CN221848240U - An aviation tire wire ring winding device - Google Patents

Abstract

The utility model relates to the technical field of aviation tire processing, and discloses an aviation tire bead ring winding device, which comprises a base, wherein the bottom surface of the base is fixedly provided with supporting legs, the number of the supporting legs is four and is uniformly distributed on the bottom surface around the base, the top surface of the right end of the base is fixedly provided with a paying-off mechanism, and the left side surface of the paying-off mechanism is fixedly connected with the right side surface of the winding mechanism; the paying-off mechanism comprises a paying-off part and a power part, power section bottom surface and pay-off the top surface of the part is fixedly connected; the power part comprises a device plate, and a motor is fixedly arranged on the top surface of the device plate; the winding mechanism comprises a winding part and a connecting part. Through being provided with winding mechanism, through being provided with the cooperation work of servo motor and carousel for the baffle can block into and place inside the roller, can protect the bead ring, appears the position offset when preventing its winding. And can leave the placing roller through the baffle plate, so that the steel wire ring can be quickly taken and used after being wound.

Description

An aviation tire wire ring winding device

Technical Field

The utility model relates to the technical field of aviation tire processing, in particular to an aviation tire wire ring winding device.

Background Art

There are wire rings inside both aircraft tires and automobile tires. The wire rings are wound and processed by a wire ring winding machine, and the wire ring winding machine usually has a wire storage drum.

A Chinese patent discloses a wire ring winding device for aviation tire production, with publication number CN219004139U, comprising a first connecting plate, the bottom end of which is fixedly connected to two first limit rods; a second connecting plate, the second connecting plate is fixedly connected to the top ends of the two first limit rods; a limit connecting plate, the limit connecting plate is arranged on the upper side of the second connecting plate, and when the limit connecting plate rotates through the second clamping block, it will drive the limit wheel to rotate, thereby achieving the effect of rotating the winding wheel.

However, there are still the following disadvantages: when the wire ring winding device for producing aircraft tires is winding the wire ring, it is impossible to quickly disassemble and take it out after winding, so a wire ring winding device for aircraft tires is designed.

Utility Model Content

The utility model aims to provide an aviation tire wire ring winding device to solve the problems raised in the above background technology.

To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an aviation tire wire ring winding device comprises a base, the bottom surface of the base is fixedly provided with support legs, the number of the support legs is four and they are evenly distributed around the bottom surface of the base, a wire-releasing mechanism is fixedly provided on the top surface of the right end of the base, and the left side surface of the wire-releasing mechanism is fixedly connected to the right side surface of the winding mechanism;

The wire-releasing mechanism comprises a wire-releasing part and a power part, and the bottom surface of the power part and the top surface of the wire-releasing part are fixedly connected;

The power unit comprises a device plate, and a motor is fixedly arranged on the top surface of the device plate;

The winding mechanism comprises a winding portion and a connecting portion, and a side surface of the winding portion and a side surface of the connecting portion are fixedly connected;

The winding part comprises a fixing plate, and the back surface of the left end of the base is fixedly connected with the front surface of the fixing plate.

Preferably, the front face of the device plate and the back face of the right end of the base are fixedly connected, the bottom face of the motor output rod passes through the top face of the device plate and extends to the inside of the device plate, an active rod is fixedly provided on the bottom face of the motor output rod, and the surface of the active rod and the inner wall of the base are rotatably connected by a bearing.

Preferably, the active rod surface fixing sleeve is provided with a winding roller, the winding roller surface fixing sleeve is provided with a wire rope, a driven rod is provided inside the left end of the base, and the driven rod surface and the inner wall of the base are rotatably connected by a bearing.

Preferably, two pulleys are fixedly sleeved on the bottom end surfaces of the active rod and the driven rod respectively, belts are wound around the surfaces of the two pulleys, and the two pulleys are connected by belt transmission.

Preferably, a placement roller is fixedly provided on the top surface of the driven rod, an electromagnet is fixedly provided on the inner wall of the placement roller, a magnet is provided on the right end surface of the electromagnet, the side surface of the electromagnet is magnetically connected to the side surface of the magnet, and the inner wall of the magnet is magnetically connected to the surface of the wire rope.

Preferably, a connecting plate is provided on the inner wall at the front end of the fixed plate, the side of the connecting plate is frictionally and slidingly connected to the inner wall of the fixed plate, a telescopic plate is hingedly provided on the inner wall at the top end of the connecting plate, an L-shaped plate is fixedly provided on the left side of the fixed plate, and a servo motor is fixedly provided on the inner wall of the L-shaped plate.

Preferably, a turntable is fixedly provided on the right end face of the servo motor output rod, the right side face of the bottom end of the turntable is fixedly connected by a light rod and a left side face of the telescopic plate, a baffle is fixedly provided on the bottom face of the connecting plate output rod, a connecting rod is fixedly provided on the bottom face of the baffle, and the surface of the connecting rod is sealed and clamped with the inner wall of the placement roller.

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

1. The aviation tire wire ring winding device is provided with a winding mechanism, and the servo motor and the turntable cooperate to make the baffle plate snap into the inside of the placement roller, so that the wire ring can be protected from position deviation when it is wound, and can leave the placement roller through the baffle plate, so that the wire ring can be quickly taken out for use after it is wound;

2. The aircraft tire wire ring winding device is provided with an electromagnet and a magnet to cooperate with each other, so that the wire rope can be quickly connected to the magnet, so that the wire rope can be quickly released and wound, and the magnet can be adsorbed on the surface of the placement roller by the electromagnet, so as to facilitate the improvement of the wire ring winding work efficiency;

3. The aviation tire wire ring winding device is provided with a wire-releasing mechanism, and the cooperation of a motor and an active rod is provided, so that the winding roller can drive the surface-wound wire rope to release the wire, so that the wire rope can be wound on the placement roller, thereby allowing the wire ring to be quickly wound and subsequently processed into the interior of the aviation tire.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG1 is a perspective schematic diagram of the front structure of the utility model;

FIG2 is a perspective cross-sectional view of the front structure of the utility model;

FIG3 is a perspective view of the back structure of the utility model;

FIG4 is a three-dimensional enlarged schematic diagram of the structure of area A in FIG2 of the present utility model;

FIG. 5 is a three-dimensional enlarged schematic diagram of the structure of area B in FIG. 3 of the present invention.

In the figure: 1. base; 2. supporting legs; 3. pay-off mechanism; 301. device plate; 302. motor; 303. active rod; 304. winding roller; 305. wire rope; 306. pulley; 307. belt; 308. driven rod; 4. winding mechanism; 401. placing roller; 402. fixing plate; 403. connecting plate; 404. baffle; 405. connecting rod; 406. electromagnet; 407. magnet; 408. L-shaped plate; 409. servo motor; 410. turntable; 411. telescopic plate.

DETAILED DESCRIPTION

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.

Embodiment 1

Please refer to Figures 1 to 5, a device for winding a wire ring of an aircraft tire comprises a base 1, a bottom surface of the base 1 is fixedly provided with support legs 2, the number of the support legs 2 is four and they are evenly distributed on the bottom surface around the base 1, and the four support legs 2 make the base 1 more stable, a wire-releasing mechanism 3 is fixedly provided on the top surface of the right end of the base 1, and the left side surface of the wire-releasing mechanism 3 is fixedly connected to the right side surface of the winding mechanism 4; the wire-releasing mechanism 3 comprises a wire-releasing part and a power part, and the bottom surface of the power part is fixedly connected to the top surface of the wire-releasing part; the power part comprises a device plate 301, and a motor 302 is fixedly provided on the top surface of the device plate 301; the winding mechanism 4 comprises a winding part and a connecting part, and the side surface of the winding part is fixedly connected to the side surface of the connecting part; the winding part comprises a fixing plate 402, and the back surface of the left end of the base 1 is fixedly connected to the front surface of the fixing plate 402;

During operation, the base 1 is placed in a processing room by means of four supporting legs 2, and the motor 302 is started to rotate the active rod 303.

Further, the front of the device plate 301 is fixedly connected to the back of the right end of the base 1, the bottom surface of the output rod of the motor 302 passes through the top surface of the device plate 301 and extends to the inside of the device plate 301, the model of the motor 302 is Y2-112M-6, and the bottom surface of the output rod of the motor 302 is fixedly provided with an active rod 303, and the surface of the active rod 303 and the inner wall of the base 1 are rotatably connected by a bearing;

During operation, the motor 302 is started to rotate the active rod 303 , and the driven rod 308 drives the placement roller 401 to rotate through the transmission effect of the pulley 306 and the belt 307 .

Furthermore, a winding roller 304 is fixedly sleeved on the surface of the active rod 303, and a steel wire 305 is fixedly sleeved on the surface of the winding roller 304. The steel wire 305 is the raw material of the steel wire ring inside the tire. A driven rod 308 is arranged inside the left end of the base 1, and the surface of the driven rod 308 and the inner wall of the base 1 are rotatably connected by a bearing;

During operation, the active rod 303 rotates, and through the transmission effect of the pulley 306 and the belt 307, the driven rod 308 drives the placement roller 401 to rotate, thereby performing the wire-laying and winding operation on the wire rope 305.

Furthermore, two pulleys 306 are fixedly sleeved on the bottom surfaces of the active rod 303 and the driven rod 308, respectively. Belts 307 are wound around the surfaces of the two pulleys 306, and the two pulleys 306 are connected by the belts 307.

During operation, the active rod 303 rotates, and through the transmission effect of the pulley 306 and the belt 307, the driven rod 308 drives the placement roller 401 to rotate.

Further, a placement roller 401 is fixedly provided on the top surface of the driven rod 308, an electromagnet 406 is fixedly provided on the inner wall of the placement roller 401, the electromagnet 406 can be controlled by an external power supply, a magnet 407 is provided on the right end surface of the electromagnet 406, the side surface of the electromagnet 406 is magnetically connected to the side surface of the magnet 407, and the inner wall of the magnet 407 is magnetically connected to the surface of the wire rope 305;

During operation, after the wire ring is wound around the surface of the placement roller 401, the connecting plate 403 is started to move the baffle 404 upward, so that the connecting rod 405 leaves the inside of the placement roller 401, and the electromagnet 406 is turned off to take the wound wire ring.

Furthermore, a connecting plate 403 is provided on the inner wall of the front end of the fixing plate 402, the side of the connecting plate 403 is frictionally and slidably connected to the inner wall of the fixing plate 402, a telescopic plate 411 is hingedly provided on the inner wall of the top end of the connecting plate 403, an L-shaped plate 408 is fixedly provided on the left side of the fixing plate 402, and a servo motor 409 is fixedly provided on the inner wall of the L-shaped plate 408;

During operation, after the wire ring is wound around the surface of the placement roller 401, the servo motor 409 is started to rotate the turntable 410.

Further, a turntable 410 is fixedly provided on the right end face of the output rod of the servo motor 409, the right side face of the bottom end of the turntable 410 is fixedly connected by a light rod and the left side face of the telescopic plate 411, a baffle 404 is fixedly provided on the bottom face of the output rod of the connecting plate 403, a connecting rod 405 is fixedly provided on the bottom face of the baffle 404, and the surface of the connecting rod 405 is sealed and clamped with the inner wall of the placement roller 401;

During operation, the connected telescopic plate 411 moves, and at the same time, the hinge of the connecting plate 403 drives it to stretch upward, so that the baffle 404 moves upward.

Working principle: When in use, first place the base 1 in the processing workshop through the four supporting legs 2, start the electromagnet 406, place the magnet 407 on the surface of the electromagnet 406, insert one end of the wire rope 305 on the surface of the winding roller 304 into the slot of the magnet 407, magnetically connect the wire rope 305 through the magnet 407, start the motor 302, make the active rod 303 rotate, and drive the driven rod 308 through the pulley 306 and the belt 307. The placement roller 401 rotates to unwind the wire rope 305. When the wire ring is wound on the surface of the placement roller 401, the servo motor 409 is started to rotate the turntable 410, which is moved through the connected telescopic plate 411 and simultaneously driven to stretch upward at the hinge with the connecting plate 403, so that the baffle 404 moves upward and the connecting rod 405 leaves the inside of the placement roller 401. The electromagnet 406 is turned off and the wound wire ring can be taken out.

Although the embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims (7)

1. An aircraft tire wire ring winding device, comprising a base (1), characterized in that: a support leg (2) is fixedly arranged on the bottom surface of the base (1), the number of the support legs (2) is four and they are evenly distributed on the bottom surface around the base (1), a wire-releasing mechanism (3) is fixedly arranged on the top surface of the right end of the base (1), and the left side surface of the wire-releasing mechanism (3) is fixedly connected to the right side surface of the winding mechanism (4); The wire-releasing mechanism (3) comprises a wire-releasing part and a power part, wherein the bottom surface of the power part and the top surface of the wire-releasing part are fixedly connected; The power unit comprises a device plate (301), and a motor (302) is fixedly arranged on the top surface of the device plate (301); The winding mechanism (4) comprises a winding portion and a connecting portion, and the side surface of the winding portion and the side surface of the connecting portion are fixedly connected; The winding portion comprises a fixing plate (402), and the back surface of the left end of the base (1) and the front surface of the fixing plate (402) are fixedly connected. 2. An aviation tire wire ring winding device according to claim 1, characterized in that: the front face of the device plate (301) is fixedly connected to the back face of the right end of the base (1), the bottom face of the output rod of the motor (302) passes through the top face of the device plate (301) and extends to the inside of the device plate (301), an active rod (303) is fixedly arranged on the bottom face of the output rod of the motor (302), and the surface of the active rod (303) and the inner wall of the base (1) are rotatably connected by a bearing. 3. An aviation tire wire ring winding device according to claim 2, characterized in that: a winding roller (304) is fixedly sleeved on the surface of the active rod (303), a steel wire rope (305) is fixedly sleeved on the surface of the winding roller (304), a driven rod (308) is arranged inside the left end of the base (1), and the surface of the driven rod (308) and the inner wall of the base (1) are rotatably connected by a bearing. 4. An aviation tire wire ring winding device according to claim 3 is characterized in that: two pulleys (306) are fixedly sleeved on the bottom end surfaces of the active rod (303) and the driven rod (308), and belts (307) are wound around the surfaces of the two pulleys (306), and the two pulleys (306) are connected by the belt (307). 5. An aviation tire wire ring winding device according to claim 3, characterized in that: a placement roller (401) is fixedly provided on the top surface of the driven rod (308), an electromagnet (406) is fixedly provided on the inner wall of the placement roller (401), a magnet (407) is provided on the right end surface of the electromagnet (406), the side surface of the electromagnet (406) is magnetically connected to the side surface of the magnet (407), and the inner wall of the magnet (407) is magnetically connected to the surface of the wire rope (305). 6. An aviation tire wire ring winding device according to claim 1, characterized in that: a connecting plate (403) is provided on the inner wall of the front end of the fixed plate (402), the side of the connecting plate (403) is frictionally and slidingly connected to the inner wall of the fixed plate (402), a telescopic plate (411) is hingedly provided on the inner wall of the top end of the connecting plate (403), an L-shaped plate (408) is fixedly provided on the left side of the fixed plate (402), and a servo motor (409) is fixedly provided on the inner wall of the L-shaped plate (408). 7. An aviation tire wire ring winding device according to claim 6, characterized in that: a turntable (410) is fixedly provided on the right end face of the output rod of the servo motor (409), the right side face of the bottom end of the turntable (410) is fixedly connected by a light rod and a left side face of a telescopic plate (411), a baffle (404) is fixedly provided on the bottom face of the output rod of the connecting plate (403), a connecting rod (405) is fixedly provided on the bottom face of the baffle (404), and the surface of the connecting rod (405) is sealed and clamped with the inner wall of the placement roller (401).