CN218696758U - Aviation tire grinding device - Google Patents
Aviation tire grinding device Download PDFInfo
- Publication number
- CN218696758U CN218696758U CN202222592423.XU CN202222592423U CN218696758U CN 218696758 U CN218696758 U CN 218696758U CN 202222592423 U CN202222592423 U CN 202222592423U CN 218696758 U CN218696758 U CN 218696758U
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- 238000005498 polishing Methods 0.000 claims abstract description 43
- 238000009434 installation Methods 0.000 claims abstract description 20
- 230000007246 mechanism Effects 0.000 claims description 23
- 230000000694 effects Effects 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 abstract description 5
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
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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
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Abstract
The utility model provides an aircraft tire polishing device, which belongs to the technical field of aircraft tire processing and comprises a bottom plate; the fixing plate is fixedly connected to the upper end of the bottom plate; the rotating plate is rotatably connected to one side end of the fixed plate; the output end of the third motor movably penetrates through one side end of the fixed plate and is fixed with one end of the rotating plate; grinding machanism, grinding machanism are equipped with the multiunit, and multiunit grinding machanism all locates in the rotor plate, when polishing through this device aircraft tire, will treat the wheel area of polishing and install the surface at tire installation pipe and can polish to the tire surface through this device is automatic, effectively improves the efficiency of polishing, improves aircraft tire's production efficiency.
Description
Technical Field
The utility model belongs to the technical field of the aircraft tire processing, concretely relates to aircraft tire grinding device.
Background
The aircraft tire is commonly called as an aircraft tire, the aircraft tire is an important part with high safety and reliability requirements on an aircraft, and the safe take-off and landing of the aircraft must depend on various unique functions of the aircraft tire;
the aviation tire needs to be produced through a series of processes, wherein after the tire is machined and molded, burrs on the surface of the tire need to be removed, and the surface of the tire needs to be polished by using a polishing tool after the removal, so that the flatness of the surface of the aviation tire is improved.
In the prior art, when the aircraft tire is polished, the tire is usually required to be installed in the device, a polishing tool is used, the surface of the tire is manually polished, the polishing efficiency is low, and the production efficiency of the aircraft tire is influenced.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aircraft tire grinding device aims at solving among the prior art aircraft tire when polishing, generally need install the tire in the device, uses the instrument of polishing, and the manual work is polished tire surface, and efficiency of polishing is on the low side, influences aircraft tire's production efficiency's problem.
In order to achieve the above purpose, the utility model provides a following technical scheme:
an aircraft tire buffing apparatus comprising:
a base plate;
the fixing plate is fixedly connected to the upper end of the bottom plate;
the rotating plate is rotatably connected to one side end of the fixed plate;
the output end of the third motor movably penetrates through one side end of the fixed plate and is fixed with one end of the rotating plate;
the polishing mechanisms are provided with a plurality of groups, and the polishing mechanisms are all arranged in the rotating plate;
the first motor is connected to the upper end of the bottom plate in a sliding mode through a sliding mechanism;
the mounting plate is fixedly connected to the output end of the first motor; and
the tire mounting pipe is fixedly connected to one side end of the mounting plate.
As a preferred scheme of the utility model, every group grinding mechanism all includes adjusting part and the subassembly of polishing, every group the subassembly of polishing all is connected with adjusting part.
As an optimized scheme, every group the adjusting part all includes spacing spout, first electric putter, spacing slider and second electric putter, a side end of rotor plate is seted up to spacing spout, spacing slider sliding connection is in spacing spout, first electric putter fixed connection is in one side inner wall of spacing spout, first electric putter's extension end fixed connection is in spacing slider's side, second electric putter fixed connection is in a side of spacing slider.
As a preferred scheme of the utility model, every group the subassembly of polishing all includes installation piece, fourth motor and the wheel of polishing, installation piece fixed connection is in second electric putter's extension end, fourth motor fixed connection is in an end of installation piece, the output activity of fourth motor runs through another end of installation piece and outside extension, wheel of polishing fixed connection is in the output of fourth motor.
As a preferred scheme, slide mechanism includes sliding tray, screw rod, first motor and screw slider, the upper end of bottom plate is seted up in the sliding tray, screw slider fixed connection is in the lower extreme of first motor, screw slider sliding connection is in the sliding tray, the screw rod rotates to be connected in the both sides inner wall of sliding tray, screw rod and screw slider threaded connection.
As an optimized scheme, a side end fixedly connected with second motor of bottom plate, the output activity of second motor runs through one side inner wall of sliding tray and is fixed with the one end of screw rod.
Compared with the prior art, the beneficial effects of the utility model are that:
1. in this scheme, when the aircraft tire is polished through this device, the wheel area that will treat to polish is installed and can be polished to the tire surface through this device is automatic on the surface of tire installation pipe, effectively improves the efficiency of polishing, improves aircraft tire's production efficiency.
2. In this scheme, control first motor drive mounting panel rotate to with fixed plate vertical position, then will treat the tire cover of polishing on the surface of tire installation pipe, control first motor drive mounting panel rotate to parallel with the fixed plate, control slide mechanism drive treat the tire of polishing remove to with the polishing wheel contact in the grinding machanism, adjust the position of polishing of wheel on tire surface through adjusting part.
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 an enlarged view of a portion A of FIG. 1;
fig. 3 is a top view of the present invention;
fig. 4 is a side view of the present invention.
In the figure: 1. a base plate; 2. a fixing plate; 3. a rotating plate; 4. a sliding groove; 5. a screw; 6. a first motor; 7. a threaded slider; 8. a second motor; 9. mounting a plate; 10. a tire mounting tube; 11. a third motor; 12. a limiting chute; 13. a first electric push rod; 14. a limiting slide block; 15. a second electric push rod; 16. mounting a block; 17. a fourth motor; 18. grinding the wheel; 19. a first limit plate; 20. a second limiting plate; 21. and a limiting sleeve.
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 work belong to the protection scope of the present invention.
Examples
Referring to fig. 1-4, the present invention provides the following technical solutions:
an aircraft tire buffing apparatus comprising:
a base plate 1;
the fixing plate 2 is fixedly connected to the upper end of the bottom plate 1;
the rotating plate 3 is rotatably connected to one side end of the fixed plate 2;
the third motor 11 is fixedly connected to the other side end of the fixed plate 2, and the output end of the third motor 11 movably penetrates through one side end of the fixed plate 2 and is fixed with one end of the rotating plate 3;
the polishing mechanisms are provided with a plurality of groups, and the plurality of groups of polishing mechanisms are all arranged in the rotating plate 3;
the first motor 6 is connected to the upper end of the bottom plate 1 in a sliding mode through a sliding mechanism;
the mounting plate 9, the mounting plate 9 is fixedly connected to the output end of the first electric motor 6; and
and the tire mounting tube 10 is fixedly connected to one side end of the mounting plate 9.
The utility model discloses an in the concrete embodiment, the slide mechanism who sets up in the bottom plate 1 is used for driving first motor 6 and removes, mounting panel 9 rotates through the operation of first motor 6, the fixed tire installation pipe 10 of mounting panel 9 side is used for the installation to treat the aircraft tire who polishes, aircraft tire cover is at the circumferential surface of tire installation pipe 10, first motor 6 drives mounting panel 9 and rotates to when being parallel with fixed plate 2, be used for polishing of aircraft tire, first motor 6 drives mounting panel 9 and rotates to when being perpendicular with fixed plate 2, be convenient for the installation and the dismantlement of tire, drive first motor 6 by slide mechanism, mounting panel 9, the tire that tire installation pipe 10 and tire installation pipe 10 circumferential surface set up removes to and contacts with grinding machanism, polish tire surface through grinding machanism, third motor 11 drives rotor plate 3 when the operation and rotates, it rotates to drive multiunit grinding machanism through rotation of rotor plate 3, under grinding machanism's rotation, evenly polish tire surface.
Referring to fig. 1-4, each polishing mechanism includes an adjusting component and a polishing component, and each polishing component is connected to the adjusting component.
In this embodiment: the adjusting assembly is used for controlling the grinding assembly to move, the grinding wheel 18 in the grinding assembly is in contact with the surface of the tire, and the grinding wheel 18 grinds the tire through the grinding materials on the surface of the grinding wheel in a rotating state.
Specifically, referring to fig. 1-4, each set of adjusting components includes a limiting sliding groove 12, a first electric push rod 13, a limiting sliding block 14, and a second electric push rod 15, the limiting sliding groove 12 is disposed at one side end of the rotating plate 3, the limiting sliding block 14 is slidably connected in the limiting sliding groove 12, the first electric push rod 13 is fixedly connected to an inner wall of one side of the limiting sliding groove 12, an extending end of the first electric push rod 13 is fixedly connected to a side end of the limiting sliding block 14, and the second electric push rod 15 is fixedly connected to one side end of the limiting sliding block 14.
In this embodiment: the limiting sliding groove 12 in the adjusting assembly is used for installing a first electric push rod 13, the first electric push rod 13 drives a limiting sliding block 14 with a fixed extending end to move when the first electric push rod is in operation, the limiting sliding block 14 drives a second electric push rod 15 to move, and the second electric push rod 15 drives a polishing assembly connected with the extending end to move.
Specifically, referring to fig. 1-4, each grinding assembly includes a mounting block 16, a fourth motor 17 and a grinding wheel 18, the mounting block 16 is fixedly connected to the extending end of the second electric push rod 15, the fourth motor 17 is fixedly connected to one side end of the mounting block 16, an output end of the fourth motor 17 movably penetrates through the other side end of the mounting block 16 and extends outward, and the grinding wheel 18 is fixedly connected to an output end of the fourth motor 17.
In this embodiment: a fourth motor 17 in the grinding assembly drives a grinding wheel 18 with a fixed output end to rotate when the grinding assembly operates, and the grinding wheel 18 is in contact with the tire in a rotating state to grind the surface of the tire.
Specifically, referring to fig. 1-4, the sliding mechanism includes a sliding groove 4, a screw rod 5, a first motor 6 and a threaded slider 7, the sliding groove 4 is disposed at the upper end of the bottom plate 1, the threaded slider 7 is fixedly connected to the lower end of the first motor 6, the threaded slider 7 is slidably connected to the sliding groove 4, the screw rod 5 is rotatably connected to the inner walls of the two sides of the sliding groove 4, and the screw rod 5 is in threaded connection with the threaded slider 7.
In this embodiment: a second motor 8 in the sliding mechanism drives a screw rod 5 with a fixed output end to rotate during operation, the screw rod 5 is in threaded connection with a threaded sliding block 7, the threaded sliding block 7 is driven to slide in a sliding groove 4 through rotation of the screw rod 5, and the threaded sliding block 7 drives a first motor 6 to slide, so that an aircraft tire to be polished is driven to be in contact with the polishing mechanism.
Preferably, all be equipped with spacing subassembly in every group grinding machanism, every group spacing subassembly all includes first limiting plate 19, second limiting plate 20 and spacing sleeve 21, it all is equipped with two to complain first limiting plate 19 and spacing sleeve 21 of fox, two first limiting plate 19 respectively fixed connection in two sides of installation piece 16, second limiting plate 20 fixed connection in second electric putter 15's one end, two spacing sleeve 21 respectively fixed connection in first limiting plate 19 and second limiting plate 20 lean on the near-end mutually, every first limiting plate 19 comprises slender pole and sleeve, the one end at first limiting plate 19 is fixed to the slender pole, the one end at second limiting plate 20 is fixed to the sleeve, slender pole sliding connection is in the sleeve, be used for spacing to installation piece 16, improve the stability of installation piece 16 when the removal.
Specifically, referring to fig. 1-4, a second motor 8 is fixedly connected to one side of the bottom plate 1, and an output end of the second motor 8 movably penetrates through an inner wall of one side of the sliding slot 4 and is fixed to one end of the screw 5.
In this embodiment: the second motor 8 drives the screw 5 fixed at the output end to rotate when in operation, thereby driving the sliding mechanism to operate; the first motor 6, the second motor 8, the third motor 11, the fourth motor 17, the first electric push rod 13 and the second electric push rod 15 used in the device are all the prior art, and are not described herein in any greater detail.
The utility model discloses a theory of operation and use flow: when the device is used, firstly, the first motor 6 is controlled to drive the mounting plate 9 to rotate to a position vertical to the fixed plate 2, then a tire to be polished is sleeved on the surface of the tire mounting pipe 10, the first motor 6 is controlled to drive the mounting plate 9 to rotate to be parallel to the fixed plate 2, the sliding mechanism is controlled to drive the tire to be polished to move to be in contact with the polishing wheel 18 in the polishing mechanism, the polishing position of the polishing wheel 18 on the surface of the tire is adjusted through the adjusting assembly, then burrs on the surface of the tire are polished through the operation of the polishing assembly, after polishing is completed, the sliding mechanism is controlled to drive the first motor 6 to move towards the direction far away from one side of the fixed plate 2, after the tire is moved to a certain position, the first motor 6 is controlled to operate to drive the mounting plate 9 to rotate to be vertical to the fixed plate 2, and then the polished tire belt is taken down from the surface of the tire mounting pipe 10; when the aircraft tire is polished by the device, the wheel belt to be polished is arranged on the surface of the tire mounting pipe 10, so that the tire surface can be polished automatically by the device, the polishing efficiency is effectively improved, and the production efficiency of the aircraft tire is improved.
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. An aircraft tire buffing apparatus, comprising:
a base plate (1);
the fixing plate (2), the said fixing plate (2) is fixedly connected to the upper end of the bottom plate (1);
the rotating plate (3), the rotating plate (3) is rotatably connected to one side end of the fixed plate (2);
the third motor (11) is fixedly connected to the other side end of the fixed plate (2), and the output end of the third motor (11) movably penetrates through one side end of the fixed plate (2) and is fixed with one end of the rotating plate (3);
the polishing mechanisms are provided with a plurality of groups, and the plurality of groups of polishing mechanisms are all arranged in the rotating plate (3);
the first motor (6) is connected to the upper end of the bottom plate (1) in a sliding mode through a sliding mechanism;
the mounting plate (9), the said mounting plate (9) is fixedly connected to the output end of the first electrical machinery (6); and
the tire mounting pipe (10), tire mounting pipe (10) fixed connection is in the one side end of mounting panel (9).
2. An aircraft tire buffing apparatus according to claim 1 wherein: every group grinding machanism all includes adjusting part and the subassembly of polishing, every group the subassembly of polishing all is connected with adjusting part.
3. An aircraft tire buffing apparatus according to claim 2 wherein: every group the adjusting part all includes spacing spout (12), first electric putter (13), limiting slide (14) and second electric putter (15), a side of rotor plate (3) is seted up in spacing spout (12), limiting slide (14) sliding connection is in spacing spout (12), first electric putter (13) fixed connection is in one side inner wall of spacing spout (12), the extension end fixed connection of first electric putter (13) is in the side of limiting slide (14), second electric putter (15) fixed connection is in a side of limiting slide (14).
4. An aircraft tire buffing apparatus according to claim 3 wherein: every group the subassembly of polishing all includes installation piece (16), fourth motor (17) and wheel (18) of polishing, installation piece (16) fixed connection is in the extension end of second electric putter (15), fourth motor (17) fixed connection is in an end of installation piece (16), another side that installation piece (16) was run through in the output activity of fourth motor (17) and outside extension, wheel (18) fixed connection is in the output of fourth motor (17).
5. An aircraft tire buffing apparatus according to claim 4 wherein: slide mechanism includes sliding tray (4), screw rod (5), first motor (6) and screw thread slider (7), the upper end of bottom plate (1) is seted up in sliding tray (4), screw thread slider (7) fixed connection is in the lower extreme of first motor (6), screw thread slider (7) sliding connection is in sliding tray (4), screw rod (5) rotate to be connected in the both sides inner wall of sliding tray (4), screw rod (5) and screw thread slider (7) threaded connection.
6. An aircraft tire buffing apparatus according to claim 5 wherein: one side end fixedly connected with second motor (8) of bottom plate (1), the output activity of second motor (8) runs through the one side inner wall of sliding tray (4) and is fixed with the one end of screw rod (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222592423.XU CN218696758U (en) | 2022-09-29 | 2022-09-29 | Aviation tire grinding device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222592423.XU CN218696758U (en) | 2022-09-29 | 2022-09-29 | Aviation tire grinding device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218696758U true CN218696758U (en) | 2023-03-24 |
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ID=85637054
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222592423.XU Active CN218696758U (en) | 2022-09-29 | 2022-09-29 | Aviation tire grinding device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218696758U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116952616A (en) * | 2023-06-15 | 2023-10-27 | 青岛森麒麟轮胎股份有限公司 | Tire slip rate testing machine |
| CN117207573A (en) * | 2023-08-07 | 2023-12-12 | 青岛森麒麟轮胎股份有限公司 | Aviation tire repair equipment |
-
2022
- 2022-09-29 CN CN202222592423.XU patent/CN218696758U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116952616A (en) * | 2023-06-15 | 2023-10-27 | 青岛森麒麟轮胎股份有限公司 | Tire slip rate testing machine |
| CN116952616B (en) * | 2023-06-15 | 2025-11-18 | 青岛森麒麟轮胎股份有限公司 | A tire slip ratio testing machine |
| CN117207573A (en) * | 2023-08-07 | 2023-12-12 | 青岛森麒麟轮胎股份有限公司 | Aviation tire repair equipment |
| CN117207573B (en) * | 2023-08-07 | 2026-01-06 | 青岛森麒麟轮胎股份有限公司 | An aircraft tire repair device |
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