CN215251622U

CN215251622U - 360 rotatory aircraft nose mechanism

Info

Publication number: CN215251622U
Application number: CN202120464189.5U
Authority: CN
Inventors: 李国胜; 林淑霞
Original assignee: Dongguan Baoyun Automation Equipment Co ltd
Current assignee: Dongguan Baoyun Automation Equipment Co ltd
Priority date: 2021-03-03
Filing date: 2021-03-03
Publication date: 2021-12-21
Anticipated expiration: 2031-03-03

Abstract

The utility model discloses a 360 rotatory aircraft nose mechanism relates to garment machinery, including aircraft nose, first motor, speed reducer, revolving stage, mounting panel, elevating gear, pneumo-electric sliding ring, elevating gear installs on the revolving stage, and first motor is installed on the speed reducer, and the speed reducer is installed on the revolving stage, is provided with the rotary disk on the revolving stage, and the speed reducer passes through gear drive and drives the rotary disk rotation, and the aircraft nose passes through the mounting panel to be installed on the rotary disk, is provided with the through-hole on the revolving stage, and the pneumo-electric sliding ring passes the through-hole and installs on the mounting panel, and the pneumo-electric circuit between external and the aircraft nose is connected to the pneumo-electric sliding ring, the beneficial effects of the utility model: the machine head can rotate towards any direction of 360 degrees through the rotating table, so that the direction of the machine head is consistent with the trend of the sewing thread all the time, the consistency of stitches in all directions is ensured, and the quality of finished clothes is improved.

Description

360 rotatory aircraft nose mechanism

Technical Field

The utility model relates to a garment machinery field is a 360 rotatory aircraft nose mechanisms particularly.

Background

Along with the advance of the automation process in the field of sewing machines, in the prior art, the machine head is driven to automatically work through the motor and the synchronous belt, the material pressing and sewing mechanism is used for driving the cloth to move in a certain direction, so that a required line is sewn, the sewing work is completed in such a way, when a sewing thread needs to turn, the material pressing and sewing mechanism can drive the cloth to move in the corresponding direction, the sewing thread is enabled to appear in the corresponding position, but the machine head cannot rotate, the trend of the sewing thread is inconsistent with the direction of the machine head, the stitch after the turning is enabled to be quite messy compared with the previous stitch, and the quality of the clothes is affected.

SUMMERY OF THE UTILITY MODEL

To the above defect, the utility model provides a 360 rotatory aircraft nose mechanism can make the aircraft nose rotatory towards 360 arbitrary directions through the revolving stage to the direction that makes the aircraft nose is unanimous with the trend of suture all the time, guarantees the unanimity of the stitch seam of each direction, has realized the stability of stitch seam, has improved the quality of finished product clothes.

The technical scheme of the utility model is that:

the utility model provides a 360 rotatory aircraft nose mechanism, includes aircraft nose, first motor, speed reducer, revolving stage, mounting panel, elevating gear, pneumoelectric slip ring, elevating gear installs on the revolving stage, a serial communication port, first motor is installed on the speed reducer, the speed reducer is installed on the revolving stage, be provided with the rotary disk on the revolving stage, be provided with gear in the revolving stage, the speed reducer passes through gear drives the rotary disk rotates, the aircraft nose passes through the mounting panel is installed on the rotary disk, be provided with the through-hole on the revolving stage, the pneumoelectric slip ring passes the through-hole is installed on the mounting panel, pneumoelectric slip ring connects the pneumoelectric circuit between external world and the aircraft nose.

Preferably, be provided with the bed hedgehopping post on the mounting panel, during the through-hole of bed hedgehopping post access revolving stage, be provided with the screw on the bed hedgehopping post, the pneumoelectric slip ring passes through the screw and installs on the bed hedgehopping post with the screw cooperation, the bed hedgehopping post can bed hedgehopping the pneumoelectric slip ring, the height of bed hedgehopping post can set up when dispatching from the factory, the bed hedgehopping post can bed hedgehopping the pneumoelectric slip ring to be applicable to different circuits, increase the application scope of pneumoelectric slip ring.

Preferably, the heightening column is fixed on the mounting plate in a welding mode, so that the heightening column can be fixed firmly and cannot fall off.

Preferably, both sides of mounting panel all are provided with the screw, and the one side of mounting panel is passed through the screw and is installed on the rotary disk with the screw cooperation, and the another side of mounting panel is passed through the screw and is installed at the aircraft nose with the screw cooperation, and the mounting panel links together rotary disk and aircraft nose, can guarantee through screw and screw cooperation fixed mounting panel that the mounting panel is fixed firm, is difficult to drop.

Preferably, the inside hollow structure that is of mounting panel, the mounting panel side is provided with the opening, and the pneumoelectric circuit of aircraft nose gets into the mounting panel from the opening part of mounting panel side, passes the inside line connection with pneumoelectric slip ring of mounting panel, and rethread pneumoelectric slip ring and external intercommunication, the hollow structure and the side opening of mounting panel can make the circuit of pneumoelectric slip ring flow out from the mounting panel, receive corresponding structurally again, and such setting can save space, and it is pleasing to the eye to increase the product.

Preferably, the second motor, the belt transmission device and the needle are arranged on the machine head, the belt transmission device comprises a driving wheel and a belt, the driving wheel is driven by the second motor to rotate, kinetic energy of the driving wheel is transmitted to the driven wheel by the belt, so that the driven wheel is driven to rotate, the needle is driven to reciprocate up and down by the driven wheel, and the kinetic energy of the motor is transmitted to the needle through the belt transmission device, so that the needle automatically works.

Preferably, the lifting device comprises a lifting cylinder, a sliding rail, a sliding block and a lifting platform, the lifting cylinder is connected with the lifting platform through a piston rod, the sliding block is installed on the lifting platform, the sliding block is fixed on the sliding rail, the lifting cylinder drives the lifting platform and the sliding block to do lifting motion on the sliding rail through the piston rod, and the lifting cylinder drives the lifting platform to rise through the piston rod, so that the machine needle is driven to move upwards, clothes are kept away, and the clothes and stitches can be adjusted; after the adjustment is finished, the lifting air cylinder drives the lifting platform to be lowered through the piston rod, so that the machine needle is driven to move downwards to return to a sewing state, and a sewing process is performed.

The utility model has the advantages that:

the utility model discloses be provided with revolving stage and aircraft nose, be provided with the rotary disk on the revolving stage, the aircraft nose passes through the mounting panel and installs on the rotary disk, and when the speed reducer passes through gear drive and drives the rotary disk pivoted, can drive mounting panel and aircraft nose rotation, the gas-electric circuit when rotating in order to solve the aircraft nose can not the pivoted problem, the utility model discloses still be provided with the gas-electric sliding ring, be provided with stator and rotor on the gas-electric sliding ring, can be with the gas-electric circuit from the stator input, transmit to the rotor in, on the reconnection aircraft nose, the aircraft nose synchronous revolution can be followed to the rotor, and the stator can not rotate, can guarantee when the aircraft nose is rotatory, the gas-electric circuit of aircraft nose can not block and tie a knot, guarantees the stability of gas-electric transmission.

The utility model is suitable for a sewing work of the suture that need turn round on the clothing, when the suture need turn round, press material sewing machine to construct and pull the cloth and remove to the direction that corresponds, rotary disk on the revolving stage also can rotate the direction that corresponds under the drive of motor to it is rotatory to drive the aircraft nose, the direction that makes the aircraft nose and the direction of suture still keep unanimous, thereby guarantee the uniformity of the suture before turning round and after turning round, make the stitch of finished product clothing stable, the quality of clothes has been improved.

To sum up, compared with the prior art, the utility model provides a pair of 360 rotatory aircraft nose mechanisms can make the aircraft nose rotatory towards 360 arbitrary directions through the revolving stage to the direction that makes the aircraft nose is unanimous with the trend of suture all the time, guarantees the unanimity of the stitch seam of each direction, has realized the stability of stitch seam, has improved the quality of finished product clothes.

Drawings

Fig. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a schematic side view of the present invention;

fig. 3 is a schematic view of the exploded structure of the present invention.

Detailed Description

In order that those skilled in the art can better understand the technical solutions provided by the present invention, the following description is provided in connection with specific embodiments.

Referring to fig. 1-3, fig. 1 is a schematic view of the overall structure of the present invention; FIG. 2 is a schematic side view of the present invention; fig. 3 is a schematic view of the exploded structure of the present invention.

An embodiment of the utility model provides a 360 rotatory aircraft nose mechanism, the part name that each reference numeral corresponds in the picture is as follows: the device comprises a machine head 1, a first motor 2, a speed reducer 3, a rotating table 4, a mounting plate 5, a gas-electric slip ring 6, a rotating disc 7, a heightening column 8, a second motor 9, a driving wheel 10, a belt 11, a driven wheel 12, a lifting cylinder 13, a sliding rail 14, a sliding block 15, a lifting platform 16 and a piston rod 17.

The utility model provides a 360 rotatory aircraft nose mechanism, includes aircraft nose 1, first motor 2, speed reducer 3, revolving stage 4, mounting panel 5, elevating gear, pneumoelectric slip ring 6, elevating gear installs on the revolving stage 4, a serial communication port, first motor 2 is installed on the speed reducer 3, speed reducer 3 is installed on the revolving stage 4, be provided with rotary disk 7 on the revolving stage 4, be provided with gear transmission in the revolving stage 4, speed reducer 3 passes through gear transmission drives rotary disk 7 rotates, aircraft nose 1 passes through mounting panel 5 is installed on the rotary disk 7, be provided with the through-hole on the revolving stage 4, pneumoelectric slip ring 6 passes the through-hole is installed on mounting panel 5, pneumoelectric slip ring 6 connects the external pneumoelectric circuit between 1 and the aircraft nose.

Be provided with bed hedgehopping post 8 on mounting panel 5, in the through-hole of bed hedgehopping post 8 access revolving stage 4, be provided with the screw on the bed hedgehopping post 8, pneumoelectric slip ring 6 passes through the screw and the screw cooperation is installed on bed hedgehopping post 8, bed hedgehopping post 8 can bed hedgehopping pneumoelectric slip ring 6, bed hedgehopping post 8 highly can set up when dispatching from the factory, bed hedgehopping post 8 can bed hedgehopping pneumoelectric slip ring 6, so as to be applicable to different circuits, increase pneumoelectric slip ring 6's application scope.

The heightening column 8 is fixed on the mounting plate 5 in a welding mode, so that the heightening column 8 can be firmly fixed and cannot fall off.

The two sides of mounting panel 5 all are provided with the screw, and the one side of mounting panel 5 is passed through the screw and is installed on rotary disk 7 with the screw cooperation, and the another side of mounting panel 5 is passed through the screw and is installed on aircraft nose 1 with the screw cooperation, and mounting panel 5 links together rotary disk 7 and aircraft nose 1, can guarantee through screw and screw cooperation fixed mounting panel 5 that mounting panel 5 is fixed firm, is difficult to drop.

The inside hollow structure that is of

mounting panel

5, 5 sides of mounting panel are provided with the opening, the pneumoelectric circuit of aircraft nose 1 gets into mounting panel 5 from the opening part of 5 sides of mounting panel, pass 5 inside and pneumoelectric slip ring 6's of mounting panel line connection, rethread pneumoelectric slip ring 6 and external intercommunication, the hollow structure and the side opening of mounting panel 5 can make pneumoelectric slip ring 6's circuit flow out from mounting panel 5, receive corresponding structurally again, such setting can save space, it is pleasing to the eye to increase the product.

Be provided with second motor 9 on the

aircraft nose

1, 11 transmission in belt, the eedle, 11 transmission in belt includes action wheel 10, belt 11, from driving wheel 12, second motor 9 drives action wheel 10 rotatory, belt 11 transmits the kinetic energy of action wheel 10 to from driving wheel 12 on, thereby it is rotatory to drive from driving wheel 12, from driving wheel 12 drive eedle and be up-and-down reciprocating motion, transmit the kinetic energy of motor to the eedle through 11 transmission in belt, make the eedle can make up work automatically.

The lifting device comprises a lifting cylinder 13, a sliding rail 14, a sliding block 15 and a lifting platform 16, the lifting cylinder 13 is connected with the lifting platform 16 through a piston rod 17, the sliding block 15 is installed on the lifting platform 16, the sliding block 15 is fixed on the sliding rail 14, the lifting cylinder 13 drives the lifting platform 16 and the sliding block 15 to do lifting motion on the sliding rail 14 through the piston rod 17, and the lifting cylinder 13 drives the lifting platform 16 to rise through the piston rod 17, so that a machine needle is driven to move upwards to be far away from clothes, and the clothes and stitches can be adjusted; after the adjustment is finished, the lifting cylinder 13 drives the lifting table 16 to lower through the piston rod 17, so as to drive the needle to move downwards, return to a sewing state and perform a sewing process.

The utility model discloses an installation and working method do:

install first motor 2 on speed reducer 3, install speed reducer 3 on revolving stage 4, install elevating gear on revolving stage 4, fix bed hedgehopping post 8 on mounting panel 5 through welded installation, install the one side of mounting panel 5 on rotary disk 7 through screw and screw cooperation, install the another side of mounting panel 5 on aircraft nose 1 through screw and screw cooperation, install pneumo-electric slip ring 6 on mounting panel 5 through the through-hole of rotary disk 7, the pneumo-electric circuit of aircraft nose 1 links to each other with the external world through pneumo-electric slip ring 6.

In the automatic sewing process of the sewing machine, when the sewing thread needs to turn, the material pressing and sewing mechanism drags the cloth to move towards the sewing thread direction, the first motor 2 works to transmit kinetic energy to the speed reducer 3, the speed reducer 3 transmits the kinetic energy to the rotating disk 7 through the rotating platform 4, and the rotating disk 7 rotates, so that the machine head 1 is driven to rotate, and the direction of the machine head 1 and the direction of the sewing thread are kept consistent.

The utility model has the advantages that:

the utility model discloses be provided with revolving stage 4 and aircraft nose 1, be provided with rotary disk 7 on the revolving stage 4, aircraft nose 1 is installed on rotary disk 7 through mounting panel 5, when speed reducer 3 passes through gear drive and drives rotary disk 7 pivoted, can drive mounting panel 5 and aircraft nose 1 and rotate, the gas-electric circuit when rotating in order to solve aircraft nose 1 can not the pivoted problem, the utility model discloses still be provided with gas-electric sliding ring 6, be provided with stator and rotor on the gas-electric sliding ring 6, can be with the gas-electric circuit from the stator input, transmit to the rotor in, on the reconnection slewing mechanism, the slewing mechanism synchronous revolution can be followed to the rotor, and the stator can not rotate, when can guaranteeing aircraft nose 1 rotation, aircraft nose 1's gas-electric circuit can not block and knot, guarantees the stability of gas-electric transmission.

The utility model is suitable for a sewing work of the suture that need turn round on the clothing, when the suture need turn round, press the material to make up the mechanism and pull the cloth and remove to the direction that corresponds, rotary disk 7 on revolving stage 4 also can rotate the direction that corresponds under the drive of motor, thereby it is rotatory to drive aircraft nose 1, the direction of advance that makes aircraft nose 1 and the direction of suture still keep unanimous, thereby the assurance turns round before and the uniformity of the suture after turning round, the stitch that makes finished product clothing is stable, the quality of clothes has been improved.

The above is only a preferred embodiment of the present invention, and it should be noted that the above preferred embodiment should not be considered as limiting the present invention, and the protection scope of the present invention should be subject to the scope defined by the claims. It will be apparent to those skilled in the art that various modifications and enhancements can be made without departing from the spirit and scope of the invention, and such modifications and enhancements are intended to be within the scope of the invention.

Claims

1. The utility model provides a 360 rotatory aircraft nose mechanism, includes aircraft nose, first motor, speed reducer, revolving stage, mounting panel, elevating gear, pneumoelectric slip ring, elevating gear installs on the revolving stage, a serial communication port, first motor is installed on the speed reducer, the speed reducer is installed on the revolving stage, be provided with the rotary disk on the revolving stage, be provided with gear in the revolving stage, the speed reducer passes through gear drives the rotary disk rotates, the aircraft nose passes through the mounting panel is installed on the rotary disk, be provided with the through-hole on the revolving stage, the pneumoelectric slip ring passes the through-hole is installed on the mounting panel, pneumoelectric slip ring connects the pneumoelectric circuit between external world and the aircraft nose.

2. The 360 ° rotary machine head mechanism of claim 1, wherein the mounting plate is provided with a raising column, the raising column is inserted into the through hole of the rotary table, the raising column is provided with a screw hole, and the gas-electric slip ring is mounted on the raising column through a screw and the screw hole in a matching manner.

3. A 360 ° rotary head mechanism as claimed in claim 2, wherein the raising column is fixed to the mounting plate by welding.

4. A 360 ° rotary die head mechanism according to claim 1, wherein the mounting plate has screw holes on both sides, one side of the mounting plate is mounted on the rotary disk by screws and screw holes, the other side of the mounting plate is mounted on the die head by screws and screw holes, and the mounting plate connects the rotary disk and the die head together.

5. The 360 ° rotary machine head mechanism of claim 1, wherein the inside of the mounting plate is hollow, the side of the mounting plate is provided with an opening, and the gas-electric circuit of the machine head enters the mounting plate from the opening on the side of the mounting plate, passes through the inside of the mounting plate to be connected with the circuit of the gas-electric slip ring, and then is communicated with the outside through the gas-electric slip ring.

6. The 360-degree-of-rotation handpiece mechanism of claim 1, wherein the handpiece is provided with a second motor, a belt transmission device and a needle, the belt transmission device comprises a driving wheel and a belt, the driven wheel is driven by the second motor to drive the driving wheel to rotate, the belt transmits kinetic energy of the driving wheel to the driven wheel so as to drive the driven wheel to rotate, and the driven wheel drives the needle to reciprocate up and down.

7. The 360-degree rotation handpiece mechanism according to claim 1, wherein the lifting device comprises a lifting cylinder, a slide rail, a slider and a lifting table, the lifting cylinder is connected with the lifting table through a piston rod, the slider is mounted on the lifting table, the slider is fixed on the slide rail, and the lifting cylinder drives the lifting table and the slider to move up and down on the slide rail through the piston rod.