CN213494617U - Surface spraying device for aerospace equipment parts - Google Patents
Surface spraying device for aerospace equipment parts Download PDFInfo
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- CN213494617U CN213494617U CN202022279462.5U CN202022279462U CN213494617U CN 213494617 U CN213494617 U CN 213494617U CN 202022279462 U CN202022279462 U CN 202022279462U CN 213494617 U CN213494617 U CN 213494617U
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- 238000005507 spraying Methods 0.000 title claims abstract description 74
- 230000001105 regulatory effect Effects 0.000 claims abstract description 7
- 230000005540 biological transmission Effects 0.000 claims description 5
- 230000000694 effects Effects 0.000 abstract description 6
- 238000001125 extrusion Methods 0.000 abstract description 5
- 239000007921 spray Substances 0.000 abstract description 4
- 230000003014 reinforcing effect Effects 0.000 abstract 1
- 239000011248 coating agent Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
- 238000002791 soaking Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000007590 electrostatic spraying Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 238000007751 thermal spraying Methods 0.000 description 1
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Abstract
The utility model relates to a spraying technical field especially relates to a surface spraying device for aerospace equipment spare part, the spare part that has proposed current aerospace equipment carries out the surface spraying when, traditional spraying mode is through carrying out the spraying to the spare part surface to the spray gun and is handled, but some four corners or turning of part are hardly by even spraying, the problem of spraying effect has been reduced, it includes the spraying case, the bottom lateral wall of spraying case is fixed with places the case, sliding connection has the regulating plate between the both sides inner wall of placing the case, the top of regulating plate extends to and places case external fixation and has the roof, top one side of spraying case is fixed with first backup pad, the top lateral wall of first backup pad is fixed with driving motor. The utility model discloses in drive the cam through rotating electrical machines and rotate, the cam carries out the extrusion that circulates to the stripper plate, makes the stripper plate drive the slide and carries out the round trip movement, and the slide can drive the connecting plate, and the connecting plate drives the spraying case and carries out the round trip movement, reinforcing spraying effect.
Description
Technical Field
The utility model relates to a spraying technical field especially relates to a surface spraying device for aerospace equipment spare part.
Background
The spray coating is applied to the surface of the object to be coated by dispersing into uniform and fine droplets by means of a spray gun or a disc atomizer by means of pressure or centrifugal force. It can be divided into air spraying, airless spraying, electrostatic spraying and various derivatives of the above basic spraying forms, such as high flow low pressure atomized spraying, thermal spraying, automatic spraying, multiple spray groups, etc.
When the surface of the part of the existing aerospace equipment is sprayed, the surface of the part is sprayed by a spraying gun in the traditional spraying mode, but the four corners or corners of the part are difficult to be uniformly sprayed, so that the spraying effect is reduced.
To this end, we propose a surface coating device for aerospace equipment parts.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving when the spare part of current aerospace equipment carries out the surface coating, traditional spraying mode is through carrying out spray coating to the spare part surface to the spray gun, but some four corners of part or turning are hardly by even spraying, have reduced the problem of spraying effect, and the surface coating device who is used for aerospace equipment spare part that proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
a surface spraying device for aerospace equipment parts comprises a spraying box, wherein a placing box is fixed on the side wall of the bottom end of the spraying box, an adjusting plate is connected between the inner walls of two sides of the placing box in a sliding mode, the top end of the adjusting plate extends to the outside of the placing box and is fixed with a top plate, a first supporting plate is fixed on one side of the top end of the spraying box, a driving motor is fixed on the side wall of the top end of the first supporting plate, an output shaft of the driving motor is fixed with a first connecting shaft through a coupler, one end, far away from the driving motor, of the first connecting shaft penetrates through the first supporting plate to be rotatably connected with the side wall of the bottom end of the spraying box, a second connecting shaft is rotatably connected between the inner walls of two sides of the spraying box, a worm is sleeved on the outer side wall of the second connecting shaft in a tight fit manner, a worm wheel is tightly sleeved on the outer side, one end of the second connecting shaft penetrates through the first through hole, a gear is sleeved on the outer side wall of the second connecting shaft in a tight fit mode and is located inside the first through hole, a plurality of racks are arranged on the side wall of one side of the first through hole along the length direction of the side wall, and the gear and the racks are in meshed transmission connection.
Preferably, the outer side wall of the placing box is provided with second through holes symmetrically arranged, the second through holes are communicated with the inside of the placing box, and the top plate is positioned right above the placing box.
Preferably, a second support plate is arranged below the spraying box, symmetrically arranged support seats are fixed on the side wall of the bottom end of the second support plate, and a first groove is formed in the side wall of the top end of the second support plate.
Preferably, the sliding plates are symmetrically arranged and are slidably connected between the side walls of the two sides of the first groove, the side wall of the top end of each sliding plate is fixedly provided with a connecting plate, one end, far away from the sliding plates, of each connecting plate is fixed to the side wall of the bottom of the spraying box, and the connecting plates are vertically arranged with the sliding plates.
Preferably, a return spring fixed with the first groove is installed on one side wall of one of the sliding plates, which is far away from each other, and a squeezing plate is fixed on one side wall of the sliding plate, which is far away from the return spring, and the squeezing plate and the sliding plate are vertically arranged.
Preferably, a rotating motor is fixed on the side wall of the bottom end of the second supporting plate, a driving shaft is fixed on an output shaft of the rotating motor through a coupler, and a cam is fixed inside the first groove and extends to one end, far away from the rotating motor, of the driving shaft.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses in through placing case and spraying case, pour the spraying night into spraying incasement portion, soak the spraying to the part, can soak the spraying to the whole aspect of part, avoid appearing the dead angle or the turning is not sprayed, improved the practicality of spraying;
2. in the utility model, the cam is driven to rotate by the rotating motor, and the cam circularly extrudes the extrusion plate, so that the extrusion plate drives the sliding plate to move back and forth, the sliding plate can drive the connecting plate, and the connecting plate drives the spraying box to move back and forth, thereby enhancing the spraying effect;
3. the utility model discloses in drive first connecting axle through driving motor and rotate, first connecting axle drives the second connecting axle and rotates, and the second connecting axle drives the regulating plate through gear drive and removes, and the regulating plate carries out ejecting ejection of compact to the part, has improved the convenience.
Drawings
Fig. 1 is a front view of the structure of a surface spraying device for aerospace equipment components and parts according to the present invention.
Fig. 2 is a structural plan view of the surface spraying device for aerospace equipment components and parts according to the present invention.
Fig. 3 is the utility model provides a worm wheel and worm cooperation schematic structure for surface coating device of aerospace equipment spare part.
Fig. 4 is a side view of the adjusting plate structure of the surface spraying device for aerospace equipment components and parts provided by the present invention.
Reference numbers in the figures: the automatic spraying device comprises a spraying box 1, a placing box 2, an adjusting plate 3, a top plate 4, a second through hole 5, a first supporting plate 6, a driving motor 7, a first connecting shaft 8, a second connecting shaft 9, a worm wheel 10, a worm 11, a second supporting plate 12, a first groove 13, a sliding plate 14, a connecting plate 15, a squeezing plate 16, a return spring 17, a rotating motor 18, a cam 19, a supporting seat 20, a first through hole 21, a rack 22 and a gear 23.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Referring to fig. 1-4, a surface spraying device for aerospace equipment components comprises a spraying box 1, a placing box 2 is fixed on the bottom side wall of the spraying box 1, an adjusting plate 3 is slidably connected between the two side inner walls of the placing box 2, a top plate 4 is fixed on the top end of the adjusting plate 3 extending to the outside of the placing box 2, a first supporting plate 6 is fixed on one side of the top end of the spraying box 1, a driving motor 7 is fixed on the top side wall of the first supporting plate 6, a first connecting shaft 8 is fixed on the output shaft of the driving motor 7 through a coupler, one end of the first connecting shaft 8 far away from the driving motor 7 penetrates through the first supporting plate 6 to be rotatably connected with the bottom side wall of the spraying box 1, a second connecting shaft 9 is rotatably connected between the two side inner walls of the spraying box 1, a worm 11 is tightly fitted and sleeved on the outer side wall of the second connecting shaft 9, a worm, and the worm 11 is in meshing transmission connection with the worm wheel 10, a first through hole 21 penetrating left and right is formed in the adjusting plate 3, one end of the second connecting shaft 9 penetrates through the first through hole 21, a gear 23 is sleeved on the outer side wall of the second connecting shaft 9 in a tight fit mode, the gear 23 is located inside the first through hole 21, a plurality of racks 22 are formed in the side wall of one side of the first through hole 21 along the length direction of the side wall, and the gear 23 is in meshing transmission connection with the racks 22.
Place the second through-hole 5 that the symmetry set up is seted up to the lateral wall of case 2, second through-hole 5 with place 2 inside intercommunications of case, and roof 4 is located and places case 2 directly over, the below of spraying case 1 is provided with second backup pad 12, the bottom lateral wall of second backup pad 12 is fixed with the supporting seat 20 that the symmetry set up, first recess 13 has been seted up to the top lateral wall of second backup pad 12, sliding connection has the slide 14 that the symmetry set up between the both sides lateral wall of first recess 13, the top lateral wall of slide 14 is fixed with connecting plate 15, the one end that slide 14 was kept away from to connecting plate 15 is fixed with spraying case 1 bottom lateral wall, and set up perpendicularly between connecting plate 15 and the slide 14.
One side lateral wall that one of them slide 14 kept away from each other is installed with the reset spring 17 fixed with first recess 13, and one side lateral wall that reset spring 17 was kept away from to slide 14 is fixed with stripper plate 16, and sets up perpendicularly between stripper plate 16 and the slide 14, and the bottom lateral wall of second backup pad 12 is fixed with rotating electrical machines 18, and rotating electrical machines 18's output shaft is fixed with the driving shaft through the shaft coupling, and the one end that rotating electrical machines 18 was kept away from to the driving shaft extends to first recess 13 inside and is fixed with cam 19.
The working principle is as follows: when the surface of a part is sprayed, spraying liquid is poured into the spraying box 1, the part is placed on the surface of the top plate 4, the part is soaked and covered, all-around spraying treatment is carried out, meanwhile, the rotating motor 18 is started, the rotating motor 18 drives the driving shaft to rotate, the driving shaft drives the cam 19 to rotate, the cam 19 carries out rapid extrusion treatment on the extrusion plate 16, the sliding plate 14 drives the connecting plate 15 to reciprocate, the connecting plate 15 drives the spraying box 1 to reciprocate, the soaking effect is improved, after soaking is finished, the driving motor 7 is started, the driving motor 7 drives the first connecting shaft 8 to rotate, the first connecting shaft 8 drives the worm wheel 10 to rotate, the worm wheel 10 and the worm 11 are meshed to drive the second connecting shaft 9 to rotate, the second connecting shaft 9 drives the gear 23 to rotate, the gear 23 and the rack 22 are meshed to drive the adjusting plate 3 to move, the adjusting plate 3 drives the top plate 4 to move upwards, and the top plate 4 ejects the parts out to discharge.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. A surface spraying device for aerospace equipment parts comprises a spraying box (1) and is characterized in that a placing box (2) is fixed on the bottom side wall of the spraying box (1), a regulating plate (3) is connected between the inner walls of two sides of the placing box (2) in a sliding mode, a top plate (4) is fixed on the top end of the regulating plate (3) and extends to the outside of the placing box (2), a first supporting plate (6) is fixed on one side of the top end of the spraying box (1), a driving motor (7) is fixed on the side wall of the top end of the first supporting plate (6), a first connecting shaft (8) is fixed on an output shaft of the driving motor (7) through a coupler, one end, far away from the driving motor (7), of the first connecting shaft (8) penetrates through the first supporting plate (6) to be connected with the bottom side wall of the spraying box (1) in a rotating mode, a second connecting shaft (9) is connected, worm (11) has been cup jointed in the lateral wall tight fit of second connecting axle (9), worm wheel (10) have been cup jointed in the lateral wall tight fit of first connecting axle (8), and mesh transmission is connected between worm (11) and worm wheel (10), first through-hole (21) that run through about seting up on regulating plate (3), first through-hole (21) are passed to the one end of second connecting axle (9), gear (23) have been cup jointed in the lateral wall tight fit of second connecting axle (9), and gear (23) are located inside first through-hole (21), a plurality of racks (22) have been seted up along its length direction to one side lateral wall of first through-hole (21), and mesh transmission is connected between gear (23) and rack (22).
2. The surface spraying device for the aerospace device parts as claimed in claim 1, wherein the outer side wall of the placing box (2) is provided with symmetrically arranged second through holes (5), the second through holes (5) are communicated with the inside of the placing box (2), and the top plate (4) is located right above the placing box (2).
3. The surface spraying device for the aerospace equipment components and parts as claimed in claim 1, wherein a second support plate (12) is arranged below the spraying box (1), symmetrically arranged support seats (20) are fixed on the side wall of the bottom end of the second support plate (12), and a first groove (13) is formed in the side wall of the top end of the second support plate (12).
4. The surface spraying device for the aerospace equipment parts and components as claimed in claim 3, wherein the sliding plates (14) are connected between the two side walls of the first groove (13) in a sliding manner, the top side walls of the sliding plates (14) are fixed with the connecting plates (15), one ends of the connecting plates (15) far away from the sliding plates (14) are fixed with the bottom side walls of the spraying box (1), and the connecting plates (15) are vertically arranged with the sliding plates (14).
5. The surface spraying device for the aerospace equipment parts and components according to claim 4, wherein a return spring (17) fixed with the first groove (13) is installed on one side wall of the sliding plate (14) far away from each other, a pressing plate (16) is fixed on one side wall of the sliding plate (14) far away from the return spring (17), and the pressing plate (16) and the sliding plate (14) are vertically arranged.
6. The surface spraying device for the aerospace equipment parts and components as claimed in claim 3, wherein a rotating motor (18) is fixed to the side wall of the bottom end of the second support plate (12), a driving shaft is fixed to an output shaft of the rotating motor (18) through a coupler, and a cam (19) is fixed to the inside of the first groove (13) and extends to one end, away from the rotating motor (18), of the driving shaft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022279462.5U CN213494617U (en) | 2020-10-14 | 2020-10-14 | Surface spraying device for aerospace equipment parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022279462.5U CN213494617U (en) | 2020-10-14 | 2020-10-14 | Surface spraying device for aerospace equipment parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213494617U true CN213494617U (en) | 2021-06-22 |
Family
ID=76397338
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022279462.5U Active CN213494617U (en) | 2020-10-14 | 2020-10-14 | Surface spraying device for aerospace equipment parts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213494617U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114082597A (en) * | 2021-11-19 | 2022-02-25 | 航天特种材料及工艺技术研究所 | Sleeving tool and sleeving method for cabin rigid closed type outer heat-proof layer |
-
2020
- 2020-10-14 CN CN202022279462.5U patent/CN213494617U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114082597A (en) * | 2021-11-19 | 2022-02-25 | 航天特种材料及工艺技术研究所 | Sleeving tool and sleeving method for cabin rigid closed type outer heat-proof layer |
| CN114082597B (en) * | 2021-11-19 | 2022-07-05 | 航天特种材料及工艺技术研究所 | Sleeving tool and sleeving method for cabin rigid closed type outer heat-proof layer |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220110 Address after: 102600 1114, floor 11, building 16, yard 1, Yongda Road, Daxing District, Beijing Patentee after: Beijing Zhongqian Technology Co.,Ltd. Address before: 510000 402, No.16, North Lu'an street, Guangzhou Avenue, Tianhe District, Guangzhou City, Guangdong Province Patentee before: Liu Kunming |
|
| TR01 | Transfer of patent right |