CN215280924U

CN215280924U - Aviation combined material drilling equipment

Info

Publication number: CN215280924U
Application number: CN202120731800.6U
Authority: CN
Inventors: 李勇
Original assignee: Yichang Hedali Composite Materials Co ltd
Current assignee: Yichang Hedali Composite Materials Co ltd
Priority date: 2021-04-08
Filing date: 2021-04-08
Publication date: 2021-12-24
Anticipated expiration: 2031-04-08

Abstract

The utility model discloses an aviation composite material drilling device, which comprises a bottom plate and a supporting component, wherein the upper surface of the bottom plate is provided with a moving component, the upper end of the moving component is provided with a driving component, and a drilling component is arranged above the driving component; the moving assembly comprises a sliding rail, a sliding plate and a sliding block, the sliding plate is connected to the upper surface of the sliding rail in a sliding mode, the sliding rail is fixedly arranged on two sides of the upper surface of the bottom plate, and the sliding block is connected to the upper surface of the sliding plate in a sliding mode; the drilling assembly comprises a rotating motor, a spindle, a chuck and a drill bit, the top end of the spindle is movably inserted into the output end of the rotating motor, the chuck is clamped at the lower end inside the spindle, and the drill bit is clamped at the lower end inside the chuck. The utility model discloses a draw-in groove will treat the aviation combined material of drilling to fix, and then removes the subassembly through control and remove, and then drives aviation combined material and removes, has realized carrying out the effect of drilling to different positions of aviation combined material.

Description

Aviation combined material drilling equipment

Technical Field

The utility model discloses drilling equipment technical field specifically is an aviation combined material drilling equipment.

Background

The aviation material is a material guarantee for developing and producing aviation products, and is a technical basis for enabling the aviation products to achieve the performance, service life and reliability expected by people; due to the basic position of the aviation material and the continuous improvement of the contribution rate of the aviation material to aviation products, the aviation material, the aviation engine and the information technology become one of three parallel aviation key technologies and are also one of six technologies which have important influence on the development of the aviation products.

Aviation product is producing the creation in-process, need use aviation combined material, during the in-service use, need carry out drilling work to aviation combined material according to actual conditions, current drilling equipment has realized the effect of driling to aviation combined material when using, nevertheless still there are some not enough in the in-service use, current drilling equipment can only bore hole to aviation combined material's single position at the during operation, because aviation material need bore hole at different position, and then current drilling equipment practicality is not strong.

SUMMERY OF THE UTILITY MODEL

The utility model discloses to the technical problem who exists among the prior art, through setting up removal subassembly and drive assembly, can remove according to the actual demand when fixed with space flight combined material, and then can carry out drilling work at different positions to solve the problem that proposes in the above-mentioned background art.

The utility model provides an above-mentioned technical problem's technical scheme as follows: the aviation composite material drilling device comprises a bottom plate and a supporting assembly, wherein a moving assembly is arranged on the upper surface of the bottom plate, a driving assembly is arranged at the upper end of the moving assembly, and a drilling assembly is arranged above the driving assembly;

the moving assembly comprises a sliding rail, a sliding plate and a sliding block, the sliding plate is connected to the upper surface of the sliding rail in a sliding mode, the sliding rail is fixedly arranged on two sides of the upper surface of the bottom plate, and the sliding block is connected to the upper surface of the sliding plate in a sliding mode;

the drilling assembly comprises a rotating motor, a spindle, a chuck and a drill bit, the top end of the spindle is movably inserted into the output end of the rotating motor, the chuck is clamped at the lower end inside the spindle, and the drill bit is clamped at the lower end inside the chuck.

Preferably, the supporting component comprises a connecting plate, a fixing plate and supporting columns, and the supporting columns are located on two sides of the lower surface of the bottom plate.

Preferably, the connecting plates are fixedly arranged on two sides of the upper surface of the bottom plate, the fixing plates are fixedly arranged on the upper surface of the connecting plates, and the fixing plates are positioned above the bottom plate.

Preferably, a through hole is formed in the middle of the inside of the fixing plate, the spindle is inserted into the through hole, and the rotating motor is fixedly mounted in the middle of the upper surface of the fixing plate.

Preferably, the driving assembly comprises a transverse electric push rod, a longitudinal electric push rod and a backup plate, the top end of the transverse electric push rod is fixedly inserted into one side inside the connecting plate, the tail end of the transverse electric push rod is fixedly inserted into one side inside the sliding plate, the top end of the longitudinal electric push rod is fixedly inserted into one side inside the backup plate, and the tail end of the longitudinal electric push rod is fixedly inserted into one side inside the sliding block.

Preferably, the driving assembly further comprises a control panel, a first travel switch and a second travel switch are arranged on the upper surface of the control panel, the first travel switch is electrically connected with the transverse electric push rod, and the second travel switch is electrically connected with the longitudinal electric push rod.

Preferably, the sliding plate is internally provided with a sliding groove, the lower surface of the sliding block is connected to the inside of the sliding groove in a sliding mode, the two sides of the upper end of the inside of the sliding block are provided with clamping grooves, and the lower end of each clamping groove is provided with an avoiding groove.

Compared with the prior art, the technical scheme of the application has the following beneficial technical effects:

1. the utility model discloses a set up and remove subassembly and drilling subassembly, the aviation combined material who will treat drilling through the draw-in groove fixes, and then removes the subassembly through control, and then drives aviation combined material and remove, has realized carrying out the effect of drilling to different positions of aviation combined material, has solved current drilling equipment and can only carry out the problem of drilling to aviation combined material's single position at the during operation.

2. The utility model discloses a set up drive assembly, and drive assembly still includes control panel, actually carries out the during operation, and relevant staff only need control drive assembly through control panel and drive the removal subassembly and remove, remove to appointed position after, through the drilling subassembly drill can, whole drilling work need not a large amount of manual works and participates in, only needs control panel can realize.

Drawings

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

FIG. 2 is a schematic top view of the present invention;

fig. 3 is a schematic view of the driving assembly and the moving assembly of the present invention;

FIG. 4 is a schematic view of the slide plate and the slide block of the present invention;

fig. 5 is a schematic view of the main structure of the fixing plate of the present invention.

In the drawings, the components represented by the respective reference numerals are listed below:

1. a base plate; 2. a support assembly; 3. a moving assembly; 4. a drive assembly; 5. a drilling assembly; 21. a connecting plate; 22. a fixing plate; 23. a support pillar; 31. a slide rail; 32. a slide plate; 33. a slider; 41. a transverse electric push rod; 42. a backup plate; 43. a longitudinal electric push rod; 44. a control panel; 51. a rotating electric machine; 52. a main shaft; 53. a chuck; 54. a drill bit; 221. a through hole; 321. a chute; 331. a card slot; 332. an avoidance groove; 441. a first travel switch; 442. a second travel switch.

Detailed Description

Referring to fig. 1-5, the present invention provides a technical solution:

the utility model provides an aviation combined material drilling equipment, including bottom plate 1 and supporting component 2, 1 upper surface of bottom plate is equipped with removal subassembly 3, removal subassembly 3 upper end is equipped with drive assembly 4, drive assembly 4 top is equipped with drilling subassembly 5, when actually using, after the aviation combined material that will treat the drilling is fixed, it can to drill through drilling subassembly 5, when needing to drill to different positions, move subassembly 3 through drive assembly 4 control, and then drive the space flight combined material and remove, when the position of treating the drilling removes under drilling subassembly 5, it can to drill through drilling subassembly 5, the effect that can carry out the drilling to the space flight combined material of different positions has been realized, support drilling subassembly 5 and bottom plate 1 through supporting component 2, and then can stable work that carries out.

The movable assembly 3 includes a slide rail 31, a slide plate 32 and a slide block 33, the slide plate 32 is slidably connected to the upper surface of the slide rail 31, the slide rail 31 is fixedly installed on two sides of the upper surface of the bottom plate 1, the slide plate 33 is slidably connected to the upper surface of the slide plate 32, a sliding groove 321 is formed in the sliding groove 321, a clamping groove 331 is formed in two sides of the inner upper end of the slide plate 33, a avoiding groove 332 is formed in the lower end of the clamping groove 331, the aerospace composite material to be drilled is fixed in the slide plate 33 through the clamping groove 331, the slide plate 33 can move back and forth along the direction of the sliding groove 321, the slide plate 32 can move left and right along the direction of the slide rail 31, the effect of adjusting the position of the aerospace composite material can be driven is achieved, during drilling, the drilling is achieved, and the drilling assembly 5 is prevented from impacting on the upper surface of the slide plate 33 during drilling through the avoiding groove 332.

The driving assembly 4 includes a transverse electric push rod 41, a longitudinal electric push rod 43 and a backup plate 42, the top end of the transverse electric push rod 41 is fixedly inserted into one side of the inside of the connecting plate 21, the end of the transverse electric push rod 41 is fixedly inserted into one side of the inside of the sliding plate 32, the top end of the longitudinal electric push rod 43 is fixedly inserted into one side of the inside of the backup plate 42, the end of the longitudinal electric push rod 43 is fixedly inserted into one side of the inside of the sliding block 33, the driving assembly 4 further includes a control panel 44, the upper surface of the control panel 44 is provided with a first travel switch 441 and a second travel switch 442, the first travel switch 441 is electrically connected with the transverse electric push rod 41, the second travel switch 442 is electrically connected with the longitudinal electric push rod 43, when the moving assembly 3 is actually controlled to move, the transverse electric push rod 41 can be controlled to extend and retract by pressing the first travel switch 441, so as to push the sliding plate 32 to slide left and right along the direction of the sliding rail 31, by pressing the second travel switch 442, the longitudinal electric push rod 43 can be controlled to extend and retract, and further the slide block 33 is pushed to move back and forth along the direction of the slide slot 321, and the position of the longitudinal electric push rod 43 is fixed by the backup plate 42.

The drilling assembly 5 comprises a rotating motor 51, a spindle 52, a chuck 53 and a drill bit 54, wherein the top end of the spindle 52 is movably inserted into the output end of the rotating motor 51, the chuck 53 is clamped at the inner lower end of the spindle 52, the drill bit 54 is clamped at the inner lower end of the chuck 53, when the drilling operation is actually performed, the spindle 52 is driven to rotate by starting the rotating motor 51, the chuck 53 and the drill bit 54 are driven to rotate while the spindle 52 rotates, and meanwhile, the spindle 52 is pulled downwards to drive the chuck 53 and the drill bit 54 to move downwards until the drill bit 54 contacts with the aeronautical composite material and performs the drilling operation.

The supporting component 2 comprises a connecting plate 21, a fixing plate 22 and supporting columns 23, the supporting columns 23 are positioned on two sides of the lower surface of the bottom plate 1, the connecting plate 21 is fixedly arranged on two sides of the upper surface of the bottom plate 1, the fixing plate 22 is fixedly arranged on the upper surface of the connecting plate 21, the fixing plate 22 is positioned above the bottom plate 1, a through hole 221 is arranged in the middle position inside the fixing plate 22, the spindle 52 is inserted into the through hole 221, the rotating motor 51 is fixedly arranged in the middle position on the upper surface of the fixing plate 22, the drilling assembly 5 is fixed by the connecting plates 21 and the fixing plates 22, and the maximum stroke of the slide rail 31 can be limited by the connecting plates 21 on both sides, so that the slide plate 32 is prevented from falling out of the upper end of the slide rail 31 beyond the range when moving, and through the through hole 221, the main shaft 52 can pass through the fixed plate 22 to be movably connected with the output end of the rotating motor 51, the whole drilling device is stably fixed on the ground through the support columns 23 at the two sides of the bottom plate 1.

When specifically using, earlier will treat the aeronautical composite who drills through the draw-in groove and fix, relevant staff only need control drive assembly through control panel and drive the removal subassembly and remove, and then drive aeronautical composite and remove, remove to appointed position after, through the drilling subassembly drill can, can drill to aeronautical composite different positions, whole drilling work need not a large amount of manual work and participates in, only need control panel can realize.

The above description is only for the preferred embodiment of the present invention, and is not intended to limit the present invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included within the protection scope of the present invention.

Claims

1. An aeronautical composite drilling device, comprising a base plate (1) and a support assembly (2), characterized in that: a moving assembly (3) is arranged on the upper surface of the bottom plate (1), a driving assembly (4) is arranged at the upper end of the moving assembly (3), and a drilling assembly (5) is arranged above the driving assembly (4);

the moving assembly (3) comprises a sliding rail (31), a sliding plate (32) and a sliding block (33), the sliding plate (32) is connected to the upper surface of the sliding rail (31) in a sliding mode, the sliding rail (31) is fixedly installed on two sides of the upper surface of the base plate (1), and the sliding block (33) is connected to the upper surface of the sliding plate (32) in a sliding mode;

the drilling assembly (5) comprises a rotating motor (51), a main shaft (52), a chuck (53) and a drill bit (54), wherein the top end of the main shaft (52) is movably inserted into the output end of the rotating motor (51), the chuck (53) is clamped at the lower end inside the main shaft (52), and the drill bit (54) is clamped at the lower end inside the chuck (53).

2. The aerospace composite drilling device of claim 1, wherein: the supporting component (2) comprises a connecting plate (21), a fixing plate (22) and supporting columns (23), and the supporting columns (23) are located on two sides of the lower surface of the base plate (1).

3. An aerospace composite drilling apparatus as defined in claim 2, wherein: the connecting plate (21) is fixedly arranged on two sides of the upper surface of the bottom plate (1), the fixing plate (22) is fixedly arranged on the upper surface of the connecting plate (21), and the fixing plate (22) is positioned above the bottom plate (1).

4. An aerospace composite drilling apparatus as defined in claim 2, wherein: a through hole (221) is formed in the middle of the inner portion of the fixing plate (22), the spindle (52) is inserted into the through hole (221), and the rotating motor (51) is fixedly installed in the middle of the upper surface of the fixing plate (22).

5. The aerospace composite drilling device of claim 1, wherein: the driving assembly (4) comprises a transverse electric push rod (41), a longitudinal electric push rod (43) and a backup plate (42), the top end of the transverse electric push rod (41) is fixedly inserted into one side of the inside of the connecting plate (21), the tail end of the transverse electric push rod (41) is fixedly inserted into one side of the inside of the sliding plate (32), the top end of the longitudinal electric push rod (43) is fixedly inserted into one side of the inside of the backup plate (42), and the tail end of the longitudinal electric push rod (43) is fixedly inserted into one side of the inside of the sliding block (33).

6. The aerospace composite drilling device of claim 1, wherein: the driving assembly (4) further comprises a control panel (44), a first travel switch (441) and a second travel switch (442) are arranged on the upper surface of the control panel (44), the first travel switch (441) is electrically connected with the transverse electric push rod (41), and the second travel switch (442) is electrically connected with the longitudinal electric push rod (43).

7. The aerospace composite drilling device of claim 1, wherein: slide (32) inside spout (321) have been seted up, slider (33) lower surface sliding connection is inside spout (321), draw-in groove (331) have been seted up to slider (33) inside upper end both sides, draw-in groove (331) lower extreme has been seted up and has been dodged groove (332).