CN220093120U

CN220093120U - Aviation accessory centering and punching tool capable of improving centering precision and punching speed

Info

Publication number: CN220093120U
Application number: CN202321643783.6U
Authority: CN
Inventors: 王二飞
Original assignee: Suzhou Degen Electromechanical Co ltd
Current assignee: Suzhou Degen Electromechanical Co ltd
Priority date: 2023-06-27
Filing date: 2023-06-27
Publication date: 2023-11-28
Anticipated expiration: 2033-06-27

Abstract

The utility model belongs to the technical field of punching equipment, and particularly relates to an aviation accessory centering punching tool for improving centering precision and punching rate. According to the utility model, the aviation accessory is fixed through the cooperation of the limiting plate and the limiting frame, and the drill bit can horizontally and forwards and backwards move under the action of the first screw rod and the second screw rod, so that the punching efficiency and the punching precision of the equipment are effectively improved.

Description

Aviation accessory centering and punching tool capable of improving centering precision and punching speed

Technical Field

The utility model relates to the technical field of punching equipment, in particular to an aviation accessory centering and punching tool capable of improving centering accuracy and punching speed.

Background

The combination of the aerospace technology and other scientific technologies creates a plurality of new technical approaches which are directly used for a plurality of departments of national economy, and huge economic and social benefits are generated.

The prior art has the following problems:

the existing aviation accessory generally needs to be centered and punched when being processed, and the existing aviation accessory centering and punching tool is easy to move due to the fact that the aviation accessory is easy to move when being used, so that the punching precision is greatly affected, meanwhile, the existing aviation accessory centering and punching tool generally needs to be adjusted to continuously punch the aviation accessory every time the hole is punched, and therefore punching efficiency is greatly reduced.

Disclosure of Invention

Aiming at the defects of the prior art, the utility model provides an aviation accessory centering and punching tool for improving centering precision and punching speed, and solves the problems of insufficient punching precision and low punching efficiency of the existing aviation accessory centering and punching tool.

In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an aviation annex centering frock of punching of improvement centering accuracy and punching rate, includes the base, upper portion surface one side fixed mounting of base has the riser, the top fixed mounting of riser has first motor, one side of riser is provided with the diaphragm, one side below fixed mounting of diaphragm has first installation piece, the below of first installation piece is provided with the second installation piece, the below of second installation piece is provided with the mount pad, the below fixed mounting of mount pad has the mount, the inside fixed mounting of mount has the drill bit subassembly, the front surface fixed mounting of riser has the fixed block, the below fixed mounting of fixed block has the slide bar, the surface sleeve of slide bar has reset spring, the below of drill bit subassembly is provided with the locating rack, one side fixed mounting of locating rack has the fixed plate, one side surface fixed mounting of riser has electric telescopic handle, one side fixed mounting of electric telescopic handle has the locating plate, one side inside fixed mounting of first installation piece has the second motor, the inside fixed mounting of one side of first installation piece has the second piece, the inside fixed mounting of first piece has the screw rod, the inside movable connection has the screw rod, the screw rod is connected to the second, the screw rod is connected to the inside fixed mounting of second screw rod.

As a preferable technical scheme of the utility model, the vertical plates are fixedly arranged on two sides of the upper surface of the base, the transverse plates are connected between the vertical plates in a sliding manner, and the first mounting blocks are fixedly arranged on two sides below the transverse plates.

As a preferable technical scheme of the utility model, the two sides of the front surface and the two sides of the back surface of the limiting frame are fixedly provided with the fixing plates, the fixing plates are in sliding connection with the sliding rods, the reset springs are fixedly connected with the fixing plates, and the middle part of the inside of the limiting frame is provided with the through holes.

As a preferable technical scheme of the utility model, two groups of fixing blocks are fixedly arranged on the front surface and the back surface of the vertical plate, and the sliding rod is fixedly connected between the fixing blocks.

As a preferable technical scheme of the utility model, a second motor is fixedly arranged in one side of each of the first installation block and the second installation block, and the second motor is respectively connected with the first screw rod and the second screw rod in a transmission way.

As a preferable technical scheme of the utility model, the first wire sleeve is fixedly arranged at two sides of the upper surface of the second installation block, the first wire sleeve is in threaded connection with the first screw rod, and the second installation block is in sliding connection with the first installation block.

As a preferable technical scheme of the utility model, the first motor is in transmission connection with the screw, the two ends of the transverse plate are fixedly provided with threaded sleeves, and the threaded sleeves are in threaded connection with the screw.

Compared with the prior art, the utility model provides the aviation accessory centering and punching tool for improving the centering precision and the punching rate, which has the following beneficial effects:

the utility model provides an aviation accessory centering punching tool for improving centering precision and punching speed, which is characterized in that a threaded sleeve which is arranged in a vertical plate and is in threaded connection with the surface of the threaded rod is fixedly arranged with a transverse plate, so that when a first motor is started to drive the threaded rod to rotate, the transverse plate drives a drill bit assembly to move downwards through a first mounting block and a second mounting block, and a driving mechanism of the drill bit assembly is started to drive the drill bit to rotate.

2. The utility model provides an aviation accessory centering punching tool capable of improving centering precision and punching speed, which is characterized in that a first installation block is fixedly installed on two sides below a transverse plate, a first screw rod is movably connected to the inside of the first installation block, a first screw sleeve is movably connected to the inside of the second installation block, a second screw rod is movably connected to the inside of the second installation block, and a second screw sleeve is fixedly installed with an installation seat, wherein the second screw sleeve is in threaded connection with the surface of the second screw rod, so that a drill bit assembly can move horizontally and forwards and backwards when a second motor is started to drive the first screw rod and the second screw rod to rotate, so that a plurality of aviation accessories can be conveniently punched, continuous punching can be performed without adjusting the aviation accessories, and punching efficiency is improved.

Drawings

FIG. 1 is a front view of the overall structure of the present utility model;

FIG. 2 is a schematic view of the structure of the first and second mounting blocks of the present utility model;

FIG. 3 is a schematic diagram of the internal structure of a second mounting block according to the present utility model;

FIG. 4 is a schematic diagram of the internal structure of the riser of the present utility model.

In the figure: 1. a base; 2. a vertical plate; 3. a first motor; 4. a cross plate; 5. a first mounting block; 6. a second mounting block; 7. a mounting base; 8. a fixing frame; 9. a drill bit assembly; 10. a fixed block; 11. a slide bar; 12. a return spring; 13. a limiting frame; 14. a fixing plate; 15. an electric telescopic rod; 16. a limiting plate; 17. a second motor; 18. a first screw rod; 19. a first wire sleeve; 20. a chute; 21. a second screw rod; 22. a second wire sleeve; 23. a screw; 24. a thread sleeve; 25. and (5) pressing the piece.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Referring to fig. 1 to 4, in the present embodiment: the aviation accessory centering and punching tool for improving centering precision and punching rate comprises a base 1, wherein a vertical plate 2 is fixedly arranged on one side of the upper surface of the base 1, a first motor 3 is fixedly arranged above the vertical plate 2, a transverse plate 4 is arranged on one side of the vertical plate 2, and the transverse plate 4 is arranged through the vertical plate 2; a first mounting block 5 is fixedly mounted below one side of the transverse plate 4, a second mounting block 6 is arranged below the first mounting block 5, a mounting seat 7 is arranged below the second mounting block 6, a fixing frame 8 is fixedly mounted below the mounting seat 7, a drill bit assembly 9 is fixedly mounted inside the fixing frame 8, and the drill bit assembly 9 is mounted through the fixing frame 8; the front surface of the vertical plate 2 is fixedly provided with a fixed block 10, a sliding rod 11 is fixedly arranged below the fixed block 10, the surface of the sliding rod 11 is sleeved with a reset spring 12, and the limit frame 13 can be reset through the reset spring 12; a limiting frame 13 is arranged below the drill bit assembly 9, a fixed plate 14 is fixedly arranged on one side of the front surface of the limiting frame 13, an electric telescopic rod 15 is fixedly arranged below one side surface of the vertical plate 2, a limiting plate 16 is fixedly arranged on one side of the electric telescopic rod 15, and aviation accessories are fixed through the limiting plate 16; a second motor 17 is fixedly arranged in one side of the first mounting block 5, a first screw rod 18 is movably connected in the first mounting block 5, a first screw sleeve 19 is fixedly arranged on one side of the upper surface of the second mounting block 6, a sliding groove 20 is fixedly arranged on the lower surface of the second mounting block 6, and the mounting seat 7 is mounted through the sliding groove 20; the inside swing joint of second installation piece 6 has second lead screw 21, and the surface threaded connection of second lead screw 21 has second silk cover 22, and the inside swing joint of riser 2 has screw rod 23, and the surface threaded connection of screw rod 23 has thread bush 24, and the fixed mounting of surface one side of second installation piece 6 has press piece 25.

In the embodiment, the vertical plates 2 are fixedly arranged on two sides of the upper surface of the base 1, the transverse plates 4 are connected between the vertical plates 2 in a sliding manner, the first mounting blocks 5 are fixedly arranged on two sides below the transverse plates 4, and the first mounting blocks 5 and the second mounting blocks 6 are arranged through the transverse plates 4; the fixing plates 14 are fixedly arranged on the two sides of the front surface and the two sides of the back surface of the limiting frame 13, the fixing plates 14 are in sliding connection with the sliding rods 11, the reset springs 12 are fixedly connected with the fixing plates 14, through holes are formed in the middle of the inside of the limiting frame 13, and aviation accessories are fixed through the limiting frame 13; two groups of fixing blocks 10 are fixedly arranged on the front surface and the back surface of the vertical plate 2, sliding rods 11 are fixedly connected between the fixing blocks 10, and the sliding rods 11 are arranged through the fixing blocks 10; a second motor 17 is fixedly arranged in one side of each of the first mounting block 5 and the second mounting block 6, the second motor 17 is respectively connected with a first screw rod 18 and a second screw rod 21 in a transmission way, and the second motor 17 drives the first screw rod 18 and the second screw rod 21 to rotate respectively; the first silk sleeves 19 are fixedly arranged on two sides of the upper surface of the second installation block 6, the first silk sleeves 19 are in threaded connection with the first screw rods 18, the second installation block 6 is in sliding connection with the first installation block 5, and the second installation block 6 is enabled to move through rotation of the first screw rods 18; the first motor 3 is in transmission connection with the screw rod 23, the threaded sleeves 24 are fixedly arranged at the two ends of the transverse plate 4, and the threaded sleeves 24 are in threaded connection with the screw rod 23.

The working principle and the using flow of the utility model are as follows: after the operator places aviation accessory on the surface of base 1, drive limiting plate 16 through starting electric telescopic handle 15 and remove and fix aviation accessory, drive drill bit pivoted through actuating mechanism that starts drill bit subassembly 9 and start first motor 3 and drive screw 23 rotation, and then make thread bush 24 drive drill bit downwardly moving through diaphragm 4, and make the push down and promote spacing 13 downwardly moving through the removal of second installation piece 6, and the fixed plate 14 of the both sides installation of spacing 13 slides and compresses reset spring 12 downwards on the surface of slide bar 11, and just can punch aviation accessory through the through-hole of spacing 13 through the rotation of drill bit, and can provide stable fixing for aviation accessory through spacing 13 cooperation limiting plate 16, thereby improve aviation accessory accuracy of punching, simultaneously because start second motor 17 can drive first lead screw 18 and second lead screw 21 respectively and rotate, and then make mount pad 7 can drive drill bit subassembly 9 and carry out horizontal and back-and-forth movement, thereby the equipment of being convenient for punches in many positions. And further effectively improves the punching efficiency.

Finally, it should be noted that: the foregoing description is only a preferred embodiment of the present utility model, and the present utility model is not limited thereto, but it is to be understood that modifications and equivalents of some of the technical features described in the foregoing embodiments may be made by those skilled in the art, although the present utility model has been described in detail with reference to the foregoing embodiments. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model should be included in the protection scope of the present utility model.

Claims

1. Aviation accessory centering and punching tool capable of improving centering precision and punching rate is characterized in that: including base (1), upper portion surface one side fixed mounting of base (1) has riser (2), the top fixed mounting of riser (2) has first motor (3), one side of riser (2) is provided with diaphragm (4), one side below fixed mounting of diaphragm (4) has first installation piece (5), the below of first installation piece (5) is provided with second installation piece (6), the below of second installation piece (6) is provided with mount pad (7), the below fixed mounting of mount pad (7) has mount (8), the inside fixed mounting of mount pad (8) has drill bit subassembly (9), the front surface fixed mounting of riser (2) has fixed block (10), the below fixed mounting of fixed block (10) has slide bar (11), the surface socket joint has reset spring (12) of one side below of diaphragm (4), the below of drill bit subassembly (9) is provided with spacing (13), the below fixed mounting of electrical drive motor (15) of one side (14) of spacing frame (13), the fixed mounting of electrical drive motor (15) has one side (15) of expansion link (15), the inside swing joint of first installation piece (5) has first lead screw (18), upper portion surface one side fixed mounting of second installation piece (6) has first silk cover (19), the below fixed surface of second installation piece (6) installs spout (20), the inside swing joint of second installation piece (6) has second lead screw (21), the surface threaded connection of second lead screw (21) has second silk cover (22), the inside swing joint of riser (2) has screw rod (23), the surface threaded connection of screw rod (23) has thread bush (24), surface one side fixed mounting of second installation piece (6) has presser (25).

2. The aviation accessory centering and punching tool for improving centering accuracy and punching rate according to claim 1, wherein the centering and punching tool is characterized in that: the vertical plates (2) are fixedly mounted on two sides of the upper surface of the base (1), the transverse plates (4) are slidably connected between the vertical plates (2), and the first mounting blocks (5) are fixedly mounted on two sides of the lower portion of the transverse plates (4).

3. The aviation accessory centering and punching tool for improving centering accuracy and punching rate according to claim 1, wherein the centering and punching tool is characterized in that: the limiting frame is characterized in that fixing plates (14) are fixedly arranged on the two sides of the front face and the two sides of the back face of the limiting frame (13), the fixing plates (14) are in sliding connection with the sliding rods (11), the reset springs (12) are fixedly connected with the fixing plates (14), and through holes are formed in the middle of the inside of the limiting frame (13).

4. The aviation accessory centering and punching tool for improving centering accuracy and punching rate according to claim 1, wherein the centering and punching tool is characterized in that: two groups of fixing blocks (10) are fixedly arranged on the front surface and the back surface of the vertical plate (2), and the sliding rod (11) is fixedly connected between the fixing blocks (10).

5. The aviation accessory centering and punching tool for improving centering accuracy and punching rate according to claim 1, wherein the centering and punching tool is characterized in that: a second motor (17) is fixedly arranged inside one side of each of the first mounting block (5) and the second mounting block (6), and the second motor (17) is respectively in transmission connection with the first screw rod (18) and the second screw rod (21).

6. The aviation accessory centering and punching tool for improving centering accuracy and punching rate according to claim 1, wherein the centering and punching tool is characterized in that: the first silk sleeve (19) is fixedly arranged on two sides of the upper surface of the second installation block (6), the first silk sleeve (19) is in threaded connection with the first screw rod (18), and the second installation block (6) is in sliding connection with the first installation block (5).

7. The aviation accessory centering and punching tool for improving centering accuracy and punching rate according to claim 1, wherein the centering and punching tool is characterized in that: the first motor (3) is in transmission connection with the screw rod (23), threaded sleeves (24) are fixedly arranged at two ends of the transverse plate (4), and the threaded sleeves (24) are in threaded connection with the screw rod (23).