CN210677016U

CN210677016U - Aerospace spare part drilling equipment

Info

Publication number: CN210677016U
Application number: CN201920800086.4U
Authority: CN
Inventors: 陶冶
Original assignee: 陶冶
Current assignee: Beijing MIG times culture technology Co., Ltd
Priority date: 2019-05-30
Filing date: 2019-05-30
Publication date: 2020-06-05
Anticipated expiration: 2029-05-30

Abstract

The utility model discloses an aerospace spare part drilling equipment, the output shaft end and the vertical axis lower extreme rigid coupling of switching motor, carousel of vertical axis upper end horizontal rigid coupling, the terminal surface left and right sides pole setting of vertical rigid coupling respectively on the carousel, terminal surface right part rigid coupling under the top of two pole settings and the diaphragm, drilling cylinder piston rod tip and L template horizontal part rigid coupling, rig of fixed mounting in the vertical portion of L template, equal slidable mounting slider on every guide rail group, fixed block of the equal rigid coupling of frame department of the inside and outside both sides of every slider, rotate installation root lead screw between two fixed blocks with one side, the lead screw passes the slider of corresponding one side and rather than threaded connection, the output shaft of adjustment motor and the lead screw outer end rigid coupling that is in same one side, every rectangular channel all slides and sets up one and founds the piece, put the thing platform in the horizontal rigid coupling in top of founding the piece, the piston rod of adjustment cylinder stretches into the. The utility model has the advantages of convenient use and high efficiency.

Description

Aerospace spare part drilling equipment

Technical Field

The utility model relates to an aerospace spare part drilling equipment is applied to spare part processing technology field.

Background

In the aerospace part machining process, the surface of the aerospace part is frequently required to be punched, the punching device in the current market is simple in structure, after one workpiece is punched, the workpiece needs to be taken down and replaced by a new workpiece, the production continuity is poor, and meanwhile, the existing punching device is troublesome in correcting the punching position of the workpiece and needs to consume more time, so that the punching efficiency is reduced.

SUMMERY OF THE UTILITY MODEL

For solving prior art scheme's defect, the utility model discloses an aerospace spare part drilling equipment has convenient to use, efficient advantage.

The utility model discloses an aerospace spare part drilling equipment, include: the automatic cutting machine comprises a frame, a U-shaped plate, a switching motor, a vertical shaft, a rotary table, vertical rods, transverse plates, a drilling cylinder, an L-shaped plate, a drilling machine, a guide rail group, a sliding block, a fixed block, a lead screw, an adjusting motor, a rectangular groove, a vertical block, an object placing table and an adjusting cylinder, wherein the U-shaped plate is fixedly connected to the middle part of the lower end face of the frame, the end parts of two vertical parts of the U-shaped plate are fixedly connected with the frame, the switching motor is arranged at the lower end face of the horizontal part of the U-shaped plate, the vertical shaft is vertically and rotatably arranged at the middle part of the frame through a bearing, the lower end of the vertical shaft downwards extends into an opening of the U-shaped plate, the tail end of an output shaft of the switching motor is fixedly connected with the lower end of the vertical shaft, the upper end of the vertical shaft is, a piston rod of a drilling cylinder penetrates through the transverse plate downwards and then is fixedly connected with the horizontal part of the L-shaped plate, a drilling machine is fixedly assembled on the vertical part of the L-shaped plate, the guide rail groups are two symmetrical and fixedly connected with the left side and the right side of the upper end surface of the frame, each guide rail group is provided with a slide block in a sliding way, the frame at the inner side and the outer side of each slide block is fixedly connected with a fixed block, a lead screw is rotatably installed between the two fixed blocks at the same side, the lead screw penetrates through the slide block at the corresponding side and is in threaded connection with the slide block, the adjusting motors are two fixed on the outer end surfaces of the two fixed blocks arranged at the outer side of the frame respectively, the output shaft of the adjusting motor is fixedly connected with the outer end of the lead screw at the same side, the rectangular grooves are arranged at the upper end surface of the slide block, an adjusting cylinder is installed on the end face, on one side, of the sliding block, which deviates from the rotary table, and a piston rod of the adjusting cylinder extends into the rectangular groove and is fixedly connected with the vertical block.

The switching motor and the adjusting motor are all servo motors capable of realizing forward and reverse rotation.

The guide rail group is composed of two parallel guide rails, and the guide rails extend longitudinally from outside to inside.

By adopting the technical scheme, the method has the following advantages:

1. the use is convenient;

2. the efficiency is high.

Drawings

Fig. 1 is a schematic structural view of the aerospace part drilling device of the present invention;

fig. 2 is a left-side view structural diagram of the middle slider of the present invention.

Wherein: 1-a frame; 2-U-shaped plate; 3-switching the motor; 4-vertical axis; 5, rotating a disc; 6-erecting a rod; 7-a transverse plate; 8-a drilling cylinder; 9-L type plate; 10-a drilling machine; 11-a set of rails; 12-a slide block; 13-fixing block; 14-a screw rod; 15-adjusting the motor; 16-a rectangular groove; 17-erecting blocks; 18-a placement table; 19-adjusting the cylinder.

Detailed Description

As shown in fig. 1 and 2, the utility model discloses an aerospace spare part drilling equipment, include: the device comprises a frame 1, a U-shaped plate 2, a switching motor 3, a vertical shaft 4, a rotary table 5, upright posts 6, a transverse plate 7, a drilling cylinder 8, an L-shaped plate 9, a drilling machine 10, a guide rail group 11, a sliding block 12, a fixed block 13, a lead screw 14, an adjusting motor 15, a rectangular groove 16, an upright block 17, an object placing table 18 and an adjusting cylinder 19, wherein the U-shaped plate 2 is fixedly connected to the middle of the lower end face of the frame 1, two end portions of the vertical portion of the U-shaped plate 2 are fixedly connected with the frame 1, the switching motor 3 is arranged at the lower end face of the horizontal portion of the U-shaped plate 2, the vertical shaft 4 is vertically and rotatably arranged at the middle of the frame 1 through a bearing, the lower end of the vertical shaft 4 downwards extends into an opening of the U-shaped plate 2, the tail end of an output shaft of the switching motor 3 is fixedly connected with the lower end of the vertical shaft 4, the upper end of the vertical shaft, the drilling cylinder 8 is vertically arranged on the left side of the upper end face of the transverse plate 7, a piston rod of the drilling cylinder 8 downwards penetrates through the transverse plate 7 and then is fixedly connected with the horizontal part of the L-shaped plate 9, a drilling machine 10 is fixedly assembled on the vertical part of the L-shaped plate 9, the guide rail groups 11 are two symmetrical and fixedly connected with the left side and the right side of the upper end face of the frame 1, each guide rail group 11 is provided with a slide block 12 in a sliding way, the frame 1 at the inner side and the outer side of each slide block 12 is fixedly connected with a fixed block 13, a screw rod 14 is rotatably arranged between the two fixed blocks 13 at the same side, the screw rod 14 penetrates through the slide block 12 at the corresponding side and is in threaded connection with the slide block, the adjusting motors 15 are two blocks 13 which are respectively arranged on the outer end faces of the two fixed blocks at the outer side of the frame, all slide in every rectangular channel 16 and set up a founding piece 17, put thing platform 18 in the horizontal rigid coupling in top of founding piece 17, it is equipped with the clamping mechanism who is used for pressing from both sides tight spare part on the thing platform 18 to put, slider 12 all installs an adjustment cylinder 19 on deviating from the terminal surface of carousel 5 one side, and adjustment cylinder 19's piston rod stretch into in the rectangular channel 16 with found a 17 rigid coupling.

The switching motor 3 and the adjusting motor 15 are all servo motors capable of realizing forward and reverse rotation.

The guide rail group 11 is two guide rails arranged in parallel, and the guide rails extend longitudinally from outside to inside.

The utility model discloses an implement like this: when drilling parts, a workpiece can be placed on the object placing tables 18 on the left side and the right side, and the workpiece is clamped and fixed through the clamping mechanisms on the object placing tables 18 (the clamping mechanisms are traditional clamping mechanisms in the market, and the description is omitted in the application), initially, the drilling machine 10 is placed on the left side of the rack 1, the positions of the object placing tables 18 can be adjusted through the adjusting motor 15 and the adjusting cylinder 19, so that the drilling positions of the workpiece can be placed under a drill bit of the drilling machine 10, during adjustment, the adjusting motor 15 can drive the screw rod 14 to rotate, and the screw rod 14 is in threaded connection with the sliding block 13, so that the sliding block 13 can be driven to move inside and outside along the guide rail group 11, and the sliding block 13 drives the object placing; meanwhile, the adjusting cylinder 19 can drive the vertical block 17 to move left and right along the rectangular groove 16, the vertical block 17 drives the object placing table 18 to move left and right, so that the position of the workpiece can be adjusted, and after the position of the workpiece is well positioned, the drilling cylinder 8 drives the drilling machine 10 to move downwards, so that the workpiece can be drilled; after the left side work piece drilling is accomplished, drive carousel 5 through switching motor 3 and rotate 180, place rig 10 in 1 right side of frame, the position of adjustment motor 15 and the adjustment cylinder 19 adjustment right side work piece on accessible right side in the same reason, drill the right side work piece through rig 10 at last, this moment when to the drilling of right side work piece, the work piece that the hole was bored to the left side can be taken off to the manual work, and the new work piece has been changed, after the first work piece drilling in right side was accomplished, can get back to initial position through switching motor 3 reverse rotation 180 immediately, because the work piece is unanimous, need not to fix a position second left side work piece, can drill the second left side immediately, in this moment in the same reason, change the work piece on right side, so relapse, can drill the work piece in succession. By adopting the technical scheme, the workpiece can be continuously drilled, and the drilling efficiency is improved.

Finally, it should be noted that: the above embodiments are only used for illustrating the present invention and do not limit the technical solution described in the present invention; thus, while the present invention has been described in detail with reference to the various embodiments thereof, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted; all such modifications and variations are intended to be included herein within the scope of this disclosure and the present invention and within the scope and spirit of the following claims.

Claims

1. An aerospace component drilling apparatus, comprising: frame, U template, switching motor, vertical axis, carousel, pole setting, diaphragm, drilling cylinder, L template, rig, guide rail group, slider, fixed block, lead screw, adjustment motor, rectangular channel, founding the piece, putting thing platform, adjustment cylinder, the terminal surface middle part under the frame of U template rigid coupling, two vertical portion tip and the frame rigid coupling of U template, the terminal surface department under U template horizontal part is installed to the switching motor, the vertical axis passes through the vertical rotation of bearing and installs at the frame middle part, and in the opening of vertical axis lower extreme stretched into the U template downwards, the output shaft end and the vertical axis lower extreme rigid coupling of switching motor, its characterized in that: the upper end of the vertical shaft is horizontally and fixedly connected with a turntable, the left side and the right side of the upper end surface of the turntable are respectively and vertically fixedly connected with a vertical rod, the top ends of the two vertical rods are fixedly connected with the right part of the lower end surface of the transverse plate, the drilling cylinder is vertically arranged on the left side of the upper end surface of the transverse plate, a piston rod of the drilling cylinder downwards passes through the rear end part of the transverse plate and is fixedly connected with the horizontal part of the L-shaped plate, a drilling machine is fixedly assembled on the vertical part of the L-shaped plate, the guide rail groups are two symmetrical and fixedly connected with the left side and the right side of the upper end surface of the frame, a sliding block is arranged on each guide rail group in a sliding way, a fixed block is fixedly connected with the frame at the inner side and the outer side of each sliding block, a lead screw is rotatably arranged between the two fixed, the rectangular channel is seted up in slider up end department, and every rectangular channel is interior all to slide and is set up an upright piece, put the thing platform in the horizontal rigid coupling in top of founding the piece, it is equipped with the clamping mechanism who is used for pressing from both sides tight spare part on the thing platform to put, an adjustment cylinder is all installed on the terminal surface that the slider deviates from carousel one side, and adjustment cylinder's piston rod stretches into in the rectangular channel and found a rigid coupling.

2. An aerospace component drilling apparatus as claimed in claim 1, wherein: the switching motor and the adjusting motor are all servo motors capable of realizing forward and reverse rotation.

3. An aerospace component drilling apparatus as claimed in claim 1, wherein: the guide rail group is composed of two parallel guide rails, and the guide rails extend longitudinally from outside to inside.