24).
8. The machine head installation guide mechanism of a machine tool according to claim 1, wherein: the surface of the sound absorption plate (4) is attached with a sound absorption material, and the sound absorption plate (4) is rectangular.
CN202021532838.2U 2020-07-29 2020-07-29 Machine head installation guide mechanism of machine tool Active CN213225087U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202021532838.2U CN213225087U (en) 2020-07-29 2020-07-29 Machine head installation guide mechanism of machine tool

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202021532838.2U CN213225087U (en) 2020-07-29 2020-07-29 Machine head installation guide mechanism of machine tool

Publications (1)

Publication Number Publication Date
CN213225087U true CN213225087U (en) 2021-05-18

Family

ID=75891317

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202021532838.2U Active CN213225087U (en) 2020-07-29 2020-07-29 Machine head installation guide mechanism of machine tool

Country Status (1)

Country Link
CN (1) CN213225087U (en)

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