CN218655686U - Surface cleaning device for aircraft tire production - Google Patents
Surface cleaning device for aircraft tire production Download PDFInfo
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- CN218655686U CN218655686U CN202222685630.XU CN202222685630U CN218655686U CN 218655686 U CN218655686 U CN 218655686U CN 202222685630 U CN202222685630 U CN 202222685630U CN 218655686 U CN218655686 U CN 218655686U
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- fixedly connected
- wall
- cleaning
- connecting groove
- lagging
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02W—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO WASTEWATER TREATMENT OR WASTE MANAGEMENT
- Y02W30/00—Technologies for solid waste management
- Y02W30/50—Reuse, recycling or recovery technologies
- Y02W30/62—Plastics recycling; Rubber recycling
Abstract
The utility model provides a surface cleaning device for aviation tire production, which belongs to the technical field of aviation tire cleaning devices and comprises a cleaning sleeve plate, wherein the front end of the cleaning sleeve plate is provided with a fixed groove, and the lower inner wall of the fixed groove is fixedly connected with a first motor; the first connecting groove is formed in the lower inner wall of the fixing groove; second spread groove, the upside that can wash aircraft tire when the cleaning brush rotates, then the staff uses the controller to start to first motor control, and when first motor started, first motor can drive the part operation among the wiper mechanism, and the part operation among the wiper mechanism, then can wash aircraft tire's surface through cleaning component, and the cleaning performance is high when making personnel wasing aircraft tire to the efficiency of washing tire can promote.
Description
Technical Field
The utility model belongs to the technical field of the aircraft tire belt cleaning device, concretely relates to surface cleaning device is used in aircraft tire production.
Background
Aircraft tires are commonly known as aircraft tires. Aircraft tires are important components on aircraft where safety and reliability requirements are high. Safe takeoff and landing of an aircraft must rely on the various unique functions of the aircraft tires.
The rubber tire is a circular ring-shaped elastic rubber product which is assembled on a vehicle and rolls in a grounding way, can bear various deformations and loads, can provide support for a vehicle body when the vehicle runs, buffers external impact, realizes contact with a road surface and ensures the running performance of the vehicle, and almost all road vehicles use the rubber tire due to the excellent performance of the rubber tire.
The rubber tire has high surface roughness and certain adhesion, so that the surface of the tire is easily contaminated by dust in the production process of the rubber tire, the tire needs to be cleaned before packaging and selling, and the automobile tire is difficult to clean in the manual cleaning process due to various irregular dents on the surface, wastes time and labor and is difficult to clean the inner part of the tire.
Authorizing publication number "CN211070542U" has recorded a belt cleaning device for tire production and processing, comprises a workbench, the fixed curb plate that is equipped with on workstation one side, the fixed roof that is equipped with on the curb plate, the roof is kept away from the fixed cylinder that is equipped with of curb plate one end, the fixed disk is fixed down and is equipped with the fixed disk, the fixed disk is fixed down and is equipped with first drum, the fixed column is fixed down to be equipped with in the fixed disk middle part, fixed column lower extreme both sides are all fixed and are equipped with a plurality of shower nozzles, fixed disk lower wall both sides are all fixed and are equipped with a plurality of shower nozzles, first drum both sides inner wall is all fixed and is equipped with a plurality of shower nozzles, the fixed booster pump that is equipped with on the roof. Has the advantages that: can drive the tire and carry out slow rotation to can wash the interior outer wall of tire simultaneously, the sanitization, it is efficient.
Above-mentioned patent can drive the tire and slowly rotate to can wash the inside and outside wall of tire simultaneously, the sanitization, it is efficient, nevertheless above-mentioned patent is difficult for realizing wasing aircraft tyre comprehensively, makes to be relatively poor to aircraft tyre cleaning performance, and the cleaning efficiency is extremely low.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a surface cleaning device is used in aircraft tire production aims at solving the tire cleaning device among the prior art and can not realize wasing aircraft tire comprehensively, makes at relatively poor to aircraft tire cleaning performance to the problem that cleaning efficiency is extremely low.
In order to achieve the above object, the utility model provides a following technical scheme:
a surface cleaning apparatus for aircraft tire production, comprising:
the cleaning sleeve plate is characterized in that the front end of the cleaning sleeve plate is provided with a fixing groove, and the lower inner wall of the fixing groove is fixedly connected with a first motor;
the first connecting groove is formed in the lower inner wall of the fixing groove;
the second connecting groove is formed in the circumferential inner wall of the first connecting groove;
the cylinder is fixedly connected to the top end of the cleaning sleeve plate;
the concave plate is fixedly connected to the telescopic end of the cylinder;
the second motor is fixedly connected in the concave plate;
the cleaning brush is rotationally connected to the lower inner wall of the concave plate; and
and the cleaning mechanism is arranged in the second connecting groove and is connected with the second connecting groove to clean the aircraft tire.
As an optimized scheme of the utility model, wiper mechanism includes:
the rotating rod is rotatably connected to the upper inner wall and the lower inner wall of the second connecting groove;
the first gear is fixedly connected to the circumferential inner wall of the rotating rod;
the second gear is arranged in the second connecting groove;
the sliding grooves are formed in the upper inner wall and the lower inner wall of the second connecting groove;
the two limiting plates are fixedly connected to the upper inner wall and the lower inner wall of the two second gears respectively;
the connecting sleeve is arranged on the upper side of the second gear;
the plastic washs the piece, the plastic washs the piece and is equipped with a plurality ofly, and is a plurality of the equal fixed connection of plastic washing piece is in connecting sleeve's circumference inner wall.
As an optimal scheme, four connecting plates of the end inner wall fixedly connected with of first connecting groove, the circumference inner wall fixedly connected with second plastic circle of first connecting groove.
As an optimal scheme, the equal fixedly connected with backup pad in bottom four corners department of wasing the lagging, the bottom fixedly connected with conveying pipe of wasing the lagging, the circumference fixed surface of conveying pipe is connected with the valve.
As an optimized scheme, wherein two the end of being close to mutually of backup pad is two second fixed plates of fixedly connected with respectively, wash a side end fixedly connected with controller of lagging, wash the first plastic circle of the equal fixedly connected with in both ends of lagging.
As an optimized scheme, the top of wasing the lagging all articulates through the hinge activity has the apron, two first fixed plates of a side end fixedly connected with of apron, two the equal threaded connection in top of first fixed plate has first bolt, two the equal threaded connection in top of wasing the lagging of first bolt.
Compared with the prior art, the beneficial effects of the utility model are that:
1. in this scheme, personnel when needing to wash aircraft tire, personnel can place needs abluent tire in first connecting groove, then the staff will need to place the abluent liquid of aircraft tire in first connecting groove, the staff uses the controller to control the cylinder start afterwards, when the cylinder starts, the flexible end of cylinder can drive first connecting groove and descend, the position that the concave plate descends can be selected according to personnel's needs, then the staff uses the controller to control the second motor and starts, the output shaft of second motor can drive the cleaning brush and rotate, can wash aircraft tire's upside when the cleaning brush rotates, then the staff uses the controller to control the first motor and starts, when the first motor starts, first motor can drive the part operation in the wiper mechanism, then can wash aircraft tire's surface through the cleaning part, make personnel when wasing aircraft tire cleaning the cleaning effect, and the efficiency of wasing tire can promote.
2. In this scheme, the backup pad adopts the welded mode to fix in the bottom four corners department of wasing the lagging, the backup pad is used for supporting the bottom four corners department of wasing the lagging, the conveying pipe adopts the welded mode to fix in the bottom of wasing the lagging, the conveying pipe with wash the lagging intercommunication, the conveying pipe is used for the liquid discharge with first connecting groove, the valve adopts the mode height that can dismantle the connection at the circumference surface of conveying pipe, the valve block of valve itself can be used to seal the liquid in the conveying pipe.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:
fig. 1 is a perspective view of the present invention;
fig. 2 is a first perspective view of the present invention;
fig. 3 is a first perspective view, cut-away and perspective view of the present invention;
fig. 4 is a partial enlarged view of a portion a in fig. 3 according to the present invention;
fig. 5 is a third perspective view of the present invention;
fig. 6 is a partial enlarged view of the position B in fig. 5 according to the present invention.
In the figure: 1. cleaning the sleeve plate; 2. a controller; 3. a support plate; 4. a first plastic ring; 5. a cover plate; 6. a first fixing plate; 7. a first bolt; 8. a cylinder; 9. fixing grooves; 10. a delivery tube; 11. a valve; 12. a connecting plate; 13. plastic cleaning blocks; 14. a connecting sleeve; 15. a second plastic ring; 16. a first connecting groove; 17. a second fixing plate; 18. a second bolt; 19. a second gear; 20. a second connecting groove; 21. rotating the rod; 22. a chute; 23. a limiting plate; 24. a first gear; 25. a first motor; 26. a concave plate; 27. a second motor; 28. and (4) cleaning brushes.
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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts all belong to the protection scope of the present invention.
Example 1
Referring to fig. 1-6, the present invention provides the following technical solutions:
a surface cleaning device for aircraft tire production, comprising:
the cleaning sleeve plate 1 is characterized in that the front end of the cleaning sleeve plate 1 is provided with a fixing groove 9, and the lower inner wall of the fixing groove 9 is fixedly connected with a first motor 25;
the first connecting groove 16 is formed in the lower inner wall of the fixing groove 9;
the second connecting groove 20 is formed in the circumferential inner wall of the first connecting groove 16;
the cylinder 8 is fixedly connected to the top end of the cleaning sleeve plate 1;
a concave plate 26, wherein the concave plate 26 is fixedly connected with the telescopic end of the cylinder 8;
the second motor 27, the second motor 27 is fixedly connected in the concave plate 26;
a washing brush 28, wherein the washing brush 28 is rotatably connected to the lower inner wall of the concave plate 26; and
the wiper mechanism, wiper mechanism locate in second spread groove 20, and wiper mechanism and second spread groove 20 are connected in order to wash aircraft tire.
In the embodiment of the present invention, the cylinder 8 is detachably connected to the top end of the cleaning sleeve plate 1, the telescopic end of the cylinder 8 is connected to the cleaning sleeve plate 1, the cover plate 5 is fixed to the top end of the cleaning sleeve plate 1 by a hinge, two first fixing plates 6 are fixed to one side end of the cover plate 5 by welding, when a person needs to fix two first fixing plates 6 to the top end of the cleaning sleeve plate 1, the person can use a tool to rotate the first bolt 7, then the first bolt 7 can penetrate the first fixing plate 6 by screw thread and be connected to the top end of the cleaning sleeve plate 1 by screw thread, so as to fix the cleaning sleeve plate 1, the controller 2 is detachably connected to one side end of the cleaning sleeve plate 1, the controller 2 is used to control and start the cylinder 8, the second motor 27 and the first motor 25, controller 2 and cylinder 8, second motor 27, first motor 25 electric connection, first plastic ring 4 adopts the mode of bonding to fix at the both ends of wasing lagging 1, first plastic ring 4 is used for protecting wasing the both ends of lagging 1, the circumference inner wall at first connecting groove 16 is seted up to second connecting groove 20, first connecting groove 16 is seted up at the lower inner wall of fixed slot 9, be used for accomodating the aircraft tire in the first connecting groove 16, the top threaded connection of connecting sleeve 14 has a plurality of second bolts 18, the equal threaded through connection sleeve 14 of a plurality of second bolts 18 and threaded connection are in the top of second gear 19, conveying pipe 10 adopts the welded mode to fix in the bottom of wasing lagging 1, conveying pipe 10 and wasing lagging 1 intercommunication, conveying pipe 10 is used for discharging the liquid that washs the aircraft tire, it is required to explain: the specific types of the second motor 27, the first motor 25, the cylinder 8 and the controller 2 are selected by a person skilled in the art, and the second motor 27, the first motor 25, the cylinder 8 and the controller 2 are all in the prior art, and the detailed description is omitted.
Referring specifically to fig. 1-6, the cleaning mechanism includes:
a rotating rod 21, wherein the rotating rod 21 is rotatably connected with the upper and lower inner walls of the second connecting groove 20;
a first gear 24, the first gear 24 being fixedly connected to a circumferential inner wall of the rotating lever 21;
a second gear 19, the second gear 19 is arranged in the second connecting groove 20;
the sliding groove 22 is formed in the upper inner wall and the lower inner wall of the second connecting groove 20;
two limiting plates 23 are arranged, and the two limiting plates 23 are respectively and fixedly connected to the upper inner wall and the lower inner wall of the two second gears 19;
a coupling sleeve 14, the coupling sleeve 14 being provided on an upper side of the second gear 19;
the plastic cleaning blocks 13 are arranged, the number of the plastic cleaning blocks 13 is multiple, and the plastic cleaning blocks 13 are fixedly connected to the inner circumferential wall of the connecting sleeve 14.
In this embodiment: first motor 25 adopts the mode of dismantling the connection to fix on the top of wasing lagging 1, the lower inner wall of first motor 25 runs through the lower inner wall and fixed connection in dwang 21 of fixed slot 9 on the circumferential surface, consequently dwang 21 is when starting, dwang 21 can rotate and drive first gear 24 and rotate, first gear 24 can drive second gear 19 when rotating and rotate, second gear 19 and first gear 24 mesh mutually, second gear 19 can drive the fixed connecting sleeve 14 rotation of circumference inner wall when rotating, connecting sleeve 14 can drive a plurality of plastics and wash piece 13 and rotate when rotating, make a plurality of plastics wash piece 13 come to wash the surface of the aircraft tire in the first connecting groove 16.
Specifically referring to fig. 3, four connecting plates 12 are fixedly connected to the bottom inner wall of the first connecting groove 16, and a second plastic ring 15 is fixedly connected to the circumferential inner wall of the first connecting groove 16.
In this embodiment: the four connecting plates 12 are fixed on the upper inner wall of the first connecting groove 16 in a welding mode, the second plastic ring 15 is fixed on the circumferential inner wall of the first connecting groove 16 in a bonding mode, and the first connecting groove 16 is used for protecting the circumferential inner wall of the first connecting groove 16.
Specifically, referring to fig. 4, the four corners of the bottom end of the cleaning sheathing plate 1 are fixedly connected with the supporting plates 3, the bottom end of the cleaning sheathing plate 1 is fixedly connected with the conveying pipe 10, and the circumferential surface of the conveying pipe 10 is fixedly connected with the valve 11.
In this embodiment: backup pad 3 adopts the welded mode to fix in the bottom four corners department that washs lagging 1, backup pad 3 is used for supporting the bottom four corners department that washs lagging 1, conveying pipe 10 adopts the welded mode to fix in the bottom that washs lagging 1, conveying pipe 10 and the intercommunication of wasing lagging 1, conveying pipe 10 is used for the liquid discharge in the first connecting groove 16, valve 11 adopts the mode height that can dismantle the connection at conveying pipe 10's circumference surface, valve 11 itself the valve block can be used to seal the liquid in conveying pipe 10.
Referring to fig. 3, two second fixing plates 17 are fixedly connected to the adjacent ends of the two supporting plates 3, respectively, a controller 2 is fixedly connected to one side end of the cleaning sleeve plate 1, and first plastic rings 4 are fixedly connected to both ends of the cleaning sleeve plate 1.
In this embodiment: the second fixing plate 17 is fixed at the near end of two support plates 3 by welding, a threaded hole is formed in the middle of the top end of the second fixing plate 17, the controller 2 is fixed at one side end of the cleaning sleeve plate 1 by adopting a detachable connection mode, and the controller 2 is used for controlling the starting of the second motor 27, the first motor 25 and the cylinder 8.
The utility model discloses a theory of operation and use flow: when a worker needs to clean an aircraft tire, the worker can place the tire to be cleaned in the first connecting groove 16, then the worker places liquid to be cleaned on the aircraft tire in the first connecting groove 16, then the worker controls and starts the cylinder 8 by using the controller 2, when the cylinder 8 is started, the telescopic end of the cylinder 8 can drive the first connecting groove 16 to descend, the position where the concave plate 26 descends can be selected according to the requirement of the worker, then the worker controls and starts the second motor 27 by using the controller 2, the output shaft of the second motor 27 can drive the cleaning brush 28 to rotate, when the cleaning brush 28 rotates, the upper side of the aircraft tire can be cleaned, then the worker controls and starts the first motor 25 by using the controller 2, when the first motor 25 is started, the output shaft of the first motor 25 can drive the rotating rod 21 to rotate, when the rotating rod 21 rotates the first gear 24, then the first gear 24 drives the rotating rod 21 to rotate, when the first gear 24 rotates, when the second gear 19 drives the rotating rod to rotate, when the second gear 14 rotates, and when the plastic sleeve 14 rotates, and the plastic tire is cleaned in all-direction.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (6)
1. A surface cleaning device for aircraft tire production, comprising:
the cleaning sleeve plate comprises a cleaning sleeve plate (1), wherein the front end of the cleaning sleeve plate (1) is provided with a fixing groove (9), and the lower inner wall of the fixing groove (9) is fixedly connected with a first motor (25);
the first connecting groove (16) is formed in the lower inner wall of the fixing groove (9);
the second connecting groove (20), the said second connecting groove (20) is opened in the circumference inner wall of the first connecting groove (16);
the cylinder (8), the said cylinder (8) is fixedly connected to the top end of the cleaning lagging (1);
the concave plate (26), the said concave plate (26) is fixedly connected to the telescopic end of the cylinder (8);
the second motor (27), the said second motor (27) is fixedly connected to the concave plate (26);
a washing brush (28), wherein the washing brush (28) is rotatably connected to the lower inner wall of the concave plate (26); and
the cleaning mechanism is arranged in the second connecting groove (20), and the cleaning mechanism is connected with the second connecting groove (20) to clean the aircraft tire.
2. The surface cleaning device for aircraft tire production according to claim 1, wherein: the cleaning mechanism includes:
the rotating rod (21) is rotatably connected to the upper inner wall and the lower inner wall of the second connecting groove (20);
the first gear (24), the said first gear (24) is fixedly connected to the circumference inner wall of the dwang (21);
a second gear (19), the second gear (19) being disposed within a second connecting slot (20);
the sliding groove (22), the sliding groove (22) is arranged on the upper and lower inner walls of the second connecting groove (20);
two limiting plates (23) are arranged, and the two limiting plates (23) are respectively and fixedly connected to the upper inner wall and the lower inner wall of the two second gears (19);
a connecting sleeve (14), wherein the connecting sleeve (14) is arranged on the upper side of the second gear (19);
the plastic cleaning block (13), the plastic cleaning block (13) is equipped with a plurality of, a plurality of the equal fixed connection of plastic cleaning block (13) is in the circumference inner wall of connecting sleeve (14).
3. The surface cleaning device for aircraft tire production according to claim 2, wherein: the bottom inner wall of the first connecting groove (16) is fixedly connected with four connecting plates (12), and the circumferential inner wall of the first connecting groove (16) is fixedly connected with a second plastic ring (15).
4. A surface cleaning device for aircraft tire production according to claim 3, wherein: the bottom four corners department of wasing lagging (1) all fixedly connected with backup pad (3), the bottom fixedly connected with conveying pipe (10) of wasing lagging (1), the circumference fixed surface of conveying pipe (10) is connected with valve (11).
5. The surface cleaning device for aircraft tire production according to claim 4, wherein: wherein two the end that is close to mutually of backup pad (3) is two second fixed plates (17) of fixedly connected with respectively, wash one side end fixedly connected with controller (2) of lagging (1), wash the equal fixedly connected with first plastic ring (4) in both ends of lagging (1).
6. The surface cleaning device for aircraft tire production according to claim 5, wherein: the top of wasing lagging (1) all articulates through the hinge activity has apron (5), one side end fixedly connected with of apron (5) has two first fixed plates (6), two the equal threaded connection in top of first fixed plate (6) has first bolt (7), two the equal threaded connection in top of wasing lagging (1) of first bolt (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222685630.XU CN218655686U (en) | 2022-10-12 | 2022-10-12 | Surface cleaning device for aircraft tire production |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222685630.XU CN218655686U (en) | 2022-10-12 | 2022-10-12 | Surface cleaning device for aircraft tire production |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218655686U true CN218655686U (en) | 2023-03-21 |
Family
ID=85562800
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222685630.XU Active CN218655686U (en) | 2022-10-12 | 2022-10-12 | Surface cleaning device for aircraft tire production |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218655686U (en) |
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2022
- 2022-10-12 CN CN202222685630.XU patent/CN218655686U/en active Active
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