CN218629017U - Aviation tire test auxiliary device - Google Patents
Aviation tire test auxiliary device Download PDFInfo
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- CN218629017U CN218629017U CN202222561587.6U CN202222561587U CN218629017U CN 218629017 U CN218629017 U CN 218629017U CN 202222561587 U CN202222561587 U CN 202222561587U CN 218629017 U CN218629017 U CN 218629017U
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- rack
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- fixedly connected
- workstation
- aircraft tire
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Abstract
The utility model provides an aircraft tire tests auxiliary device, belong to tire processing technology field, this aircraft tire tests auxiliary device includes the workstation, two first spouts, the upper end of workstation is all seted up to two first spouts, the second spout, the upper end of workstation is seted up to the second spout, the gear, gear revolve connects in the second spout, the fixed plate, fixed plate fixed connection is in the lower extreme of workstation, two centre gripping swash plates draw close each other and just can be in the laminating of aircraft tire circumference surface, at this moment alright play the effect of supplementary firm aircraft tire, improve the high efficiency of tire test compressive capacity, after aircraft tire is consolidated, press the tire through the dedicated press of tire, so that detect the tire and receiving the impact in-process, whether there is the condition that the crack appears, accessible centre gripping swash plate rectifies the tire, alright help the tire when the extrusion is crooked, the difficult condition that takes place the off tracking, and the work efficiency is improved.
Description
Technical Field
The utility model belongs to the technical field of tire processing, concretely relates to aircraft tire tests auxiliary device.
Background
A tire is a ground-rolling circular ring-shaped elastic rubber article mounted on various vehicles or machines. Generally mounted on a metal rim, and is capable of supporting a vehicle body, buffering external impact, achieving contact with a road surface and ensuring the driving performance of a vehicle. Tires are often used under complex and severe conditions, which are subjected to various deformations, loads, forces and high and low temperature effects during running, and therefore must have high load-bearing, traction and cushioning properties. At the same time, high abrasion resistance and flexibility resistance, and low rolling resistance and heat build-up are also required.
The authorization publication number "CN212871744U" describes "an auxiliary device for testing the wear resistance of a tire, which increases the convenience of the wear resistance test of the tire, reduces manual use, and improves the practicability; including the chassis, first motor, the slide, the riser, the second motor, the tire mounting bracket, the mounting bracket, first wearing and tearing are changeed the roller, second wearing and tearing are changeed roller and truckle, first motor is installed on the chassis, the inside cavity that is provided with of chassis, the output of first motor is provided with the lead screw, the lead screw rotates with the chassis and is connected and be located the chassis cavity, the bottom and the lead screw of slide rotate to be connected, the bottom and the top of slide of riser are connected, the bottom and the top of slide of second motor are connected, the output of second motor is provided with the pivot, the pivot rotates with the riser to be connected, the output in the pivot is installed to the tire mounting bracket, the bottom of mounting bracket is connected with the top of chassis, the mounting bracket is located the right side of tire mounting bracket, the inside cavity that is provided with of mounting bracket ".
Can increase the convenience of tire wearability test in the above-mentioned patent, reduce artifical the use, but supplementary testing arrangement is not stable enough in the above-mentioned patent, can cause the tire to rock, and on the tire production line, the staff often needs the compressive capacity of test tire, prevent that the tire from receiving the condition of impact in-process and the fracture appears, but the device of general fixed tire is all comparatively simple, it is not stable enough, when the dedicated press of tire pressed the tire, the condition of off tracking can take place because of the shape of tire, if the tire is placed not in place, the condition of extrusion deformation can appear in addition, the quality and the work efficiency that influence the tire reduce.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aircraft tire test auxiliary device, it is not stable enough to aim at solving the auxiliary test device among the prior art, can cause the tire to rock, and on the tire production line, the staff often needs the compressive capacity of test tire, prevent that the tire from receiving the condition of impact in-process and the fracture appears, but the device of general fixed tire is all comparatively simple, it is not stable enough, when the tire is pressed to the dedicated press of tire, the condition of off tracking can take place because of the shape of tire, if the tire is placed not in place, extrusion deformation's the condition can appear in addition, influence the quality of tire and the problem that work efficiency reduces.
In order to achieve the above purpose, the utility model provides a following technical scheme:
an aircraft tire testing assistance device comprising:
a work table;
the two first sliding grooves are formed in the upper end of the workbench;
the second sliding chute is arranged at the upper end of the workbench;
the gear is rotationally connected in the second sliding groove;
the fixed plate is fixedly connected to the lower end of the workbench;
the motor is fixedly connected to one side end of the fixing plate;
the rotating rod is rotatably connected in the workbench, fixedly connected to the lower end of the gear and fixedly connected to an output shaft of the motor;
the two tire placing grooves are formed in the upper end of the workbench;
the first rack and the second rack are both connected in the second sliding chute in a sliding manner and are mutually meshed through gears;
the two sliding blocks are respectively and fixedly connected to one side ends of the first rack and the second rack;
the two hollow grooves are respectively formed in one side end of each of the two sliding blocks, and the first rack and the second rack are respectively connected into the two hollow grooves in a sliding manner;
and the clamping inclined plates are fixedly connected to the upper ends of the two sliding blocks respectively.
As a preferred scheme, the both sides inner wall fixedly connected with limiting plate of second spout, the limiting plate is located the upper end of first rack and second rack.
As a preferred scheme of the utility model, two transparent baffles of the upper end fixedly connected with of workstation, two transparent baffle is located being close to the end department mutually of a plurality of centre gripping swash plates respectively.
As a preferred scheme, a side end difference fixedly connected with stopper, two of first rack and second rack stopper difference sliding connection is in two hollow inslots.
As an optimized scheme, the equal fixedly connected with universal wheel of four sets of landing leg lower extreme of workstation, be equipped with brake subassembly in the universal wheel.
As an optimal scheme of the utility model, the four corners department of workstation adopts the fillet design.
Compared with the prior art, the beneficial effects of the utility model are that:
1. in this scheme, at first place the aircraft tire in the tire standing groove, then starter motor drives the bull stick and rotates and take the gear to rotate, through first rack in second rack and gear engagement relation, first rack and second rack just can take the slider to move to being close to the end mutually, when the centre gripping swash plate in the circumference surface contact of tire, alright lean on the aircraft tire and live, alright in order to assist the tire to carry out compressive capacity test operation like this, improve the high efficiency of tire test compressive capacity, alright help the tire when extrusion bending, the difficult condition that takes place the off tracking, and the work efficiency is improved.
2. In this scheme, when the position of workstation is removed to needs, the universal wheel that the accessible set up helps the workstation to remove, removes and accomplishes the back, and the inside brake assembly that sets up of personnel's accessible universal wheel stops the universal wheel, prevents that the universal wheel from continuing to take place the rolling condition forward when stopping, the safety and stability of protection workstation.
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 first perspective view of the present invention;
fig. 2 is a perspective view of a second viewing angle of the present invention;
fig. 3 is a first top perspective view of the present invention;
fig. 4 is a second top perspective view of the present invention.
In the figure: 1. a work table; 2. a universal wheel; 3. clamping the inclined plate; 4. a slider; 5. a tire placing groove; 6. a transparent baffle; 7. a fixing plate; 8. a rotating rod; 9. a motor; 10. a first chute; 11. a second chute; 12. a first rack; 13. a second rack; 14. a limiting block; 15. a gear; 16. a hollow groove; 17. and a limiting plate.
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. 1-4, the present invention provides the following technical solutions:
an aircraft tire testing aid comprising:
a work table 1;
the two first sliding chutes 10 are arranged at the upper end of the workbench 1;
the second sliding chute 11 is formed in the upper end of the workbench 1;
the gear 15 is rotationally connected in the second sliding chute 11;
the fixed plate 7, the fixed plate 7 is fixedly connected to the bottom end of the work bench 1;
the motor 9, the motor 9 is fixedly connected to one side end of the fixed plate 7;
the rotating rod 8 is rotatably connected into the workbench 1, the rotating rod 8 is fixedly connected to the lower end of the gear 15, and the rotating rod 8 is fixedly connected to an output shaft of the motor 9;
two tire placing grooves 5, wherein the two tire placing grooves 5 are both arranged at the upper end of the workbench 1;
the first rack 12 and the second rack 13, the first rack 12 and the second rack 13 are both connected in the second chute 11 in a sliding manner, and the first rack 12 and the second rack 13 are both meshed with each other through a gear 15;
the two sliding blocks 4 are respectively and fixedly connected to one side ends of the first rack 12 and the second rack 13;
the two hollow grooves 16 are respectively arranged at one side end of the two sliding blocks 4, and the first rack 12 and the second rack 13 are respectively connected in the two hollow grooves 16 in a sliding manner;
a plurality of centre gripping swash plate 3, a plurality of centre gripping swash plate 3 are fixed connection respectively in the upper end of two sliders 4.
In the embodiment of the present invention, when the aircraft tire is transported to the upper end of the workbench 1 by the aircraft tire production line, firstly, a person can roll the aircraft tire longitudinally into the tire placing groove 5, if the aircraft tire has the pressure resistance, the motor 9 can be started, the output shaft of the motor 9 drives the rotating rod 8 to rotate in the workbench 1, the motor 9 can be fixed by the fixing plate 7, so that the motor 9 does not rotate, the safe operation of the motor 9 is protected, meanwhile, the rotating rod 8 drives the gear 15 to rotate, at this time, the second rack 13 and the first rack 12 are meshed with the gear 15, and the two sliders 4 are driven to move towards the adjacent end in the first sliding groove 10, and the hollow groove 16 is opened to provide a moving track for the first rack 12 and the second rack 13, prevent first rack 12 or second rack 13 from bumping with slider 4 when removing, cause the condition of equipment damage, at this moment slider 4 just can stop moving when removing the one side inner wall summit of first spout 10, draw close each other through two centre gripping swash plates 3 that set up and just can be in the laminating of aircraft tire circumference surface, at this moment alright play supplementary firm aircraft tire's effect, improve tire test compressive capacity's high efficiency, after aircraft tire is consolidated, alright press the tire through the dedicated press of tire, so that detect tire is receiving the impact in-process, whether the condition of crack appears, and still can rectify the tire through centre gripping swash plate 3, alright help tire is when the extrusion bending, the difficult condition that takes place the off tracking, and the work efficiency is improved, what need explain: the specific types of the motor 9, the universal wheel 2, the gear 15, the first rack 12 and the second rack 13 are selected by a person skilled in the art, and the motor 9, the universal wheel 2, the gear 15, the first rack 12 and the second rack 13 belong to the prior art.
Specifically, referring to fig. 1, the inner walls of the two sides of the second chute 11 are fixedly connected with a limiting plate 17, and the limiting plate 17 is located at the upper ends of the first rack 12 and the second rack 13.
In this embodiment: the limiting plate 17 can cover the first rack 12 and the second rack 13, so that the first rack 12 and the second rack 13 can be prevented from rotating upwards, the safety of the second rack 13 and the first rack 12 is protected, and parts can be placed at the upper end of the limiting plate 17 to facilitate storage.
Specifically, referring to fig. 1, the upper end of the worktable 1 is fixedly connected with two transparent baffles 6, and the two transparent baffles 6 are respectively located at the positions close to the plurality of inclined clamping plates 3.
In this embodiment: one side of the aircraft tire is protected by the transparent baffle 6, when a person places the tire in the tire placing groove 5, the transparent baffle 6 can reinforce the tire by reinforcing the clamping inclined plate 3, and the transparent baffle 6 is transparent, so that the person is not hindered from observing the surface condition of the tire.
Referring to fig. 3-4, the first rack 12 and the second rack 13 are fixedly connected with a limiting block 14 at one side end thereof, and the two limiting blocks 14 are slidably connected to the two hollow grooves 16 respectively.
In this embodiment: the first rack 12 and the second rack 13 can be limited by the aid of the limiting blocks 14, the situation that the first rack 12 and the second rack 13 are not prone to displacement and dislocation due to overlong moving distance is avoided, when the limiting blocks 14 are in contact with the gears 15, the first rack 12 and the second rack 13 can stop, safe operation of the first rack 12 and the second rack 13 is protected, and the limiting blocks 14 can enter the hollow grooves 16 along with the first rack 12 and the second rack 13 to improve overall flowability.
Specifically, referring to fig. 1-2, the lower ends of four sets of legs of the workbench 1 are fixedly connected with universal wheels 2, and brake assemblies are arranged in the universal wheels 2.
In this embodiment: when needs move workstation 1's position, workstation 1 is helped to the universal wheel 2 that the accessible set up removes, removes and accomplishes the back, and the inside brake assembly that sets up of personnel's accessible universal wheel 2 comes to stop universal wheel 2, prevents that universal wheel 2 from continuing the condition emergence of rolling forward when stopping, the safety and stability of protection workstation 1.
Specifically, referring to fig. 1, the four corners of the worktable 1 are designed to be rounded.
In this embodiment: four angles of workstation 1 all adopt the design of fillet, alright prevent like this that personnel are placing or when carrying the tire, the condition that the difficult emergence of colliding with workstation 1 contacts, protection personnel's safety.
The utility model discloses a theory of operation and use flow: firstly place the aircraft tire in tire standing groove 5, then starting motor 9 drives bull stick 8 at the internal rotation of workstation 1, bull stick 8 drives gear 15 and rotates simultaneously, because second rack 13 and first rack 12 and the meshing relation of gear 15, just can drive two sliders 4 and move to being close to the end mutually in first spout 10, at this moment when slider 4 moves one side inner wall summit of first spout 10, two centre gripping swash plates 3 draw close to each other just can be in the laminating of aircraft tire circumference surface, at this moment alright play the effect of supplementary firm aircraft tire, improve the high efficiency of tire test compressive capacity, after the aircraft tire is consolidated, press the tire through the dedicated press of tire, so that detect the tire and be receiving the impact in-process, whether the condition that the crack appears, accessible centre gripping swash plate 3 rectifies the tire, alright help the tire when extrusion bending, the condition of off tracking is difficult for taking place, improve work efficiency.
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 testing aid, comprising:
a work table (1);
the two first sliding chutes (10) are arranged at the upper end of the workbench (1);
the second sliding chute (11) is formed in the upper end of the workbench (1);
the gear (15), the said gear (15) is connected to the second concrete chute (11) rotatably;
the fixing plate (7), the said fixing plate (7) is fixedly connected to the underpart of the work level (1);
the motor (9), the said motor (9) is fixedly connected to one side end of the fixed plate (7);
the rotating rod (8) is rotatably connected into the workbench (1), the rotating rod (8) is fixedly connected to the lower end of the gear (15), and the rotating rod (8) is fixedly connected to an output shaft of the motor (9);
the two tire placing grooves (5) are formed in the upper end of the workbench (1);
the first rack (12) and the second rack (13), the first rack (12) and the second rack (13) are both connected in the second sliding groove (11) in a sliding manner, and the first rack (12) and the second rack (13) are both meshed with each other through a gear (15);
the two sliding blocks (4) are respectively and fixedly connected to one side ends of the first rack (12) and the second rack (13);
the two hollow grooves (16) are respectively formed in one side end of each of the two sliding blocks (4), and the first rack (12) and the second rack (13) are respectively connected into the two hollow grooves (16) in a sliding manner;
a plurality of centre gripping swash plate (3), it is a plurality of centre gripping swash plate (3) are fixed connection respectively in the upper end of two slider (4).
2. An aircraft tire testing assisting device according to claim 1, wherein: and limiting plates (17) are fixedly connected to the inner walls of the two sides of the second sliding groove (11), and the limiting plates (17) are located at the upper ends of the first rack (12) and the second rack (13).
3. An aircraft tire testing aid according to claim 2, wherein: the upper end fixedly connected with two transparent baffles (6) of workstation (1), two transparent baffles (6) are located the department that is close to mutually of a plurality of centre gripping swash plates (3) respectively.
4. An aircraft tire testing aid according to claim 3, wherein: one side ends of the first rack (12) and the second rack (13) are fixedly connected with limit blocks (14) respectively, and the two limit blocks (14) are connected in the two hollow grooves (16) in a sliding mode respectively.
5. An aircraft tire testing assisting device according to claim 4, wherein: the four sets of landing legs lower extreme of workstation (1) all fixedly connected with universal wheel (2), be equipped with brake subassembly in universal wheel (2).
6. An aircraft tire testing aid according to claim 5, wherein: the four corners of the workbench (1) adopt a fillet design.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222561587.6U CN218629017U (en) | 2022-09-27 | 2022-09-27 | Aviation tire test auxiliary device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222561587.6U CN218629017U (en) | 2022-09-27 | 2022-09-27 | Aviation tire test auxiliary device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218629017U true CN218629017U (en) | 2023-03-14 |
Family
ID=85469073
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222561587.6U Active CN218629017U (en) | 2022-09-27 | 2022-09-27 | Aviation tire test auxiliary device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218629017U (en) |
-
2022
- 2022-09-27 CN CN202222561587.6U patent/CN218629017U/en active Active
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