CN211890527U

CN211890527U - Clamping structure for production and processing of aircraft parts

Info

Publication number: CN211890527U
Application number: CN202020258432.3U
Authority: CN
Inventors: 崔晓智
Original assignee: Tianjin Feiyue Aviation Parts Surface Treatment Co ltd
Current assignee: Tianjin Feiyue Aviation Parts Surface Treatment Co ltd
Priority date: 2020-03-05
Filing date: 2020-03-05
Publication date: 2020-11-10
Anticipated expiration: 2030-03-05

Abstract

The utility model discloses a clamping structure is used in aircraft parts production and processing, comprising a base plate, the first installation piece of bottom plate top fixedly connected with, the one end fixedly connected with second installation piece of first installation piece is kept away from at the bottom plate top, first installation piece is close to second installation piece one side fixedly connected with erection column, the erection column is close to second installation piece one side fixedly connected with mounting disc, second installation piece lateral wall is inserted and is equipped with the rack, the rack is close to erection column one side fixedly connected with removal dish, the vertical board of bottom plate top fixedly connected with, it is equipped with the connecting gear to insert between the vertical board, connect the wheel and rack and rotate, it runs through vertical board to connect the gear, has solved and has screwed the bolt and just can fix, screws complex operation, and low efficiency influences work efficiency, inconvenient very little problem.

Description

Clamping structure for production and processing of aircraft parts

Technical Field

The utility model relates to a clamping structure technical field specifically is a clamping structure is used in aircraft parts production and processing.

Background

The screw tap belongs to one of parts of an airplane, and a clamp is required to be used for fixing a workpiece to be machined in the production and machining process of the screw tap.

Among the prior art, a fixed clamp is used in processing of screw tap holder with bulletin number CN208427642U, which comprises an installation base, grip block and positioning screw, positioning screw and helicla flute spiral fixed mounting, the installation end of grip block is through rotating seat and positioning screw tip fixed connection, the relative fixed mounting in grip block bottom has supplementary grip block and supplementary lagging, positioning screw's end corresponds the helicla flute and has the stopper through the positioning screw spiral installation, the stopper is offered the meshing fluted disc that is the salient structure with the relative terminal surface of locating plate, the locating plate corresponds the meshing fluted disc and offers the meshing tooth's socket that corresponds with the meshing fluted disc.

However, the device still has the following obvious defect in the using process, workers can fix the device only by screwing the bolts, the screwing operation is complex and complicated, the efficiency is low, the working efficiency is influenced, and the device is very inconvenient.

Therefore, the utility model provides an aircraft spare part is clamping structure for production and processing.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an aircraft spare part clamping structure for production and processing 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: a clamping structure for producing and processing aircraft parts comprises a bottom plate, a first mounting block is fixedly connected to the top of the bottom plate, one end of the top of the bottom plate, which is far away from the first mounting block, is fixedly connected with a second mounting block, one side of the first mounting block, which is close to the second mounting block, is fixedly connected with a mounting column, a mounting disc is fixedly connected to one side of the mounting column close to the second mounting block, a rack is inserted into the side wall of the second mounting block, one side of the rack close to the mounting column is fixedly connected with a movable plate, the top of the bottom plate is fixedly connected with a vertical plate, a connecting gear is inserted between the vertical plates and rotates with the rack, the connecting gear penetrates through the vertical plates, the connecting gear is characterized in that a moving rod is fixedly connected to the side wall of the connecting gear, a heavy object box is fixedly connected to one end, far away from the connecting gear, of the top of the moving rod, and the mounting disc is identical to the central axis of the moving disc.

Through adopting above-mentioned technical scheme, during the use, place the article between mounting disc and removal dish, to adding the weight in the heavy object box, alright press from both sides tight article, solved and need screwed the bolt just can fix, screw complex operation, it is complicated, and the inefficiency influences work efficiency, very inconvenient problem.

Preferably, one side of the rack, which is far away from the movable plate, is fixedly connected with a limiting plate, and the limiting plate is perpendicular to the rack.

Through adopting above-mentioned technical scheme, through setting up the limiting plate, prevent that the rack from deviating from.

Preferably, a buffer pad is fixedly connected to one side of the mounting disc, which is close to the movable disc, and the central axis of the buffer pad is the same as the central axis of the movable disc.

Through adopting above-mentioned technical scheme, through setting up the blotter, prevent that the article from pressing from both sides the back wearing and tearing mounting disc.

Preferably, a cleaning valve is fixedly connected to the bottom of the weight box, and the cleaning valve extends into the weight box.

By adopting the technical scheme, the cleaning valve is arranged, so that dirt falling in the weight box can be cleaned conveniently.

Preferably, one end, far away from the moving rod, of the weight box is fixedly connected with a handle, and a rubber sleeve fixedly connected with the handle is sleeved on the side wall of the handle.

Through adopting above-mentioned technical scheme, through setting up the handle, be convenient for lift up the article of taking of heavy object box.

Preferably, a friction pad is fixedly connected to the bottom of the bottom plate, and the friction pad is parallel to the bottom plate.

Through adopting above-mentioned technical scheme, through setting up the friction pad, prevent that the fuselage from sliding.

Compared with the prior art, the beneficial effects of the utility model are that: during the use, place the article between mounting disc and removal dish, add the weight in to the heavy object box, alright press from both sides tight article, it can fix to have solved the bolt that needs to screw, the complex operation of screwing, it is complicated, and low efficiency influences work efficiency, very inconvenient problem, through setting up the limiting plate, prevent that the rack from deviating from, through setting up the blotter, prevent that the article from pressing from both sides tight back wearing and tearing mounting disc, through setting up clean valve, be convenient for clean the filth that drops in the heavy object box, through setting up the handle, be convenient for lift the heavy object box article of taking, through setting up the friction pad, prevent that the fuselage from sliding, the practicality is very strong, be very worth.

Drawings

Fig. 1 is a schematic external structural view of the present invention;

fig. 2 is a schematic side structure view of the present invention;

fig. 3 is a schematic bottom structure diagram of the present invention.

In the figure: 1. a base plate; 2. a second mounting block; 3. a first mounting block; 4. mounting a column; 5. mounting a disc; 6. a rack; 7. a movable tray; 8. a vertical plate; 9. a connecting gear; 10. a travel bar; 11. a weight box; 12. a handle; 13. a rubber sleeve; 14. cleaning the valve; 15. a limiting plate; 16. a cushion pad; 17. a friction pad.

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.

Referring to fig. 1 to 3, the present invention provides a technical solution:

a clamping structure for producing and processing aircraft parts comprises a bottom plate 1, wherein the top of the bottom plate 1 is fixedly connected with a first installation block 3, one end of the top of the bottom plate 1, which is far away from the first installation block 3, is fixedly connected with a second installation block 2, one side of the first installation block 3, which is close to the second installation block 2, is fixedly connected with an installation column 4, one side of the installation column 4, which is close to the second installation block 2, is fixedly connected with an installation disc 5, a rack 6 is inserted in the side wall of the second installation block 2, one side of the rack 6, which is close to the installation column 4, is fixedly connected with a moving disc 7 for clamping objects, the top of the bottom plate 1 is fixedly connected with a vertical plate 8, a connecting gear 9 is inserted between the vertical plates 8, the connecting gear 9 rotates with the rack 6, the connecting gear 9 penetrates through the vertical plate 8 and is used for installing the connecting gear 9, the side wall of the connecting gear 9 is fixedly, for placing heavy objects, the mounting plate 5 has the same central axis as the moving plate 7.

Rack 6 is far away from 7 one side fixedly connected with limiting plate 15 of removal dish, limiting plate 15 perpendicular to rack 6, mounting disc 5 is close to 7 one side fixedly connected with blotter 16 of removal dish, through setting up blotter 16, prevent that the article from pressing from both sides tight back wearing and tearing mounting disc 5, increase of service life, blotter 16 is the same with removal dish 7 the central axis, heavy object box 11 bottom fixedly connected with cleaning valve 14, through setting up cleaning valve 14, be convenient for clean the filth that falls in heavy object box 11, reduce the cleaning difficulty, cleaning valve 14 extends to in the heavy object box 11, the heavy object box 11 is kept away from 10 one end fixedly connected with handles 12 of carriage release lever, handle 12 lateral wall cover is equipped with rubber sleeve 13 rather than fixed connection, 1 bottom fixedly connected with friction pad 17 of.

The working principle is as follows: during the use, place the article between mounting disc 5 and removal dish 7, add the weight in to heavy object box 11, alright press from both sides tight article, it just can fix to have solved the bolt that needs to screw, the complex operation of screwing, it is complicated, and low efficiency influences work efficiency, very inconvenient problem, through setting up limiting plate 15, prevent that rack 6 from deviating from, through setting up blotter 16, prevent that the article from pressing from both sides tight back wearing and tearing mounting disc 5, through setting up clean valve 14, be convenient for clean the filth that falls in heavy object box 11, through setting up handle 12, be convenient for lift up heavy object box 11 and take the article, through setting up friction pad 17, prevent that the fuselage from sliding, the practicality is very strong, be worth promoting very much.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an aircraft spare part is clamping structure for production and processing, includes bottom plate (1), its characterized in that: the top of the bottom plate (1) is fixedly connected with a first installation block (3), one end, far away from the first installation block (3), of the top of the bottom plate (1) is fixedly connected with a second installation block (2), one side, close to the second installation block (2), of the first installation block (3) is fixedly connected with an installation column (4), one side, close to the second installation block (2), of the installation column (4) is fixedly connected with an installation disc (5), a rack (6) is inserted into the side wall of the second installation block (2), one side, close to the installation column (4), of the rack (6) is fixedly connected with a moving disc (7), the top of the bottom plate (1) is fixedly connected with vertical plates (8), a connecting gear (9) is inserted between the vertical plates (8), the connecting gear (9) rotates with the rack (6), the connecting gear (9) penetrates through the vertical plates (8), and the side wall of the connecting gear (9) is fixedly connected with a moving rod, one end, far away from the connecting gear (9), of the top of the moving rod (10) is fixedly connected with a weight box (11), and the central axis of the mounting disc (5) is the same as that of the moving disc (7).

2. The clamping structure for producing and processing the aircraft component as claimed in claim 1, wherein: one side, far away from the moving disc (7), of the rack (6) is fixedly connected with a limiting plate (15), and the limiting plate (15) is perpendicular to the rack (6).

3. The clamping structure for producing and processing the aircraft component as claimed in claim 1, wherein: a buffer pad (16) is fixedly connected to one side, close to the movable disc (7), of the mounting disc (5), and the central axis of the buffer pad (16) is the same as that of the movable disc (7).

4. The clamping structure for producing and processing the aircraft component as claimed in claim 1, wherein: the bottom of the weight box (11) is fixedly connected with a cleaning valve (14), and the cleaning valve (14) extends into the weight box (11).

5. The clamping structure for producing and processing the aircraft component as claimed in claim 1, wherein: one end, far away from the moving rod (10), of the weight box (11) is fixedly connected with a handle (12), and a rubber sleeve (13) fixedly connected with the handle is sleeved on the side wall of the handle (12).

6. The clamping structure for producing and processing the aircraft component as claimed in claim 1, wherein: the bottom of the bottom plate (1) is fixedly connected with a friction pad (17), and the friction pad (17) is parallel to the bottom plate (1).