CN215698277U

CN215698277U - Aviation front connector milling device

Info

Publication number: CN215698277U
Application number: CN202122105017.1U
Authority: CN
Inventors: 闵立志; 唐铭龙; 王真
Original assignee: Shaanxi Huachen Aviation Technology Co ltd
Current assignee: Shaanxi Huachen Aviation Technology Co ltd
Priority date: 2021-09-01
Filing date: 2021-09-01
Publication date: 2022-02-01
Anticipated expiration: 2031-09-01

Abstract

The utility model relates to the technical field of mechanical equipment, in particular to an aviation front connector milling device, which improves the convenience of equipment use; the milling efficiency of the equipment is improved; the base, first slider, the riser, the bull stick, the installation piece, connect the spare, the diaphragm, the lifter, the briquetting, the limiting plate, a spring, the curb plate, the second slider, first accessory plate, first motor, erector and milling cutter, the upper end of base is provided with first slide rail groove, first slider slides at first slide rail inslot, the upper end at first slider is installed to the riser, the upper end at first slider is installed through the bearing to the bull stick, the upper end at the bull stick is installed to the installation piece, the upper end of installation piece is provided with the mounting groove, it places in the mounting groove of installation piece upper end to connect the spare, the side at the riser is installed to the diaphragm, the lifter can reciprocate on the diaphragm, the briquetting is installed to the lower extreme of lifter, the lower extreme of briquetting is provided with the cooperation groove.

Description

Aviation front connector milling device

Technical Field

The utility model relates to the technical field of mechanical equipment, in particular to an aviation front connector milling device.

Background

The milling processing device for the aviation front connector is an auxiliary device for milling aviation front connector parts, and is widely used in the field of mechanical equipment; the existing milling device for the aerial front connector is found in use, when different surfaces of a part are milled by the conventional milling device, the part needs to be repeatedly disassembled and the surface needs to be changed fixedly, and the machining efficiency of equipment is poor.

SUMMERY OF THE UTILITY MODEL

In order to solve the technical problems, the utility model provides a device which improves the convenience of using the device; the milling efficiency of equipment is improved.

The utility model relates to an aviation front joint milling device, which comprises a base, a first sliding block, a vertical plate, a rotating rod, an installation block, a joint piece, a transverse plate, a lifting rod, a pressing block, a limiting plate, a spring, a side plate, a second sliding block, a first auxiliary plate, a first motor, an installer and a milling cutter, wherein the upper end of the base is provided with a first sliding rail groove, the first sliding block slides in the first sliding rail groove, the vertical plate is installed at the upper end of the first sliding block, the rotating rod is installed at the upper end of the first sliding block through a bearing, the installation block is installed at the upper end of the rotating rod, the upper end of the installation block is provided with an installation groove, the joint piece is placed in the installation groove at the upper end of the installation block, the transverse plate is installed at the side end of the vertical plate, the lifting rod can move up and down on the transverse plate, the lower end of the lifting rod is provided with the pressing block, the lower end of the pressing block is provided with a matching groove, the upper end of the joint piece is located in the matching groove at the lower end of the pressing block, the limiting plate is installed at the upper end of the lifting rod, the limiting plate is connected with the upper end of the transverse plate through a spring, the side plate is installed at the upper end of the base, a second slide rail groove is formed in the side end of the side plate, the second slide block slides in the second slide rail groove, the two first auxiliary plates are installed at the side end of the second slide block, the first motor is installed between the two first auxiliary plates, an installer is installed at the output end of the first motor, and the milling cutter is installed at the side end of the installer.

The milling device for the aviation front connector further comprises a second motor, a first meshing wheel and a second meshing wheel, wherein the second motor is mounted at the upper end of the first sliding block, the output end of the second motor penetrates through the vertical plate through a bearing, the first meshing wheel is mounted at the output end of the second motor, the first meshing wheel and the second meshing wheel are in meshing transmission, and the second meshing wheel is mounted on the rotating rod.

The milling device for the aviation front connector further comprises a hydraulic cylinder, wherein the hydraulic cylinder is installed at the upper end of the base, and the output end of the hydraulic cylinder is connected with the first sliding block.

The milling device for the aviation front connector further comprises a limiting rod, a first limiting block and a second limiting block, wherein the second sliding block is provided with a mounting hole, the limiting rod is mounted in the mounting hole of the second sliding block, the first limiting block and the second limiting block are mounted at the side end of the side plate, and the limiting rod can move on the first limiting block and the second limiting block.

The utility model relates to an aviation front connector milling device which further comprises a mounting plate, two second auxiliary plates, a third motor, a third meshing wheel, two meshing rotating rods and two rotating discs, wherein the mounting plate is mounted at the upper end of a side plate, the two second auxiliary plates are mounted at the side ends of the mounting plate, the third motor is mounted between the two second auxiliary plates, the output end of the third motor penetrates through the mounting plate through a bearing, the output end of the third motor is provided with the third meshing wheel, the third meshing wheel is in meshing transmission with the two meshing rotating rods, the two meshing rotating rods are mounted at the side ends of the mounting plate through bearings, the rotating discs are respectively mounted at the side ends of the two meshing rotating rods, meshing teeth are arranged at the outer ends of the rotating discs, a plurality of meshing grooves are formed in the limiting rod, and the meshing teeth are in meshing transmission with the meshing grooves.

The milling device for the aviation front connector further comprises a collecting box, and the collecting box is mounted at the upper end of the first sliding block.

Compared with the prior art, the utility model has the beneficial effects that: applying downward pressure on a limiting plate under the action of a spring, descending the limiting plate under the downward pressure, driving a pressing block to descend through a lifting rod by the descending of the limiting plate, fixing a joint piece by the descending of the pressing block and the matching of an installation block, sliding a first sliding block, driving the joint piece to move through a rotating rod and the installation block by the sliding of the first sliding block, enabling the joint piece to be close to a milling cutter, starting a first motor, driving a milling cutter to rotate through an installer by the output end of the first motor, milling the side end of the joint piece by the rotation of the milling cutter, sliding a second sliding block, driving the milling cutter to move through a first auxiliary plate, the first motor and the installer by the sliding of the second sliding block, so that the milling cutter comprehensively mills one surface of the joint piece, then rotating the rotating rod, driving the joint piece to rotate through the installation block by the rotation of the rotating rod, and further enabling the joint piece to rotate to the other surface for milling processing, the convenience of equipment use is improved.

Drawings

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

FIG. 2 is a schematic view of a third motor and a limiting rod;

FIG. 3 is an enlarged view of the second motor and the joint member;

reference numerals: 1. a base; 2. a first slide rail groove; 3. a first slider; 4. a vertical plate; 5. a rotating rod; 6. mounting blocks; 7. a joint member; 8. a transverse plate; 9. a lifting rod; 10. briquetting; 11. a limiting plate; 12. a spring; 13. a side plate; 14. a second slide rail groove; 15. a second slider; 16. a first auxiliary plate; 17. a first motor; 18. an installer; 19. milling cutters; 20. a second motor; 21. a first meshing wheel; 22. a second meshing wheel; 23. a hydraulic cylinder; 24. a limiting rod; 25. a first stopper; 26. a second limiting block; 27. mounting a plate; 28. a second auxiliary plate; 29. a third motor; 30. a third meshing wheel; 31. engaging the rotating rod; 32. a turntable; 33. meshing teeth; 34. an engagement groove; 35. and a collection box.

Detailed Description

The following detailed description of embodiments of the present invention is provided in connection with the accompanying drawings and examples. The following examples are intended to illustrate the utility model but are not intended to limit the scope of the utility model.

As shown in fig. 1 to 3, the milling device for the aviation front connector of the utility model comprises a base 1, a first slide block 3, a vertical plate 4, a rotating rod 5, a mounting block 6, a connector 7, a transverse plate 8, a lifting rod 9, a pressing block 10, a limiting plate 11, a spring 12, a side plate 13, a second slide block 15, a first auxiliary plate 16, a first motor 17, a mounting device 18 and a milling cutter 19, wherein the upper end of the base 1 is provided with a first slide rail groove 2, the first slide block 3 slides in the first slide rail groove 2, the vertical plate 4 is mounted at the upper end of the first slide block 3, the rotating rod 5 is mounted at the upper end of the first slide block 3 through a bearing, the mounting block 6 is mounted at the upper end of the rotating rod 5, the connector 7 is placed in the mounting groove at the upper end of the mounting block 6, the transverse plate 8 is mounted at the side end of the vertical plate 4, the lifting rod 9 can move up and down on the transverse plate 8, the pressing block 10 is mounted at the lower end of the lifting rod 9, the lower end of the pressing block 10 is provided with a matching groove, the upper end of the joint piece 7 is positioned in the matching groove at the lower end of the pressing block 10, the upper end of the lifting rod 9 is provided with a limiting plate 11, the limiting plate 11 is connected with the upper end of the transverse plate 8 through a spring 12, a side plate 13 is arranged at the upper end of the base 1, the side end of the side plate 13 is provided with a second slide rail groove 14, a second slide block 15 slides in the second slide rail groove 14, two first auxiliary plates 16 are arranged at the side end of the second slide block 15, a first motor 17 is arranged between the two first auxiliary plates 16, the output end of the first motor 17 is provided with a mounting device 18, and a milling cutter 19 is arranged at the side end of the mounting device 18; downward pressure is applied to a limiting plate 11 under the action of a spring 12, the limiting plate 11 is subjected to downward pressure to descend, the descending of the limiting plate 11 drives a pressing block 10 to descend through a lifting rod 9, the pressing block 10 descends to be matched with a mounting block 6 to fix a connector 7, a first sliding block 3 slides, the sliding of the first sliding block 3 drives the connector 7 to move through a rotating rod 5 and the mounting block 6, the connector 7 is close to a milling cutter 19, a first motor 17 is started, the output end of the first motor 17 drives the milling cutter 19 to rotate through a mounting device 18, the side end of the connector 7 is milled through the rotation of the milling cutter 19, a second sliding block 15 slides, the sliding of the second sliding block 15 drives the milling cutter 19 to move through a first auxiliary plate 16, the first motor 17 and the mounting device 18, so that the milling cutter 19 comprehensively mills one surface of the connector 7, then the rotating rod 5 is rotated, the rotation of the rotating rod 5 drives the connector 7 to rotate through the mounting block 6, thereby make the joint spare 7 rotate to the another side and mill processing, improved the convenience that equipment used.

The milling device for the aviation front connector further comprises a second motor 20, a first meshing wheel 21 and a second meshing wheel 22, wherein the second motor 20 is installed at the upper end of the first sliding block 3, the output end of the second motor 20 penetrates through the vertical plate 4 through a bearing, the first meshing wheel 21 is installed at the output end of the second motor 20, the first meshing wheel 21 and the second meshing wheel 22 are in meshing transmission, and the second meshing wheel 22 is installed on the rotating rod 5; the second motor 20 is started, the output end of the second motor 20 drives the first meshing wheel 21 to rotate, the first meshing wheel 21 rotates to drive the second meshing wheel 22 to rotate through meshing transmission, the second meshing wheel 22 rotates to drive the rotating rod 5 to rotate, power is provided for the rotating rod 5 to rotate through the second motor 20, the rotating rod 5 is enabled to rotate more stably and controllably, and the use stability and controllability of the equipment are improved.

The milling device for the aviation front connector further comprises a hydraulic cylinder 23, wherein the hydraulic cylinder 23 is installed at the upper end of the base 1, and the output end of the hydraulic cylinder 23 is connected with the first sliding block 3; the hydraulic cylinder 23 is started, the output end of the hydraulic cylinder 23 drives the first sliding block 3 to move, power is provided for the first sliding block 3 to move through the hydraulic cylinder 23, the first sliding block 3 is more stable and controllable in movement, and the use stability and controllability of the equipment are improved.

The milling device for the aviation front connector further comprises a limiting rod 24, a first limiting block 25 and a second limiting block 26, wherein a mounting hole is formed in the second sliding block 15, the limiting rod 24 is mounted in the mounting hole of the second sliding block 15, the first limiting block 25 and the second limiting block 26 are mounted at the side end of the side plate 13, and the limiting rod 24 can move on the first limiting block 25 and the second limiting block 26; when the second slider 15 moves on the second slide rail groove 14, the limiting rod 24, the first limiting block 25 and the second limiting block 26 are matched to enable the second slider 15 to move more stably, and the use stability of the device is improved.

The milling device for the aviation front connector further comprises a mounting plate 27, two second auxiliary plates 28 and a third motor 29, the mounting plate 27 is mounted at the upper end of the side plate 13, the two second auxiliary plates 28 are mounted at the side ends of the mounting plate 27, the third motor 29 is mounted between the two second auxiliary plates 28, the output end of the third motor 29 penetrates through the mounting plate 27 through a bearing, the output end of the third motor 29 is provided with the third engaging wheel 30, the third engaging wheel 30 is in engaging transmission with the two engaging rotary rods 31, the two engaging rotary rods 31 are mounted at the side ends of the mounting plate 27 through bearings, the side ends of the two engaging rotary rods 31 are respectively provided with the rotary plate 32, the outer end of the rotary plate 32 is provided with engaging teeth 33, the limiting rod 24 is provided with a plurality of engaging grooves 34, and the engaging teeth 33 are in engaging transmission with the engaging grooves 34; the third motor 29 is started, the output end of the third motor 29 drives the third meshing wheel 30 to rotate, the third meshing wheel 30 rotates to drive the two meshing rotating rods 31 to rotate through meshing transmission, the two meshing rotating rods 31 rotate to drive the two rotating discs 32 to rotate respectively, the two rotating discs 32 rotate to drive the circulating lifting of the limiting rod 24 through the matching of the meshing teeth 33 and the meshing grooves 34 respectively, the circulating lifting of the limiting rod 24 drives the circulating lifting of the second sliding block 15, power is provided for the circulating lifting of the second sliding block 15 through the third motor 29, the lifting of the second sliding block 15 is more stable and controllable, and the use stability and controllability of the device are improved.

The milling device for the aviation front connector further comprises a collecting box 35, wherein the collecting box 35 is arranged at the upper end of the first sliding block 3; the milling cutter 19 carries out the milling process to the adapter 7 and produces the piece and falls to collect in the collecting box 35, has improved the convenience that equipment used.

The utility model relates to an aviation front connector milling device, which is operated, firstly, downward pressure is applied to a limiting plate 11 under the action of a spring 12, the limiting plate 11 is descended under the downward pressure, the descending of the limiting plate 11 drives a pressing block 10 to descend through a lifting rod 9, the pressing block 10 descends to be matched with a mounting block 6 to fix a connector 7, a hydraulic cylinder 23 is started, the output end of the hydraulic cylinder 23 drives a first sliding block 3 to move, the sliding of the first sliding block 3 drives the connector 7 to move through a rotating rod 5 and the mounting block 6, the connector 7 is close to a milling cutter 19, a first motor 17 is started, the output end of the first motor 17 drives a milling cutter 19 to rotate through a mounting device 18, the rotation of the milling cutter 19 mills the side end of the connector 7, a third motor 29 is started, the output end of the third motor 29 drives a third meshing wheel 30 to rotate, the rotation of the third meshing wheel 30 drives two meshing rotating rods 31 to rotate through meshing transmission, the rotation of the two engaging rotating rods 31 respectively drives the two rotating disks 32 to rotate, the rotation of the two rotating disks 32 respectively drives the circular lifting of the limiting rod 24 through the matching of the engaging teeth 33 and the engaging grooves 34, the circular lifting of the limiting rod 24 drives the circular lifting of the second sliding block 15, the movement of the second sliding block 15 drives the movement of the milling cutter 19 through the first auxiliary plate 16, the first motor 17 and the mounting device 18, so that the milling cutter 19 comprehensively mills one surface of the joint piece 7, then the second motor 20 is started, the output end of the second motor 20 drives the rotation of the first engaging wheel 21, the rotation of the first engaging wheel 21 drives the rotation of the second engaging wheel 22 through the engaging transmission, the rotation of the second engaging wheel 22 drives the rotation of the rotating rod 5, the rotation of the rotating rod 5 drives the rotation of the joint piece 7 through the mounting block 6, so that the joint piece 7 rotates to the other surface for milling processing, the equipment is used after the use is finished.

According to the milling device for the aviation front connector, the installation mode, the connection mode or the arrangement mode are common mechanical modes, and the milling device can be implemented as long as the beneficial effects of the milling device can be achieved; the spring 12, the first motor 17, the second motor 20, the hydraulic cylinder 23 and the third motor 29 of the milling device for the aviation front connector are purchased from the market, and technicians in the industry only need to install and operate the milling device according to the attached operating instructions.

The above description is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, several modifications and variations can be made without departing from the technical principle of the present invention, and these modifications and variations should also be regarded as the protection scope of the present invention.

Claims

1. An aviation front joint milling device is characterized by comprising a base (1), a first sliding block (3), a vertical plate (4), a rotating rod (5), a mounting block (6), a joint piece (7), a transverse plate (8), a lifting rod (9), a pressing block (10), a limiting plate (11), a spring (12), a side plate (13), a second sliding block (15), a first auxiliary plate (16), a first motor (17), a mounting device (18) and a milling cutter (19), wherein the upper end of the base (1) is provided with a first sliding rail groove (2), the first sliding block (3) slides in the first sliding rail groove (2), the vertical plate (4) is mounted at the upper end of the first sliding block (3), the rotating rod (5) is mounted at the upper end of the first sliding block (3) through a bearing, the mounting block (6) is mounted at the upper end of the rotating rod (5), and a mounting groove is formed at the upper end of the mounting block (6), the joint piece (7) is placed in a mounting groove at the upper end of the mounting block (6), the transverse plate (8) is mounted at the side end of the vertical plate (4), the lifting rod (9) can move up and down on the transverse plate (8), the lower end of the lifting rod (9) is provided with a pressing block (10), the lower end of the pressing block (10) is provided with a matching groove, the upper end of the joint piece (7) is positioned in the matching groove at the lower end of the pressing block (10), the upper end of the lifting rod (9) is provided with a limiting plate (11), the limiting plate (11) is connected with the upper end of the transverse plate (8) through a spring (12), the side plate (13) is mounted at the upper end of the base (1), the side end of the side plate (13) is provided with a second sliding rail groove (14), the second sliding block (15) slides in the second sliding rail groove (14), the two first auxiliary plates (16) are mounted at the side end of the second sliding block (15), and the first motor (17) is mounted between the two first auxiliary plates (16), the output end of the first motor (17) is provided with a mounting device (18), and the milling cutter (19) is arranged at the side end of the mounting device (18).

2. The milling device for the aviation front connector, according to claim 1, is characterized by further comprising a second motor (20), a first meshing wheel (21) and a second meshing wheel (22), wherein the second motor (20) is installed at the upper end of the first sliding block (3), the output end of the second motor (20) penetrates through the vertical plate (4) through a bearing, the first meshing wheel (21) is installed at the output end of the second motor (20), the first meshing wheel (21) and the second meshing wheel (22) are in meshing transmission, and the second meshing wheel (22) is installed on the rotating rod (5).

3. The milling device for the aviation front connector as claimed in claim 1, characterized by further comprising a hydraulic cylinder (23), wherein the hydraulic cylinder (23) is mounted at the upper end of the base (1), and the output end of the hydraulic cylinder (23) is connected with the first sliding block (3).

4. The milling device for the aviation front connector according to claim 1, further comprising a limiting rod (24), a first limiting block (25) and a second limiting block (26), wherein a mounting hole is formed in the second slider (15), the limiting rod (24) is mounted in the mounting hole of the second slider (15), the first limiting block (25) and the second limiting block (26) are mounted at the side end of the side plate (13), and the limiting rod (24) can move on the first limiting block (25) and the second limiting block (26).

5. The milling device for the aviation front connector according to claim 4, characterized in that the milling device further comprises a mounting plate (27), two second auxiliary plates (28), a third motor (29), a third engaging wheel (30), two engaging rotating rods (31) and two rotating discs (32), the mounting plate (27) is mounted at the upper end of the side plate (13), the two second auxiliary plates (28) are mounted at the side end of the mounting plate (27), the third motor (29) is mounted between the two second auxiliary plates (28), the output end of the third motor (29) passes through the mounting plate (27) through a bearing, the output end of the third motor (29) is mounted with the third engaging wheel (30), the third engaging wheel (30) is in engaging transmission with the two engaging rotating rods (31), the two engaging rotating rods (31) are mounted at the side end of the mounting plate (27) through a bearing, the rotating discs (32) are respectively mounted at the side ends of the two engaging rotating rods (31), the outer end of the rotary table (32) is provided with meshing teeth (33), the limiting rod (24) is provided with a plurality of meshing grooves (34), and the meshing teeth (33) are in meshing transmission with the meshing grooves (34).

6. The milling device for the aeronautical front joint according to claim 1, characterized in that it further comprises a collection box (35), the collection box (35) being mounted on the upper end of the first slider (3).