Aviation tire body stacking and aligning device

Abstract

The utility model relates to the technical field of tire manufacturing, in particular to an aircraft tire body stacking and aligning device, which is provided with a positioning device and a cutting device, automatically positions the stacking position of raw materials during stacking, automatically cuts the raw materials and reduces the labor intensity of workers. Comprising a body; the positioning device and the cutting device are both mounted on the machine body; the machine body carries out stacking machining forming on tires, the positioning device positions the raw material cutting-off position, and the cutting-off device cuts off raw materials to carry out stacking alignment.

Description

TECHNICAL FIELD

[0001] The utility model relates to the technical field of tire manufacturing, in particular to an aviation tire body layering alignment device. BACKGROUND

[0002] A tire is a round annular elastic rubber product for rolling on the ground, which includes a tire body and a plurality of components including a belt layer.

[0003] For example, the Chinese invention patent with the publication number CN1871118A, which is an assembly for manufacturing non-vulcanized radial tires and a method for manufacturing such tires, mainly includes a tire body forming drum, a belt layer forming drum and a finishing drum. The tire body forming drum is used to form and manufacture a tire body, the belt layer forming drum is used to form and manufacture a belt layer, and the finishing drum is used to combine the tire body and the belt layer together.

[0004] However, the existing technical equipment still has the following problems when in use: the existing tire body forming drum needs to be manually controlled by workers to stack the position of the tire body raw material when the tire body is formed and processed, and the labor intensity of the workers is high. UTILITY MODEL CONTENTS

[0005] To solve the above technical problems, the utility model provides an aviation tire body layering alignment device by setting a positioning device and a cutting device, which automatically positions the raw material layering position during layering and automatically cuts the raw material, thereby reducing the labor intensity of workers.

[0006] The aviation tire body layering alignment device of the utility model, comprising a fuselage, further comprising a positioning device and a cutting device, the positioning device and the cutting device are both installed on the fuselage, the fuselage is used for layering processing and forming a tire, the positioning device is used for positioning the cutting position of raw material, and the cutting device is used for cutting raw material for layering alignment.

[0007] Preferably, the fuselage comprises a linear drive device, a support one, a main machine box, a forming drum and a plurality of feeding belts, the support one is slidingly installed at the top end of the linear drive device, the main machine box is fixedly installed at the top end of the support one, the forming drum is rotationally installed at the front end of the main machine box, and the plurality of feeding belts are all located above the forming drum; the linear drive device and the support one are used for cooperatively driving the forming drum to move forward and backward, the main machine box is used for driving the forming drum to rotate, and the feeding belts are used for feeding the forming drum.

[0008] Preferably, the positioning device comprises a positioning ring, a bracket two, a laser transmitter and a laser receiver, the positioning ring is installed at the front end of the forming drum, the positioning ring is provided with a notch, the bracket two is installed at the front end of the bracket one, the laser transmitter is installed at the middle part of the bracket two, the laser receiver is installed at the top of the bracket two, and the laser transmitter and the laser receiver are concentric; the laser transmitter emits laser, the laser receiver receives laser, the positioning ring rotates to shield the laser, when rotating to the notch position, the laser receiver receives the laser emitted by the laser transmitter, thereby positioning the cutting position of the raw material.

[0009] Preferably, the positioning device comprises a bracket three fixedly installed at the top end of the bracket one, a bracket four slidingly installed on the bracket three, and a roller rotatably installed on the bracket four; the roller reduces the friction when contacting the forming drum, and the upper layer of the raw material on the forming drum pushes the bracket four to slide, and the length of the raw material required is calculated by the sliding length of the bracket four, thereby positioning the cutting position of the raw material when next layering.

[0010] Preferably, the cutting device comprises a bracket five, a bracket six, a linear motor one, a light lever one, a sliding block one, a connecting block and a cutter one, the bracket five is installed at the front end of the bracket one, the bracket six is installed at the top end of the main machine box, the linear motor one is installed on the bracket five and the bracket six, the light lever one is installed on the bracket five and the main machine box, the sliding block one is slidingly installed on the light lever one, the connecting block is installed on the linear motor one and the sliding block one, and the cutter one is installed at the right end of the sliding block one; the linear motor one provides power to drive the cutter one to move forward and backward, and the cutter one moves forward and backward to cut the raw material.

[0011] Preferably, the cutting device comprises a plurality of bracket sevens, a plurality of bracket eights, a plurality of bracket nines, a plurality of bracket tens, a plurality of bracket elevenths, a plurality of bracket twelves, a plurality of linear motor twos, a plurality of bracket thirteens, a plurality of light lever twos, a plurality of sliding block twos, a plurality of bracket fourteens and a plurality of cutter twos, the plurality of bracket sevens and the plurality of bracket eights are respectively installed at the front and rear ends of the plurality of feeding belts, the plurality of bracket nines are respectively installed at the top ends of the plurality of bracket sevens, the plurality of bracket tens are respectively installed at the top ends of the plurality of bracket eights, the plurality of bracket elevenths and the plurality of bracket twelves are respectively installed at the top ends of the plurality of bracket nines and the plurality of bracket tens, the plurality of linear motor twos are respectively installed on the plurality of bracket elevenths, the plurality of bracket thirteens are respectively installed on the plurality of bracket twelves, the plurality of light lever twos are respectively installed on the plurality of bracket thirteens, the plurality of sliding block twos are slidingly installed on the plurality of light lever twos, the plurality of bracket fourteens are respectively installed at the bottom ends of the plurality of linear motor twos and the plurality of sliding block twos, and the plurality of cutter twos are respectively installed at the bottom ends of the plurality of bracket fourteens; the linear motor two provides power to drive the cutter two to move along the linear motor two, and the cutter two moves to cut the raw material.

[0012] Compared with the prior art, the raw material can be automatically positioned and cut, and the labor intensity of workers is low. BRIEF DESCRIPTION OF DRAWINGS

[0013] Figure 1 Fig. 1 is a schematic diagram of an axial structure of a body, a positioning ring and a bracket two;

[0014] Figure 2 Fig. 2 is a schematic diagram of an axial structure of a body, a bracket three and a bracket four;

[0015] Figure 3 Fig. 3 is a schematic diagram of an axial structure of a body;

[0016] Figure 4 Fig. 4 is a schematic diagram of an axial structure of a positioning ring, a bracket two, a laser emitter and a laser receiver;

[0017] Figure 5 Fig. 5 is a schematic diagram of an axial structure of a bracket three, a bracket four and a roller;

[0018] Figure 6 Fig. 6 is a schematic diagram of an axial structure of a bracket five, a bracket six and a linear motor one;

[0019] Figure 7 Fig. 7 is a schematic diagram of an axial structure of a bracket seven, a bracket eight and a bracket nine;

[0020] Figure 8 Fig. 8 is a schematic diagram of an axial structure of a bracket seven, a bracket eight and a bracket nine.

[0021] In the drawings, 01 is a body; 11 is a linear driving device; 12 is a bracket one; 13 is a main box; 14 is a forming drum; 15 is a feeding belt; 02 is a positioning device; 21 is a positioning ring; 22 is a bracket two; 23 is a laser emitter; 24 is a laser receiver; 25 is a bracket three; 26 is a bracket four; 27 is a roller; 03 is a cutting device; 31 is a bracket five; 32 is a bracket six; 33 is a linear motor one; 34 is a light lever one; 35 is a sliding block one; 36 is a connecting block; 37 is a cutter one; 41 is a bracket seven; 42 is a bracket eight; 43 is a bracket nine; 44 is a bracket ten; 45 is a bracket eleven; 46 is a bracket twelve; 47 is a linear motor two; 48 is a bracket thirteen; 49 is a light lever two; 50 is a sliding block two; 51 is a bracket fourteen; 52 is a cutter two. DETAILED DESCRIPTION

[0022] In order to facilitate the understanding of the present application, the present application will be described more fully below with reference to the accompanying drawings. The present application can be implemented in many different forms and is not limited to the embodiments described herein. On the contrary, the purpose of providing these embodiments is to make the disclosure of the present application more thorough and comprehensive. Embodiment 1

[0023] As Figure 1 , Figure 3 , Figure 4 and Figure 6As shown, it includes a machine body 01; it also includes a positioning device 02 and a cutting device 03, both of which are mounted on the machine body 01; the machine body 01 performs a layering process to form the tire, the positioning device 02 positions the raw material cutting position, and the cutting device 03 cuts the raw material to perform layering and alignment.

[0024] like Figure 3 As shown, the machine body 01 includes a linear drive device 11, a bracket 12, a main unit box 13, a forming drum 14 and multiple feeding belts 15. The bracket 12 is slidably mounted on the top of the linear drive device 11, the main unit box 13 is fixedly mounted on the top of the bracket 12, the forming drum 14 is rotatably mounted on the front end of the main unit box 13, and the multiple feeding belts 15 are all located above the forming drum 14.

[0025] like Figure 4 As shown, the positioning device 02 includes a positioning ring 21, a second bracket 22, a laser emitter 23, and a laser receiver 24. The positioning ring 21 is installed at the front end of the forming drum 14 and has a notch. The second bracket 22 is installed at the front end of the first bracket 12. The laser emitter 23 is installed in the middle of the second bracket 22 and the laser receiver 24 is installed at the top of the second bracket 22. The laser emitter 23 and the laser receiver 24 are concentric.

[0026] like Figure 6 As shown, the cutting device 03 includes a bracket 5 31, a bracket 6 32, a linear motor 1 33, a light bar 1 34, a slider 1 35, a connecting block 36, and a cutter 1 37. The bracket 5 31 is installed at the front end of the bracket 1 12, the bracket 6 32 is installed at the top of the main unit box 13, the linear motor 1 33 is installed on the bracket 5 31 and the bracket 6 32, the light bar 1 34 is installed on the bracket 5 31 and the main unit box 13, the slider 1 35 is slidably installed on the light bar 1 34, the connecting block 36 is installed on the linear motor 1 33 and the slider 1 35, and the cutter 1 37 is installed at the right end of the slider 1 35.

[0027] First, turn on the linear drive device 11 and the bracket 12. The linear drive device 11 and the bracket 12 work together to drive the forming drum 14 to move back and forth, so that the forming drum 14 moves to below a feeding belt 15. The feeding belt 15 feeds the forming drum 14. Then, turn on the main unit 13. The main unit 13 drives the forming drum 14 to rotate, so that the raw material is stacked on the surface of the forming drum 14. When stacking, the laser emitter 23 emits laser, and the laser receiver 24 receives the laser. The positioning ring 21 rotates to block the laser. When it rotates to the notch position, the laser receiver 24 receives the laser emitted by the laser emitter 23, thereby locating the raw material cutting position. When cutting is required, turn on the linear motor 33. The linear motor 33 provides power to drive the cutter 37 to move back and forth. The cutter 37 moves back and forth to cut the raw material. Example 2

[0028] likeFigure 2 , Figure 3 , Figure 5 , Figure 7 and Figure 8 As shown, it includes a machine body 01; it also includes a positioning device 02 and a cutting device 03, both of which are mounted on the machine body 01; the machine body 01 performs a layering process to form the tire, the positioning device 02 positions the raw material cutting position, and the cutting device 03 cuts the raw material to perform layering and alignment.

[0029] like Figure 3 As shown, the machine body 01 includes a linear drive device 11, a bracket 12, a main unit box 13, a forming drum 14 and multiple feeding belts 15. The bracket 12 is slidably mounted on the top of the linear drive device 11, the main unit box 13 is fixedly mounted on the top of the bracket 12, the forming drum 14 is rotatably mounted on the front end of the main unit box 13, and the multiple feeding belts 15 are all located above the forming drum 14.

[0030] like Figure 5 As shown, the positioning device 02 includes a bracket 3 25 fixedly installed on the top of the bracket 1 12, a bracket 4 26 slidably installed on the bracket 3 25, and a roller 27 rotatably installed on the bracket 4 26.

[0031] like Figure 7 and Figure 8 As shown, the cutting device 03 includes multiple supports 41, 42, 43, 44, 45, 46, 47, 48, 49, 50, 51, and 52, a plurality of linear motors 47, a plurality of supports 48, a plurality of light bars 49, a plurality of sliders 50, a plurality of supports 51, and a plurality of cutters 52. Supports 41 and 42 are respectively installed at the front and rear ends of multiple feeding belts 15. Supports 9 and 43 are respectively installed at the top of supports 41, and supports 10 and 44 are respectively installed at the top of supports 42. At the end, multiple brackets 11 45 and multiple brackets 12 46 are respectively installed on the top of multiple brackets 9 43 and multiple brackets 10 44, multiple linear motors 2 47 are respectively installed on multiple brackets 11 45, multiple sets of brackets 13 48 are respectively installed on multiple brackets 12 46, multiple light bars 2 49 are respectively installed on multiple sets of brackets 13 48, multiple sliders 2 50 are respectively slidably installed on multiple light bars 2 49, multiple brackets 14 51 are respectively installed on the bottom of multiple linear motors 2 47 and multiple sliders 2 50, and multiple cutters 2 52 are respectively installed on the bottom of multiple brackets 14 51;

[0032] First open linear drive device 11 and support one 12, linear drive device 11 and support one 12 cooperate and drive forming drum 14 to move back and forth, make forming drum 14 move to one under the material belt 15, material belt 15 is loaded to forming drum 14, then open main machine box 13, main machine box 13 drives forming drum 14 to rotate, make raw material layering on the surface of forming drum 14, the friction of roller 27 reduces when contacting forming drum 14 during layering, when raw material is layered on forming drum 14, it will push support four 26 to slide, calculate the length of raw material required by the sliding length of support four 26, thereby positioning the cutting position of raw material when next layering, when cutting is required, open linear motor two 47 on the same material belt 15, linear motor two 47 provides power, drives cutter two 52 to move along linear motor two 47, cutter two 52 movement cuts raw material.

[0033] As Figures 1 to 8 shown, the utility model discloses a kind of aviation tyre carcass layering alignment devices, when working, first open linear drive device 11 and support one 12, linear drive device 11 and support one 12 cooperate and drive forming drum 14 to move back and forth, make forming drum 14 move to one under the material belt 15, material belt 15 is loaded to forming drum 14, then open main machine box 13, main machine box 13 drives forming drum 14 to rotate, make raw material layering on the surface of forming drum 14, the friction of roller 27 reduces when contacting forming drum 14 during layering, when raw material is layered on forming drum 14, it will push support four 26 to slide, calculate the length of raw material required by the sliding length of support four 26, thereby positioning the cutting position of raw material when next layering, when cutting is required, open linear motor two 47 on the same material belt 15, linear motor two 47 provides power, drives cutter two 52 to move along linear motor two 47, cutter two 52 movement cuts raw material.

[0034] Linear drive device 11 can be ball screw pair, gear rack pair or linear motor with position control ability.

[0035] Linear drive device 11, main machine box 13, forming drum 14, material belt 15, laser transmitter 23, laser receiver 24, linear motor one 33 and multiple linear motor two 47 of the utility model are purchased on the market, and technical personnel in this industry only need to install and operate according to the attached instruction manual, without the creative labor of technical personnel in the field.

[0036] The utility model realizes the main function is: through setting positioning device 02 and cutting device 03, automatically position raw material layering position when layering, and automatically cut raw material, reduce the labor intensity of worker, solve the existing carcass forming drum when forming processing to carcass, need worker to control the layering position of carcass raw material, and the labor intensity of worker is higher existing technical problem.

[0037] The above merely describes preferred embodiments of the present application, and it should be noted that, for those skilled in the art, without departing from the technical principles of the present application, a number of improvements and modifications can be made, and these improvements and modifications should also be considered as the protection scope of the present application.

Claims

1. An aircraft tire carcass layer lamination alignment device, comprising a fuselage (01); characterized in that, Also include positioning device (02) and cutting device (03), positioning device (02) and cutting device (03) are installed on the fuselage (01); The fuselage (01) is stacked and processed to form a tire, the positioning device (02) positions the cutting position of the raw material, and the cutting device (03) cuts the raw material for stacking alignment.

2. An aircraft tire carcass lay-up alignment device as in claim 1 wherein, The fuselage (01) includes a linear drive device (11), a support one (12), a main machine box (13), a forming drum (14) and a plurality of feeding belts (15), the support one (12) is slidingly installed at the top end of the linear drive device (11), the main machine box (13) is fixedly installed at the top end of the support one (12), the forming drum (14) is rotatably installed at the front end of the main machine box (13), and the plurality of feeding belts (15) are located above the forming drum (14).

3. An aircraft tire carcass lay-up alignment device as in claim 2 wherein, The positioning device (02) includes a positioning ring (21), a support two (22), a laser emitter (23) and a laser receiver (24), the positioning ring (21) is installed at the front end of the forming drum (14), the positioning ring (21) is provided with a notch, the support two (22) is installed at the front end of the support one (12), the laser emitter (23) is installed at the middle of the support two (22), the laser receiver (24) is installed at the top of the support two (22), and the laser emitter (23) and the laser receiver (24) are concentric.

4. An aircraft tire carcass lay-up alignment device as claimed in claim 2 wherein, The positioning device (02) includes a support three (25) fixedly installed at the top end of the support one (12), a support four (26) slidingly installed on the support three (25), and a roller (27) rotatably installed on the support four (26).

5. An aircraft tire carcass lay-up alignment device as claimed in claim 2 wherein, The cutting device (03) includes a support five (31), a support six (32), a linear motor one (33), a light lever one (34), a sliding block one (35), a connecting block (36) and a cutter one (37), the support five (31) is installed at the front end of the support one (12), the support six (32) is installed at the top end of the main machine box (13), the linear motor one (33) is installed on the support five (31) and the support six (32), the light lever one (34) is installed on the support five (31) and the main machine box (13), the sliding block one (35) is slidingly installed on the light lever one (34), the connecting block (36) is installed on the linear motor one (33) and the sliding block one (35), and the cutter one (37) is installed at the right end of the sliding block one (35).

6. An aircraft tire carcass lay-up alignment device as claimed in claim 2 wherein, The cutting device (03) comprises a plurality of supports seven (41), a plurality of supports eight (42), a plurality of supports nine (43), a plurality of supports ten (44), a plurality of supports eleven (45), a plurality of supports twelve (46), a plurality of linear motors two (47), a plurality of groups of supports thirteen (48), a plurality of light rods two (49), a plurality of sliding blocks two (50), a plurality of supports fourteen (51) and a plurality of cutters two (52), the plurality of supports seven (41) and the plurality of supports eight (42) are respectively installed at the front and back ends of the plurality of feeding belts (15), the plurality of supports nine (43) are respectively installed at the top ends of the plurality of supports seven (41), the plurality of supports ten (44) are respectively installed at the top ends of the plurality of supports eight (42), the plurality of supports eleven (45) and the plurality of supports twelve (46) are respectively installed at the top ends of the plurality of supports nine (43) and the plurality of supports ten (44), the plurality of linear motors two (47) are respectively installed on the plurality of supports eleven (45), the plurality of groups of supports thirteen (48) are respectively installed on the plurality of supports twelve (46), the plurality of light rods two (49) are respectively installed on the plurality of groups of supports thirteen (48), the plurality of sliding blocks two (50) are respectively slidably installed on the plurality of light rods two (49), the plurality of supports fourteen (51) are respectively installed at the bottom ends of the plurality of linear motors two (47) and the plurality of sliding blocks two (50), and the plurality of cutters two (52) are respectively installed at the bottom ends of the plurality of supports fourteen (51).

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