阅读说明：本技术 一种航空航天材料打孔机 (Aerospace material puncher ) 是由 不公告发明人 于 2018-06-22 设计创作，主要内容包括：本发明提供一种航空航天材料打孔机,涉及航空航天技术领域。该航空航天材料打孔机,包括底座,底座的底部四角均固定连接有支撑脚,底座的顶部四角均固定连接有支撑杆,支撑杆的顶部固定连接有横梁,横梁的顶部固定连接有控制箱,控制箱的正面固定连接有操作面板,横梁的底部固定连接有滑轨,滑轨的底部滑动连接有打孔装置,打孔装置的底部固定安装有打孔头。该航空航天材料打孔机,设置有板型材料固定装置和圆筒型材料固定装置,可以分别对板型航空航天材料和圆筒型航空航天材料进行固定,使材料打孔的时候更加稳固,避免材料移位造成打孔误差,圆型材料固定装置可以根据需要取下,避免板型材料打孔的时候不方便。(The invention provides an aerospace material perforating machine, and relates to the technical field of aerospace. This aerospace material puncher, including the base, the equal fixedly connected with supporting legs in the bottom four corners of base, the equal fixedly connected with bracing piece in the top four corners of base, the top fixedly connected with crossbeam of bracing piece, the top fixedly connected with control box of crossbeam, the positive fixedly connected with operating panel of control box, the bottom fixedly connected with slide rail of crossbeam, the bottom sliding connection of slide rail has perforating device, perforating device's bottom fixed mounting has the head of punching. This aerospace material puncher is provided with board type material fixing device and drum type material fixing device, can fix board type aerospace material and drum type aerospace material respectively, and is more firm when making the material punch, avoids the material to shift and causes the error of punching, and round material fixing device can take off as required, and is inconvenient when avoiding board type material to punch.)

1. The utility model provides an aerospace material puncher, includes base (1), the equal fixedly connected with supporting legs in bottom four corners (2) of base (1), the equal fixedly connected with bracing piece in top four corners (3) of base (1), the top fixedly connected with crossbeam (4) of bracing piece (3), the top fixedly connected with control box (5) of crossbeam (4), the positive fixedly connected with operating panel (6) of control box (5), the bottom fixedly connected with slide rail (7) of crossbeam (4), the bottom sliding connection of slide rail (7) has perforating device (8), the bottom fixed mounting of perforating device (8) has perforating head (9), its characterized in that: the top of the base (1) is movably connected with two movable plates (10) through hinges; the top of the base (1) is fixedly connected with a lower pressing plate (13) on the side of the supporting rod (3), the side of the supporting rod (3) is fixedly connected with an adjusting platform (14) on the upper side of the lower pressing plate (13), an adjusting bolt (15) is movably inserted in the adjusting platform (14), two ends of the adjusting bolt (15) penetrate through the adjusting platform (14) and respectively extend to the upper side and the lower side of the adjusting platform (14), one end of the adjusting bolt (15) extending to the lower side of the adjusting platform (14) is fixedly connected with an upper pressing plate (16), one end of the adjusting bolt (15) extending to the upper side of the adjusting platform (14) is fixedly sleeved with an adjusting handle (17), a lead screw (18) is movably inserted in the inner part of the movable plate (10), two ends of the lead screw (18) both penetrate through the movable plate (10) and respectively extend to the front side and the rear side of the movable plate (10), the clamping plate (19) is fixedly connected to one end, extending to the rear side of the movable plate (10), of the screw rod (18), and a rotating handle (20) is fixedly sleeved on the surface of one end, extending to the front side of the movable plate (10), of the screw rod (18).

2. An aerospace material punch, according to claim 1, wherein: the inner wall bottom fixed mounting of control box (5) has battery (11), the inner wall bottom of control box (5) and the right side fixed mounting who is located battery (11) have controller (12).

3. An aerospace material punch, according to claim 1, wherein: the bottom of the upper pressing plate (16), the top of the lower pressing plate (13) and the side face of the clamping plate (19) are all bonded with anti-skidding pads (25), and one side of the movable plate (10) is in lap joint with the surface of the supporting rod (3).

4. An aerospace material punch, according to claim 1, wherein: the other side of the movable plate (10) is fixedly connected with a clamping seat (21), and one side of the support rod (3) close to the movable plate (10) is fixedly connected with a rotating seat (22).

5. An aerospace material punch, according to claim 4, wherein: one side of the rotating base (22) far away from the supporting rod (3) is movably connected with a rotating plate (23) through a rotating shaft, and the bottom of the rotating plate (23) is in lap joint with the top of the clamping base (21).

6. An aerospace material punch, according to claim 1, wherein: a thread groove (24) is formed in the adjusting platform (14), and the surface of the adjusting bolt (15) is in threaded connection with the surface of the thread groove (24).

Technical Field

The invention relates to the technical field of aerospace, in particular to an aerospace material punching machine.

Background

The aerospace technology relates to the profound academic operations such as human resource allocation, equipment and instrument matching, installation and use, is a high pursuit of the development of the nation, the nation and the whole human, enables the civilization of the human to enter a three-dimensional era, is the flight activity in the atmosphere, is the comprehensive high technology, is the key point of the material technology on the basis of theory and design, is the soul of the electronic technology, and often needs a punching machine to punch during the manufacturing and processing process of aerospace materials.

For example, the Chinese patent discloses 'a novel aerospace material laser drilling machine adopting magnetic levitation technology' (patent number: 201721223105.9), which comprises a control console, wherein a power supply is arranged below the control console, one side of the power supply is provided with a motor, and one side of the motor is provided with four support frames in number. The problem that traditional laser-beam drilling machine is slow in moving speed and not suitable for drilling aerospace materials due to insufficient drilling accuracy is solved, but the laser-beam drilling machine is only suitable for drilling plate-type materials and is not suitable for cylindrical or cylindrical aerospace materials.

Disclosure of Invention

Technical problem to be solved

Aiming at the defects of the prior art, the invention provides the aerospace material punching machine, which solves the problems that the laser punching machine is only suitable for punching of plate-type materials and is not suitable for cylindrical or cylindrical aerospace materials.

(II) technical scheme

In order to achieve the purpose, the invention is realized by the following technical scheme: the utility model provides an aerospace material puncher, includes the base, the equal fixedly connected with supporting legs in bottom four corners of base, the equal fixedly connected with bracing piece in top four corners of base, the top fixedly connected with crossbeam of bracing piece, the top fixedly connected with control box of crossbeam, the positive fixedly connected with operating panel of control box, the bottom fixedly connected with slide rail of crossbeam, the bottom sliding connection of slide rail has perforating device, perforating device's bottom fixed mounting has the head of punching a hole, there are two fly leafs at the top of base through hinge swing joint. The utility model discloses a portable electronic device, including base, bracing piece, regulation platform, adjusting bolt, movable bolt, lead screw, movable plate, lead screw, movable plate, swivel nut, the top fixedly connected with holding plate of the top of base and the side fixedly connected with holding plate that is located the bracing piece, the top fixedly connected with regulating station that the side of bracing piece and the top fixedly connected with regulating station that is located the holding plate, the inside activity of regulating bolt is pegged graft and is extended to the top and the below of regulating station respectively, adjusting bolt extends to the one end fixed surface that the regulating station was located the regulating station top and has connect adjusting handle, the inside activity of movable plate is pegged graft and has the lead screw, the both ends of lead.

Preferably, the inner wall bottom fixed mounting of control box has the battery, the inner wall bottom of control box and the right side fixed mounting who is located the battery have the controller.

Preferably, the bottom of the upper pressure plate, the top of the lower pressure plate and the side face of the clamping plate are all bonded with anti-slip pads, and one side of the movable plate is in lap joint with the surface of the supporting rod.

Preferably, the other side of the movable plate is fixedly connected with a clamping seat, and one side of the supporting rod, which is close to the movable plate, is fixedly connected with a rotating seat.

Preferably, one side of the rotating seat, which is far away from the supporting rod, is movably connected with a rotating plate through a rotating shaft, and the bottom of the rotating plate is in lap joint with the top of the clamping seat.

Preferably, a thread groove is formed in the adjusting table, and the surface of the adjusting bolt is in threaded connection with the surface of the thread groove.

(III) advantageous effects

The invention provides an aerospace material punching machine. The method has the following beneficial effects:

1. this aerospace material puncher is provided with board type material fixing device and drum type material fixing device, can fix board type aerospace material and drum type aerospace material respectively, and is more firm when making the material punch, avoids the material aversion to cause the error of punching, and round material fixing device can take off as required, and is inconvenient when avoiding board type material to punch, has solved this laser puncher and has only been fit for punching of board type material, to the aerospace material of cylinder or drum type and inapplicable problem.

2. This aerospace material puncher, simple structure, convenient operation have increased round material fixing device on original laser-beam drilling machine's basis, make round material convenient more fixed when punching, compare the aerospace material that traditional laser-beam drilling machine was suitable for wider, can play the fixed action to the clamp plate through the slipmat, can further fix the aerospace in addition, prevent that the material from sliding can also regularly changing.

Drawings

FIG. 1 is a first schematic structural diagram of the present invention;

FIG. 2 is a cross-sectional view of the structure of the present invention;

FIG. 3 is a schematic view of a second embodiment of the present invention; FIG. 4 is an enlarged view of a portion A of FIG. 3 according to the present invention.

In the figure: the device comprises a base 1, supporting legs 2, supporting rods 3, a cross beam 4, a control box 5, an operation panel 6, a sliding rail 7, a punching device 8, a punching head 9, a movable plate 10, a storage battery 11, a controller 12, a lower pressing plate 13, an adjusting table 14, an adjusting bolt 15, an upper pressing plate 16, an adjusting handle 17, a screw rod 18, a clamping plate 19, a rotating handle 20, a clamping seat 21, a rotating seat 22, a rotating plate 23, a threaded groove 24 and a non-slip mat 25.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

The embodiment of the invention provides an aerospace material punching machine, as shown in figures 1-4, which comprises a base 1, wherein four corners of the bottom of the base 1 are fixedly connected with supporting legs 2, four corners of the top of the base 1 are fixedly connected with supporting rods 3, the top of the supporting rods 3 is fixedly connected with a cross beam 4, the top of the cross beam 4 is fixedly connected with a control box 5, the bottom of the inner wall of the control box 5 is fixedly provided with a storage battery 11, the bottom of the inner wall of the control box 5 is fixedly provided with a controller 12 positioned at the right side of the storage battery 11, the storage battery 11 supplies power for the whole device, the front of the control box 5 is fixedly connected with an operating panel 6, the bottom of the cross beam 4 is fixedly connected with a sliding rail 7, the bottom of the sliding rail 7 is slidably connected with a punching device 8, the punching device 8 can move left and right on the sliding rail 7, the, the top of the base 1 is movably connected with two movable plates 10 through hinges, and the movable plates 10 can be lifted up and put down as required. A lower pressing plate 13 is fixedly connected to the top of the base 1 and the side of the supporting rod 3, when punching a plate-type material, the plate-type material is placed on the lower pressing plate 13, an adjusting platform 14 is fixedly connected to the side of the supporting rod 3 and the side of the supporting rod is positioned above the lower pressing plate 13, an adjusting bolt 15 is movably inserted in the adjusting platform 14, a threaded groove 24 is formed in the adjusting platform 14, the surface of the adjusting bolt 15 is in threaded connection with the surface of the threaded groove 24, both ends of the adjusting bolt 15 penetrate through the adjusting platform 14 and respectively extend to the upper part and the lower part of the adjusting platform 14, an upper pressing plate 16 is fixedly connected to one end of the adjusting bolt 15 extending to the lower part of the adjusting platform 14, an adjusting handle 17 is fixedly sleeved on the surface of one end of the adjusting bolt 15 extending to the upper part of the adjusting platform 14, the adjusting handle 17 is rotated to drive the adjusting bolt 15 to rotate, so that the, the two ends of the screw rod 18 penetrate through the movable plate 10 and respectively extend to the front side and the rear side of the movable plate 10, one end of the screw rod 18 extending to the rear side of the movable plate 10 is fixedly connected with a clamping plate 19, the bottom of the upper pressing plate 16, the top of the lower pressing plate 13 and the side surface of the clamping plate 19 are respectively bonded with a non-slip mat 25, the pressing plate can be fixed through the non-slip mats 25, and can be further fixed to the aerospace, the material can be replaced at regular time, a rotating handle 20 is fixedly sleeved on the surface of one end of the screw rod 18 extending to the front side of the movable plate 10, the rotating handle 20 is rotated to drive the screw rod 18 to rotate, so that the clamping plate 19 slowly moves towards the material direction until the material surface is clamped, one side of the movable plate 10 is overlapped with the surface of the support rod 3, the other side of the movable plate 10, one side that bracing piece 3 was kept away from to roating seat 22 has rotor plate 23 through pivot swing joint, and the bottom of rotor plate 23 and the top overlap joint of cassette 21 when punching to panel type material rotate rotor plate 23 and rotate rotor plate 23 to cassette 21 another side to move down fly leaf 10, make fly leaf 10 leave bracing piece 3, it is inconvenient when avoiding the panel type material to punch.

The electrical components presented in the document are all electrically connected with an external master controller and 220V mains, and the master controller can be a conventional known device controlled by a computer or the like.

The working principle is as follows: when punching, firstly, selecting a corresponding fixing device according to the shape of the punched material, when punching the cylindrical material, putting the cylindrical material on the base 1, rotating the rotating handle 20 to drive the screw rod 18 to rotate, making the clamping plate 19 slowly move towards the material until clamping the surface of the material, then the operation is carried out on the operation panel 6, the perforating device 8 is started to drive the perforating head 9 to rotate to perforate the material, the rotating handle 20 is rotated after the perforation is finished, the material is put down and taken out, when the plate-shaped material is punched, the rotating plate 23 is rotated to rotate the rotating plate 23 to the other side of the clamping seat 21, the movable plate 10 is moved down to make the movable plate 10 leave the supporting rod 3, then, the plate-shaped material is placed on the lower pressing plate 13, the adjusting handle 17 is rotated to drive the adjusting bolt 15 to rotate, the upper pressing plate 16 moves downwards to compress the material, and finally, the punching device 8 is started to punch.

In conclusion, the aerospace material perforating machine is provided with the plate-type material fixing device and the cylindrical material fixing device, so that the plate-type aerospace material and the cylindrical aerospace material can be fixed respectively, the material is more stable during perforating, perforating errors caused by material displacement are avoided, the circular material fixing device can be taken down as required, inconvenience during perforating the plate-type material is avoided, and the problems that the laser perforating machine is only suitable for perforating the plate-type material and is not suitable for cylindrical or cylindrical aerospace materials are solved.

This aerospace material puncher, simple structure, convenient operation have increased round material fixing device on original laser-beam drilling machine's basis, make round material convenient more fixed when punching, compare the aerospace material that traditional laser-beam drilling machine was suitable for wider, can play the fixed action to the clamp plate through slipmat 25, can further fix the aerospace in addition, prevent that the material from sliding can also regularly changing.

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.