CN215237144U

CN215237144U - Perforating device is used in manufacturing of high efficiency space flight material

Info

Publication number: CN215237144U
Application number: CN202120953641.4U
Authority: CN
Inventors: 李国栋
Original assignee: Xuzhou Naying Information Technology Co ltd
Current assignee: Xuzhou Naying Information Technology Co ltd
Priority date: 2021-05-07
Filing date: 2021-05-07
Publication date: 2021-12-21
Anticipated expiration: 2031-05-07

Abstract

The utility model discloses a high-efficiency punching device for manufacturing aerospace materials, which belongs to the technical field of aerospace, and comprises supporting legs, wherein the top ends of the supporting legs are fixedly connected with a processing table, the surface of the processing table is provided with a controller, the upper surface of the processing table is embedded and connected with a rotator and a scrap collecting box, the power output end of the rotator is matched and connected with an electric telescopic fixing rod, the top ends of the electric telescopic fixing rod are fixedly connected with a fixing top plate, the lower surface of the fixing top plate is provided with a sliding rail, and the surface of the sliding rail is slidably connected with a slider. Avoid causing a skilled worker's environment dirty and disorderly poor, conveniently punch.

Description

Perforating device is used in manufacturing of high efficiency space flight material

Technical Field

The utility model relates to an aerospace technical field especially relates to a perforating device is used in manufacturing of high efficiency space flight material.

Background

At present to aerospace material, need punch the processing, usually, constructor is handheld puncher and punches, and workman intensity of labour is big, wastes time and energy, and the surface unevenness after punching, and the effect of punching is poor, and the precision of punching is poor. The prior art discloses the application numbers as follows: CN201520906670. X's a special perforating device of aerospace material, including the puncher with be used for supporting the base of L type frame, base fixedly connected with leans on the platform, it is equipped with the arcwall face to lean on the platform, the arcwall face is conflict setting with curved section, the base is the spacing part of fixedly connected with still, spacing part is conflict setting with the montant, but this prior art often carries out during aerospace material drilling, and manual control is difficult to in time stop, and the hole surpasss predetermined size easily.

Patent number CN201922161529.2 discloses a special perforating device of aerospace material, relates to the aerospace field. The special perforating device for the aerospace material comprises a perforating box, wherein the outside of the perforating box comprises a support column and a rotating shaft, the top end of the support column is movably connected with the lower part of the perforating box, and the upper part of the rotating shaft is movably connected with the bottom end of the support column. This special perforating device of aerospace material, box of punching through setting up, and the pillar, the apparatus further comprises a rotating shaft, a pedestal, the cooperation setting of screw hole and first nut, thereby place through the base that sets up during the messenger uses, and go on through setting up at the inside screw hole of base and fix the base with ground, thereby it carries out rotation angle to make through the pivot that sets up, and carry out fixed equipment at the pillar that the pivot top was fixed through setting up, fix through the box of punching that sets up and the first nut that sets up, and rotatory box of punching carries out work, the effect of fixing perforating device has been reached.

The special perforating device for aerospace materials in the technology has the following defects: 1. the device is inconvenient to adjust the punching position of the aerospace material during punching, and punching is performed regardless of manually adjusting the position of the aerospace material, so that the punching efficiency is reduced; 2. the device can not collect the recovery to the sweeps that punches the hole and produce when using, causes the environment of punching dirty and disorderly, for punching cause the hindrance, reduces the efficiency of punching, for this reason, we provide a perforating device for high efficiency aerospace material manufacturing.

SUMMERY OF THE UTILITY MODEL

The utility model provides a perforating device is used in manufacturing of high efficiency space flight material can the automatically regulated space flight material foraminiferous position and angle when punching after fixing space flight material, does not need the manual work to adjust, and it is laborsaving to save trouble, effectively improves punching efficiency, and can retrieve the waste material that produces when punching, avoids causing a skilled worker's environment dirty in disorder poor, conveniently punches.

The utility model provides a specific technical scheme as follows:

the utility model provides a pair of perforating device is used in manufacturing of high efficiency aerospace material, including supporting leg, fixed plate and solid fixed splint, supporting leg top fixedly connected with processing platform, processing platform surface mounting has the controller, processing platform upper surface is inlayed and is connected with and rotates ware and sweeps collecting box, it is connected with electronic flexible dead lever to rotate the cooperation of ware power take off end, electronic flexible dead lever top fixedly connected with fixed roof, fixed roof surface mounting has the slide rail under the fixed roof, slide rail sliding surface is connected with the slider, the slider bottom can be dismantled and be connected with the hole puncher, processing platform upper surface mounting has the mount, and the mount has a plurality ofly.

Optionally, the fixed frame comprises a fixed plate, a driver and a fixed clamping plate, the driver is embedded and connected to the outer side wall of the fixed plate, and the fixed clamping plate is fixedly connected to the power output end of the driver.

Optionally, a material pusher is inlaid in the left side wall of the scrap collecting box, and a cleaning opening is formed in the right side wall of the scrap collecting box.

Optionally, the bottom end of the fixing plate is fixedly connected with the processing table, and the clamping position of the fixing clamping plate is provided with an anti-slip pad.

Optionally, a sealing cover is mounted on the surface of the cleaning opening.

Optionally, the rotator, the electric telescopic fixing rod, the slider, the puncher, the driver and the material pusher are electrically connected with the controller through wires, and the controller is electrically connected with an external power supply through wires.

The utility model has the advantages as follows:

the embodiment of the utility model provides a perforating device is used in manufacturing of high efficiency space flight material:

1. the upper surface of the processing table is provided with a plurality of fixing frames, each fixing frame is composed of a fixing plate, a driver and a fixing splint, the fixing frames are fixed on the upper surface of the processing table through the fixing plates, during punching, the aerospace materials are placed between the fixing frames, the aerospace materials are clamped through the fixing splints, the sliders drive the puncher to move on the fixing top plate through the slide rails, the electric telescopic fixing rods are driven to rotate through the rotators, the fixing top plate can move along with the electric telescopic fixing rods, the angle of the puncher can be indirectly adjusted, the puncher can be conveniently and quickly positioned, the puncher is driven to move downwards through the electric telescopic fixing rods to punch the aerospace materials on the fixing frames, meanwhile, the fixing splints can be driven to rotate through the drivers, the aerospace materials can be driven to rotate through the rotation of the fixing splints, the punching position of the aerospace materials can be quickly adjusted, manual adjustment is not needed, effectively improve the efficiency of punching.

2. Processing platform upper surface internally mounted has the sweeps collecting box, and the sweeps collecting box is located mount inside wall low tube, can produce the sweeps when punching, the sweeps can drop into inside the sweeps collecting box, the sweeps that can effectively will punch the production through the sweeps collecting box is collected, can not cause the processing platform surface to be mixed and disorderly poor, simultaneously the clearance mouth is installed to sweeps collecting box right side wall, the left side wall is inlayed and is had the stoker, when the sweeps of the inside collection of sweeps collecting box is too much, open the closing cap on clearance mouth surface, the power of stoker is put through to the rethread controller, the stoker circular telegram promotes forward, can effectively push the sweeps to the clearance mouth, can clear up the sweeps out through the clearance mouth and recycle, can reduce the cost of production, also can not influence the result of use of sweeps collecting box, and is convenient to use, and the machining efficiency is improved.

Drawings

In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without creative efforts.

Fig. 1 is a schematic overall structure diagram of a punching device for manufacturing high-efficiency aerospace materials according to an embodiment of the present invention;

fig. 2 is a schematic structural view of a fixing frame of the punching device for manufacturing high-efficiency aerospace materials according to the embodiment of the present invention;

fig. 3 is the utility model discloses a structural schematic diagram of high efficiency aerospace perforating device's flying saucer collecting box for material manufacturing.

In the figure: 1. supporting legs; 2. a processing table; 3. a controller; 4. a rotator; 5. an electric telescopic fixing rod; 6. fixing a top plate; 7. a slide rail; 8. a slider; 9. a hole puncher; 10. a fixed mount; 11. a scrap collecting box; 12. a fixing plate; 13. a driver; 14. fixing the clamping plate; 15. a pusher; 16. and cleaning the opening.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention clearer, the present invention will be described in further detail with reference to the accompanying drawings, 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 efforts belong to the protection scope of the present invention.

The following describes in detail a high-efficiency punching device for manufacturing aerospace materials according to an embodiment of the present invention with reference to fig. 1 to 3.

Referring to fig. 1-3, the embodiment of the utility model provides a pair of high efficiency perforating device for aerospace material manufacturing, including supporting leg 1, fixed plate 12 and solid fixed

splint

14, 1 top fixedly connected with processing platform 2 of supporting leg, 2 surface mounting on processing platform have

controller

3, 2 upper surfaces of processing platform are inlayed and are connected with rotor 4 and sweeps collecting box 11, the cooperation of 4 power take off ends of rotor is connected with electronic flexible dead lever 5, 5 top fixedly connected with roof 6 of electronic flexible dead lever, 6 lower surface mounting on the roof has

slide rail

7, and 7 surface sliding connections on slide rail have slider 8, slider 8 bottom can be dismantled and be connected with

hole puncher

9, 3 upper surface mounting on the processing platform has mount 10, and mount 10 has a plurality ofly.

The example, punch the time spent to the space flight material after fixed and mutually support foraminiferous position and the angle that can automatically regulated space flight material through rotating ware 4, electronic flexible dead lever 5, fixed roof 6 and mount 10, do not need the manual work to adjust, it is laborsaving to save trouble, effectively improves punching efficiency, and can retrieve the waste material that produces when punching through sweeps collecting box 11, avoids causing a skilled worker's environment dirty in disorder poor, conveniently punches.

Referring to fig. 2, the fixing frame 10 is composed of a fixing plate 12, a driver 13 and a fixing clamp plate 14, wherein the driver 13 is embedded and connected to the outer side wall of the fixing plate 12, and the fixing clamp plate 14 is fixedly connected to the power output end of the driver 15.

The fixed clamping plate 14 can be driven to rotate through the driver 13, the aerospace material can be driven to rotate through rotation of the fixed clamping plate 14, the punching position of the aerospace material can be adjusted rapidly, manual adjustment is not needed, and punching efficiency is effectively improved.

Referring to fig. 3, a pusher 15 is embedded in the left side wall of the scrap collecting box 11, and a cleaning opening 16 is formed in the right side wall of the scrap collecting box 11.

The example, when the sweeps of the inside collection of sweeps collecting box 11 is too much, open the closing cap on clearance mouth 16 surface, rethread controller 3 switch-on stoker 15's power, stoker 15 circular telegram promotes forward, can effectively push the sweeps to clearance mouth 16, can clear up the sweeps out through clearance mouth 16 and recycle, can reduce the manufacturing cost, also can not influence the result of use of sweeps collecting box 11, conveniently use, improve machining efficiency.

Referring to fig. 1 and 2, the bottom end of the fixing plate 12 is fixedly connected to the processing table 2, and a non-slip mat is disposed at the clamping position of the fixing clamp plate 14.

By way of example, the fixing frame 10 is conveniently fixed on the surface 2 of the processing table through the fixing plate 12, the phenomenon that the fixing clamping plate 14 slides when clamping aerospace materials can be avoided through the anti-slip pad, the clamping stability is improved, and punching is convenient.

Referring to fig. 3, the cleaning port 16 is surface mounted with a cover.

The cleaning opening can be sealed through the sealing cover, waste is collected and prevented from falling from the waste collection and collection box 11, and collection is convenient.

Referring to fig. 1 to 3, the rotator 4, the electric telescopic fixing rod 5, the slider 5, the puncher 9, the driver 13 and the material pusher 15 are all electrically connected to the controller 3 through wires, and the controller 3 is electrically connected to an external power source through wires.

The electric conduction speed is high, the service life is long, the controller 3 conveniently controls the rotator 4, the electric telescopic fixing rod 5, the slider 5, the puncher 9, the driver 13 and the material pushing device 15 through the wires, and an external power source conveniently provides power for the controller 3 through the wires, so that the electric conduction device is convenient to use.

When the device is used, a processing table 2 is stably placed on the ground through supporting legs 1, a plurality of fixing frames 10 are arranged on the upper surface of the processing table 2, each fixing frame 10 consists of a fixing plate 12, a driver 13 and a fixing clamp plate 14, each fixing frame 10 is fixed on the upper surface of the processing table 2 through the corresponding fixing plate 12, an aerospace material is placed between the corresponding fixing frames 10 during punching, the aerospace material is clamped through the corresponding fixing clamp plate 14, a slider 8 drives a puncher 9 to move on a fixed top plate 6 through a sliding rail 7, a rotator 4 can drive an electric telescopic fixing rod 5 to rotate, the fixed top plate 6 can move along with the electric telescopic fixing rod 5, the angle of the puncher 9 can be indirectly adjusted, the puncher 9 can be conveniently and rapidly positioned, the puncher 9 is driven to move downwards through the electric telescopic fixing rod 5 to punch the aerospace material on the corresponding fixing frame 10, and the fixing clamp plates 14 can be driven to rotate through the driver 13, the aerospace material can be driven to rotate through the rotation of the fixed clamping plate 14, the punching position of the aerospace material can be quickly adjusted, manual adjustment is not needed, the punching efficiency is effectively improved, the scrap collecting box 11 is arranged in the upper surface of the processing table 2, the scrap collecting box 11 is positioned in the lower pipe of the inner side wall of the fixed frame 10, scraps can be generated during punching, the scraps can fall into the scrap collecting box 11, the scraps generated by punching can be effectively collected through the scrap collecting box 11, the surface disorder of the processing table 2 cannot be caused, meanwhile, a cleaning port 16 is arranged on the right side wall of the scrap collecting box 11, a material pusher 15 is embedded in the left side wall, when too many scraps are collected in the scrap collecting box 11, a sealing cover on the surface of the cleaning port 16 is opened, the controller 3 is connected with a power supply of the material pusher 15, the material pusher 15 is electrically pushed forwards, the scraps can be effectively pushed to the cleaning port 16, the scraps can be cleaned out through the cleaning port 16 for recycling, not only can reduce the production cost, but also can not influence the use effect of the sweeps collecting box 11, is convenient to use and improves the processing efficiency.

The utility model relates to a high-efficiency punching device for aerospace material manufacture, which comprises a support leg 1; 2. a processing table; 3. a controller; 4. a rotator; 5. an electric telescopic fixing rod; 6. fixing a top plate; 7. a slide rail; 8. a slider; 9. a hole puncher; 10. a fixed mount; 11. a scrap collecting box; 12. a fixing plate; 13. a driver; 14. fixing the clamping plate; 15. a pusher; 16. the cleaning ports and the components are all standard or known to those skilled in the art, and the structure and principle thereof are known to those skilled in the art through technical manuals or through routine experimentation.

It is apparent that those skilled in the art can make various changes and modifications to the embodiments of the present invention without departing from the spirit and scope of the embodiments of the present invention. Thus, if such modifications and variations of the embodiments of the present invention fall within the scope of the claims and their equivalents, the present invention is also intended to include such modifications and variations.

Claims

1. The punching device for manufacturing the high-efficiency aerospace material comprises supporting legs (1), a fixing plate (12) and a fixing clamp plate (14), and is characterized in that the top ends of the supporting legs (1) are fixedly connected with a processing table (2), the surface of the processing table (2) is provided with a controller (3), the upper surface of the processing table (2) is connected with a rotator (4) and a scrap collecting box (11) in an embedded manner, the power output end of the rotator (4) is connected with an electric telescopic fixing rod (5) in a matched manner, the top end of the electric telescopic fixing rod (5) is fixedly connected with a fixing top plate (6), the lower surface of the fixing top plate (6) is provided with a sliding rail (7), the surface of the sliding rail (7) is connected with a slider (8) in a sliding manner, the bottom end of the slider (8) is detachably connected with a puncher (9), the upper surface of the processing table (2) is provided with a fixing frame (10), and a plurality of fixing frames (10) are provided.

2. The high-efficiency perforating device for aerospace material manufacturing of claim 1, wherein the fixing frame (10) is composed of a fixing plate (12), a driver (13) and a fixing clamp plate (14), the driver (13) is embedded and connected to the outer side wall of the fixing plate (12), and the fixing clamp plate (14) is fixedly connected to the power output end of the driver (13).

3. The high-efficiency perforating device for aerospace material manufacturing of claim 1, wherein the left side wall of the scrap collecting box (11) is embedded with a pusher (15), and the right side wall of the scrap collecting box (11) is provided with a cleaning opening (16).

4. The high-efficiency perforating device for aerospace material manufacturing of claim 1, wherein the bottom end of the fixing plate (12) is fixedly connected with the processing table (2), and the clamping position of the fixing clamping plate (14) is provided with a non-slip mat.

5. A high efficiency perforating device for aerospace material manufacture as claimed in claim 3, wherein said cleaning port (16) is surface mounted with a cover.

6. The high-efficiency punching device for aerospace material manufacturing of claim 1, wherein the rotator (4), the electric telescopic fixing rod (5), the slider (8), the puncher (9), the driver (13) and the pusher (15) are all electrically connected with the controller (3) through wires, and the controller (3) is electrically connected with an external power supply through wires.