Waste aircraft tire cutting and recycling device

Abstract

The utility model relates to the technical field of aircraft tire recycling, and discloses a waste aircraft tire cutting and recycling device which comprises a workbench, four supporting legs are fixedly arranged on the bottom face of the workbench and evenly distributed on the bottom face of the periphery of the workbench, and a clamping mechanism is fixedly arranged on the top face of the workbench. A cutting mechanism is fixedly arranged on the side face of the workbench. The clamping mechanism comprises a clamping part and a crushing part, and the bottom surface of the clamping part is fixedly connected with the top surface of the crushing part; the clamping part comprises a supporting plate, the bottom face of the supporting plate is fixedly connected with the top face of the workbench, and a motor B is fixedly arranged on the back face of the supporting plate; and the cutting mechanism comprises a cutting part and a power part. The cutting mechanism is arranged, and a hydraulic rod and a device block are arranged to work cooperatively, so that a cutting knife can be adjusted up and down, the waste aircraft tire can be rapidly cut according to actual requirements, operation is simple and rapid, and time, labor and labor are saved.

Description

Technical Field

[0001] The utility model relates to the technical field of aviation tire recycling, in particular to a waste aviation tire cutting and recycling device. Background Art

[0002] Aircraft tires, commonly known as aircraft tires, are a key component of the aircraft landing gear system. The main function of aircraft tires is to support, load and cushion the aircraft during parking, takeoff and landing. Aircraft tires are a whole made of rubber, skeleton materials and various additives cross-linked through complex chemical reactions.

[0003] A Chinese patent discloses a cutting and recycling device with the publication number CN112045896A, which includes a bottom plate with a supporting arc plate arranged in the middle of the top of the bottom plate; a rotating mechanism with a rotating mechanism arranged on one side of the top of the bottom plate; and a cutting mechanism with a cutting mechanism arranged on one end of the top of the bottom plate near the supporting arc plate, which controls the first cutting knife and the second cutting knife to cut both sides of the waste tire at the same time through the cooperation of a rack and a circular gear, thereby saving cutting time and increasing cutting efficiency.

[0004] However, there are still the following disadvantages: when the cutting and recycling device is cutting the tire, it is unable to adjust the cutting accordingly according to actual needs, and at the same time perform secondary crushing on it to make its recycling efficiency higher, so it is urgent to design a waste aviation tire cutting and recycling device. Utility Model Content

[0005] The utility model aims to provide a waste aviation tire cutting and recycling device to solve the problems raised in the above background technology.

[0006] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a waste aircraft tire cutting and recycling device comprises a workbench, the bottom surface of the workbench is fixedly provided with supporting legs, the number of the supporting legs is four and they are evenly distributed around the bottom surface of the workbench, the top surface of the workbench is fixedly provided with a clamping mechanism, and the side surface of the workbench is fixedly provided with a cutting mechanism;

[0007] The clamping mechanism comprises a clamping part and a crushing part, and the bottom surface of the clamping part and the top surface of the crushing part are fixedly connected;

[0008] The clamping part includes a support plate, the bottom surface of the support plate is fixedly connected to the top surface of the workbench, and a motor B is fixedly arranged on the back of the support plate;

[0009] The cutting mechanism comprises a cutting part and a power part, and the side surface of the power part and the side surface of the cutting part are fixedly connected;

[0010] The power unit comprises a fixing plate, the back side of the fixing plate is fixedly connected to the front side of the workbench, and a hydraulic rod is fixedly arranged on the top side of the fixing plate.

[0011] Preferably, the front side of the output rod of the motor B passes through the back side of the support plate and extends to the inside of the support plate. A bidirectional threaded rod is fixedly provided on the front side of the output rod of the motor B. The surface of the bidirectional threaded rod and the inner wall of the support plate are rotatably connected by a bearing.

[0012] Preferably, two clamping blocks are threadedly sleeved on the front and rear end surfaces of the bidirectional threaded rod respectively, and the side surfaces of the clamping blocks are frictionally and slidingly connected to the inner wall of the support plate. A motor A is fixedly installed on the front right end of the workbench, and the back end surface of the output rod of the motor A passes through the front of the workbench and extends to the inside of the workbench.

[0013] Preferably, an active rod is fixedly provided on the back end surface of the output rod of the motor A, and the surface of the active rod and the inner wall of the workbench are rotatably connected by a bearing. A driven rod is provided inside the workbench, and the surface of the driven rod and the inner wall of the workbench are rotatably connected by a bearing.

[0014] Preferably, two gears are fixedly sleeved on the back end surfaces of the active rod and the driven rod respectively, and the two gears are meshed and connected with each other. Crushing rollers are fixedly sleeved on the surfaces of the active rod and the driven rod respectively.

[0015] Preferably, a device block is fixedly provided on the top surface of the hydraulic rod output rod, a threaded rod is provided inside the device block, the surface of the threaded rod and the inner wall of the device block are rotatably connected by a bearing, a turning handle is fixedly provided on the left end surface of the threaded rod, and a connecting block is threadedly sleeved on the surface of the threaded rod.

[0016] Preferably, the side surface of the connecting block and the inner wall of the device block are frictionally and slidingly connected, the top surface of the connecting block is fixedly provided with a motor C, the bottom surface of the output rod of the motor C penetrates through the top surface of the connecting block and extends to the inside of the connecting block, a rotating rod is fixedly provided on the bottom surface of the output rod of the motor C, the surface of the rotating rod and the inner wall of the connecting block are rotatably connected by a bearing, and a cutting knife is fixedly sleeved on the surface of the rotating rod.

[0017] Compared with the prior art, the beneficial effects of the utility model are:

[0018] 1. The waste aircraft tire cutting and recycling device is provided with a cutting mechanism, and the cooperation of the hydraulic rod and the device block enables the cutting knife to be adjusted up and down, so that the waste aircraft tires can be quickly cut according to actual needs, which is simple and fast to operate, saving time, effort and labor;

[0019] 2. The waste aviation tire cutting and recycling device is provided with a motor A and an active rod to work together. Through the transmission effect of the gears, the active rod and the driven rod simultaneously drive two crushing rollers to perform secondary crushing on the cut tires, so that the cutting and crushing efficiency is higher and the subsequent recycling is convenient;

[0020] 3. The waste aircraft tire cutting and recycling device is provided with a clamping mechanism. Through the cooperation of the motor B and the bidirectional threaded rod, the two clamping blocks can move towards each other at the same time, so that when the aircraft tire is cut, it can be fixed and clamped to prevent it from falling out of position and affecting the subsequent cutting work. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Figure 1 It is a three-dimensional schematic diagram of the front structure of the utility model;

[0022] Figure 2 It is a three-dimensional cross-sectional schematic diagram of the front structure of the utility model;

[0023] Figure 3 It is a three-dimensional schematic diagram of the back structure of the utility model;

[0024] Figure 4 It is a three-dimensional cross-sectional schematic diagram of the left-side structure of the utility model;

[0025] Figure 5 For this utility model Figure 3 A three-dimensional enlarged schematic diagram of the structure of area A in the middle.

[0026] In the figure: 1. workbench; 2. supporting legs; 3. clamping mechanism; 301. motor A; 302. active rod; 303. driven rod; 304. gear; 305. crushing roller; 306. supporting plate; 307. motor B; 308. bidirectional threaded rod; 309. clamping block; 4. cutting mechanism; 401. fixed plate; 402. hydraulic rod; 403. device block; 404. turning handle; 405. threaded rod; 406. connecting block; 407. motor C; 408. rotating rod; 409. cutting knife. DETAILED DESCRIPTION

[0027] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0028] Embodiment 1

[0029] See also Figure 1-Figure 5As shown, a waste aircraft tire cutting and recycling device includes a workbench 1, the bottom surface of the workbench 1 is fixedly provided with support legs 2, the number of support legs 2 is four and evenly distributed on the bottom surface around the workbench 1, the top surface of the workbench 1 is fixedly provided with a clamping mechanism 3, and the side surface of the workbench 1 is fixedly provided with a cutting mechanism 4; the clamping mechanism 3 includes a clamping part and a crushing part, and the bottom surface of the clamping part and the top surface of the crushing part are fixedly connected; the clamping part includes a support plate 306, the support plate 306 is an L-shaped plate, the bottom surface of the support plate 306 is fixedly connected to the top surface of the workbench 1, and the back surface of the support plate 306 is fixedly provided with a motor B307; the cutting mechanism 4 includes a cutting part and a power part, and the side surface of the power part is fixedly connected to the side surface of the cutting part; the power part includes a fixed plate 401, the back surface of the fixed plate 401 is fixedly connected to the front surface of the workbench 1, and the top surface of the fixed plate 401 is fixedly provided with a hydraulic rod 402;

[0030] During operation, the hydraulic rod 402 is activated, so that the device block 403 can drive the cutting knife 409 to move up and down, thereby realizing rapid all-round cutting of the aircraft tire.

[0031] Furthermore, the front of the output rod of the motor B307 passes through the back of the support plate 306 and extends to the inside of the support plate 306. The model of the motor B307 is Y2-112M-6. A bidirectional threaded rod 308 is fixedly arranged on the front of the output rod of the motor B307. The surface of the bidirectional threaded rod 308 and the inner wall of the support plate 306 are rotatably connected by a bearing.

[0032] During operation, the motor B307 is started to rotate the bidirectional threaded rod 308 .

[0033] Furthermore, two clamping blocks 309 are respectively threadedly sleeved on the front and rear end surfaces of the bidirectional threaded rod 308, and the side surfaces of the clamping blocks 309 are frictionally and slidably connected to the inner wall of the support plate 306. A motor A301 is fixedly arranged on the front of the right end of the workbench 1, and the back end surface of the output rod of the motor A301 passes through the front of the workbench 1 and extends to the inside of the workbench 1;

[0034] During operation, the bidirectional threaded rod 308 rotates, and through the action of two reverse threads, the two clamping blocks 309 fix and clamp the front and rear ends of the aircraft tire.

[0035] Further, an active rod 302 is fixedly arranged on the back end face of the output rod of the motor A301, and the surface of the active rod 302 is rotatably connected to the inner wall of the workbench 1 by a bearing, and a driven rod 303 is arranged inside the workbench 1, and the surface of the driven rod 303 is rotatably connected to the inner wall of the workbench 1 by a bearing;

[0036] During operation, the motor A301 is started to rotate the active rod 302, and the driven rod 303 is rotated through the mutual transmission of the two gears 304.

[0037] Furthermore, two gears 304 are fixedly sleeved on the back end surfaces of the active rod 302 and the driven rod 303, respectively. The two gears 304 are meshed and connected with each other. Crushing rollers 305 are fixedly sleeved on the surfaces of the active rod 302 and the driven rod 303, respectively. There is a partial gap between the two crushing rollers 305.

[0038] During operation, the two gears 304 are mutually driven to rotate the driven rod 303, thereby driving the two crushing rollers 305 to rotate and crush.

[0039] Further, a device block 403 is fixedly provided on the top surface of the output rod of the hydraulic rod 402, a threaded rod 405 is provided inside the device block 403, the surface of the threaded rod 405 and the inner wall of the device block 403 are rotatably connected by a bearing, a turning handle 404 is fixedly provided on the left end surface of the threaded rod 405, and a connection block 406 is threadedly sleeved on the surface of the threaded rod 405;

[0040] During operation, the handle 404 is rotated to rotate the threaded rod 405, thereby driving the cutting knife 409 to move left and right.

[0041] Further, the side surface of the connecting block 406 and the inner wall of the device block 403 are frictionally and slidably connected, a motor C407 is fixedly arranged on the top surface of the connecting block 406, the bottom surface of the output rod of the motor C407 penetrates the top surface of the connecting block 406 and extends to the inside of the connecting block 406, a rotating rod 408 is fixedly arranged on the bottom surface of the output rod of the motor C407, the surface of the rotating rod 408 and the inner wall of the connecting block 406 are rotatably connected by a bearing, a cutting knife 409 is fixedly sleeved on the surface of the rotating rod 408, and a plurality of saw teeth are arranged on the surface of the cutting knife 409;

[0042] During operation, the motor C407 is started to rotate the rotating rod 408, thereby driving the cutting knife 409 to perform rotary cutting.

[0043] Working principle: When in use, first place the waste aviation tire to be recycled on the workbench 1, start the motor B307, so that the bidirectional threaded rod 308 rotates, and through the action of the two reverse threads, the two clamping blocks 309 fix the front and rear ends of the aviation tire, start the motor A301, so that the active rod 302 rotates, and through the mutual transmission of the two gears 304, the driven rod 303 rotates, thereby driving the two crushing rollers 305 to rotate and crush, start the motor C407, so that the rotating rod 408 rotates, thereby driving the cutting knife 409 to rotate and cut, turn the handle 404, so that the threaded rod 405 rotates, thereby driving the cutting knife 409 to move left and right, contact the aviation tire for cutting, start the hydraulic rod 402, so that the device block 403 can drive the cutting knife 409 to move up and down, thereby realizing rapid all-round cutting of the aviation tire.

[0044] The above description is only a preferred embodiment of the utility model and is not intended to limit the utility model. Although the utility model is described in detail with reference to the above embodiments, those skilled in the art can still modify the technical solutions recorded in the above embodiments or replace some of the technical features therein by equivalents. Any modification, equivalent replacement, similar improvement, etc. made within the theoretical and principle content of the utility model shall be included in the protection scope of the utility model.

Claims

1. A waste aircraft tire cutting and recycling device, comprising a workbench (1), characterized in that: The bottom surface of the workbench (1) is fixedly provided with supporting legs (2), the number of the supporting legs (2) is four and they are evenly distributed around the bottom surface of the workbench (1), the top surface of the workbench (1) is fixedly provided with a clamping mechanism (3), and the side surface of the workbench (1) is fixedly provided with a cutting mechanism (4); The clamping mechanism (3) comprises a clamping part and a crushing part, wherein the bottom surface of the clamping part and the top surface of the crushing part are fixedly connected; The clamping portion comprises a support plate (306), the bottom surface of the support plate (306) is fixedly connected to the top surface of the workbench (1), and a motor B (307) is fixedly arranged on the back surface of the support plate (306); The cutting mechanism (4) comprises a cutting part and a power part, and the side surface of the power part and the side surface of the cutting part are fixedly connected; The power unit comprises a fixing plate (401), the back surface of the fixing plate (401) is fixedly connected to the front surface of the workbench (1), and a hydraulic rod (402) is fixedly arranged on the top surface of the fixing plate (401).

2. The waste aircraft tire cutting and recycling device according to claim 1 is characterized in that: The front side of the output rod of the motor B (307) passes through the back side of the support plate (306) and extends into the interior of the support plate (306). A bidirectional threaded rod (308) is fixedly arranged on the front side of the output rod of the motor B (307). The surface of the bidirectional threaded rod (308) and the inner wall of the support plate (306) are rotatably connected by a bearing.

3. The waste aircraft tire cutting and recycling device according to claim 2 is characterized in that: Two clamping blocks (309) are respectively threadedly sleeved on the front and rear end surfaces of the bidirectional threaded rod (308), and the side surfaces of the clamping blocks (309) are frictionally and slidably connected to the inner wall of the support plate (306). A motor A (301) is fixedly arranged on the front right end of the workbench (1), and the back end surface of the output rod of the motor A (301) passes through the front of the workbench (1) and extends to the inside of the workbench (1).

4. The waste aircraft tire cutting and recycling device according to claim 3 is characterized in that: An active rod (302) is fixedly arranged on the back end surface of the output rod of the motor A (301), and the surface of the active rod (302) is rotatably connected to the inner wall of the workbench (1) by a bearing. A driven rod (303) is arranged inside the workbench (1), and the surface of the driven rod (303) is rotatably connected to the inner wall of the workbench (1) by a bearing.

5. The waste aircraft tire cutting and recycling device according to claim 4 is characterized in that: Two gears (304) are fixedly sleeved on the back end surfaces of the active rod (302) and the driven rod (303), respectively. The two gears (304) are meshed and connected with each other. A crushing roller (305) is fixedly sleeved on the surface of the active rod (302) and the driven rod (303).

6. The waste aircraft tire cutting and recycling device according to claim 1 is characterized by: A device block (403) is fixedly arranged on the top surface of the output rod of the hydraulic rod (402), a threaded rod (405) is arranged inside the device block (403), the surface of the threaded rod (405) and the inner wall of the device block (403) are rotatably connected by a bearing, a turning handle (404) is fixedly arranged on the left end surface of the threaded rod (405), and a connection block (406) is threadedly sleeved on the surface of the threaded rod (405).

7. The waste aircraft tire cutting and recycling device according to claim 6 is characterized by: The side surface of the connecting block (406) and the inner wall of the device block (403) are frictionally and slidably connected, a motor C (407) is fixedly arranged on the top surface of the connecting block (406), the bottom surface of the output rod of the motor C (407) penetrates the top surface of the connecting block (406) and extends to the inside of the connecting block (406), a rotating rod (408) is fixedly arranged on the bottom surface of the output rod of the motor C (407), the surface of the rotating rod (408) and the inner wall of the connecting block (406) are rotatably connected by a bearing, and a cutting knife (409) is fixedly sleeved on the surface of the rotating rod (408).

Images