CN214242858U - Automatic winding displacement conveyor of screw for aircraft skin - Google Patents
Automatic winding displacement conveyor of screw for aircraft skin Download PDFInfo
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- CN214242858U CN214242858U CN202022767089.8U CN202022767089U CN214242858U CN 214242858 U CN214242858 U CN 214242858U CN 202022767089 U CN202022767089 U CN 202022767089U CN 214242858 U CN214242858 U CN 214242858U
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- guide rail
- adsorption
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- frame
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Abstract
The utility model discloses an automatic wire arranging and conveying device for a screw for an aircraft skin, which comprises a frame, a conveying mechanism and an adsorption mechanism; the transmission mechanism comprises a transmission gear, a transmission belt and a screw bracket; the transmission gear is positioned on the rack, and the transmission direction of the transmission gear is provided with the corresponding conveyor belt; the conveying belt is connected with the screw bracket in a bearing way; the adsorption mechanism comprises a guide rail, a slide bar, a telescopic rod, an adsorption frame and a coil; one half of the guide rail is positioned at the upper end of the conveying mechanism, and the other half of the guide rail extends to the upper end of the adsorption mechanism at one side of the conveying mechanism; the lower end of the guide rail is provided with a slide bar which can do linear reciprocating motion along the guide rail; connecting rods are respectively vertically arranged at two end parts of the sliding rod; the lower end of the slide bar is also provided with a telescopic rod; the lower ends of the telescopic rod and the two connecting rods are connected with the adsorption frame; a coil is arranged on the adsorption frame; the utility model discloses efficient, with low costs and can rationally collect and carry the screw.
Description
Technical Field
The utility model belongs to the screw processing field, in particular to automatic winding displacement conveyor of screw for aircraft skin.
Background
In the processing process of screws, the screws are placed in vessels in a disordered manner after being threaded, if next procedures such as deburring are required, the automatic implementation is difficult, the labor input is large in the using process of the conventional screw host conveying device, the consumed labor force is large, the production cost is improved, and the conventional conveying device only simply conveys the screws to a detection device when conveying the screws and does not arrange the screws into uniform positions in sequence so as to facilitate subsequent stamping or detection; it is therefore desirable to design a device that will place screws in order in the same direction to facilitate the next process, i.e., automated operation such as deburring by equipment, to improve production efficiency and reduce machining costs.
Disclosure of Invention
The to-be-solved technical problem of the utility model is to provide an automatic winding displacement conveyor of screw that is efficient, with low costs and can rationally collect and carry the screw.
The technical scheme of the utility model is that: an automatic wire arranging and conveying device for a screw for an aircraft skin comprises a rack, a conveying mechanism and an adsorption mechanism; the transmission mechanism and the adsorption mechanism are connected in parallel;
the transmission mechanism comprises a transmission gear, a transmission belt and a screw bracket; the transmission gear is positioned on the rack, and the transmission direction of the transmission gear is provided with the corresponding conveyor belt; the conveying belt is connected with the screw bracket in a bearing way;
the adsorption mechanism comprises a guide rail, a slide bar, a telescopic rod, an adsorption frame and a coil; one half of the guide rail is positioned at the upper end of the conveying mechanism, and the other half of the guide rail extends to the upper end of the adsorption mechanism at one side of the conveying mechanism; the lower end of the guide rail is provided with a slide bar which can do linear reciprocating motion along the guide rail; connecting rods are respectively vertically arranged at two end parts of the sliding rod; the lower end of the slide bar is also provided with a telescopic rod; the telescopic rod is positioned between the two connecting rods; the lower ends of the telescopic rod and the two connecting rods are connected with the adsorption frame; the adsorption frame is wound with a coil.
Specifically, the two ends of the guide rail are provided with limiting blocks for limiting the sliding position of the sliding rod.
Specifically, the length of the adsorption frame is 1/4 of the length of the guide rail.
Specifically, the transmission gear is connected with a speed reduction motor, and the speed reduction motor drives the transmission gear to rotate.
Specifically, a linear vibrator is further arranged on the machine frame.
Compared with the prior art, the beneficial effects of the utility model are that: the utility model discloses a behind the coil circular telegram with the adsorption frame desorption screw, slide to drive mechanism through the guide rail, the outage can make the screw fall, neatly in unison fall to the screw bracket on carry, linear vibrator in the frame can ensure that the screw piles up in the same position of screw bracket when the whereabouts, all the other spaces just idle out, at this moment, the vibrational action of accessible linear vibrator makes screw evenly distributed on the screw bracket, be convenient for acquire more reasonable collection space, it is efficient and rational in infrastructure, use cost is reduced.
Drawings
Fig. 1 is a first schematic structural diagram of the present invention;
FIG. 2 is a second schematic structural diagram of the present invention;
in the figure: 1-a frame; 2-a transmission gear; 3-a conveyor belt; 4, a telescopic rod; 5-screw bracket; 6-a slide bar; 7-an adsorption rack; 8-a guide rail; 9-a coil; 10-a limiting block; 11-a reduction motor; 12-linear vibrator.
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 of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
As shown in fig. 1-2, an automatic cable arranging and conveying device for screws for aircraft skin comprises a frame 1, a conveying mechanism and an adsorption mechanism; the transmission mechanism and the adsorption mechanism are connected in parallel; the frame 1 is also provided with a linear vibrator 12
The transmission mechanism comprises a transmission gear 2, a transmission belt 3 and a screw bracket 5; the transmission gear 2 is positioned on the frame 1, and the transmission direction of the transmission gear 2 is provided with a corresponding conveyor belt 3; the conveyor belt 3 is connected with a screw bracket 5; the transmission gear 2 is connected with a speed reducing motor 11, and the speed reducing motor 11 drives the transmission gear 2 to rotate;
the adsorption mechanism comprises a guide rail 8, a slide bar 6, an expansion link 4, an adsorption frame 7 and a coil 9; one half of the guide rail 8 is positioned at the upper end of the conveying mechanism, and the other half of the guide rail 8 extends to the upper end of the adsorption mechanism at one side of the conveying mechanism; the lower end of the guide rail 8 is provided with a slide bar 6 which can do linear reciprocating motion along the guide rail 8; two ends of the guide rail 8 are provided with limiting blocks 10 for limiting the sliding position of the sliding rod 6; two ends of the slide bar 6 are respectively vertically provided with a connecting rod; the lower end of the slide bar 6 is also provided with a telescopic rod 4; the telescopic rod 4 is positioned between the two connecting rods; the lower ends of the telescopic rod 4 and the two connecting rods are connected with an adsorption frame 7; the coil 9 is wound on the adsorption frame 7, and the length of the adsorption frame 7 is 1/4 of the length of the guide rail 8; the width of the suction frame 7 is the same as the screw width.
When the screw clamping device works, the slide rod 6 slides to the adsorption mechanism through the guide rail 8, the telescopic rod 4 is pressed down, the coil 9 is electrified, the adsorption frame 7 can adsorb screws placed on a workbench, the adsorption force of the large end of each screw is stronger during adsorption, the contact area is larger, the slide rod 6 slides to the upper end of the conveying mechanism, the telescopic rod 4 is pressed down, the coil 9 is powered off, and the screws fall on the screw bracket 5 when losing the adsorption force; this process is constantly repeated, and the position of adsorbing the frame in the upper end of screw bracket is unchangeable, and consequently the position of screw whereabouts can be piled up gradually, and remaining space just is idle to come out, and at this moment, the vibration effect of accessible linear vibrator makes screw evenly distributed on the screw bracket, is convenient for acquire more reasonable collection space, conveys at last.
The preferred embodiments of the present invention disclosed above are intended only to help illustrate the present invention. The preferred embodiments are not intended to be exhaustive or to limit the invention to the precise embodiments disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and its practical application, to thereby enable others skilled in the art to best understand and utilize the invention.
Claims (5)
1. The utility model provides an automatic winding displacement conveyor of screw for aircraft skin which characterized in that: comprises a frame (1), a conveying mechanism and an adsorption mechanism; the transmission mechanism and the adsorption mechanism are connected in parallel;
the transmission mechanism comprises a transmission gear (2), a transmission belt (3) and a screw bracket (5); the transmission gear (2) is positioned on the rack (1), and the corresponding conveyor belt (3) is arranged in the transmission direction of the transmission gear (2); the conveyor belt (3) is connected with the screw bracket (5) in a bearing way;
the adsorption mechanism comprises a guide rail (8), a slide bar (6), an expansion link (4), an adsorption frame (7) and a coil (9); one half of the guide rail (8) is positioned at the upper end of the conveying mechanism, and the other half of the guide rail extends to the upper end of the adsorption mechanism at one side of the conveying mechanism; the lower end of the guide rail (8) is provided with a slide bar (6) which can do linear reciprocating motion along the guide rail (8); two ends of the slide bar (6) are respectively and vertically provided with a connecting rod; the lower end of the slide bar (6) is also provided with a telescopic rod (4); the telescopic rod (4) is positioned between the two connecting rods; the lower ends of the telescopic rod (4) and the two connecting rods are connected with an adsorption frame; and a coil (9) is wound on the adsorption frame (7).
2. The automatic cable feeding device for the screws for the aircraft skin according to claim 1, wherein: and two ends of the guide rail (8) are provided with limiting blocks (10) for limiting the sliding position of the sliding rod (6).
3. The automatic cable feeding device for the screws for the aircraft skin according to claim 1, wherein: the length of the adsorption frame is 1/4 of the length of the guide rail (8).
4. The automatic cable feeding device for the screws for the aircraft skin according to claim 1, wherein: the transmission gear (2) is connected with the speed reducing motor (11), and the speed reducing motor (11) drives the transmission gear (2) to rotate.
5. The automatic cable feeding device for the screws for the aircraft skin according to claim 1, wherein: the frame (1) is also provided with a linear vibrator (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022767089.8U CN214242858U (en) | 2020-11-25 | 2020-11-25 | Automatic winding displacement conveyor of screw for aircraft skin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022767089.8U CN214242858U (en) | 2020-11-25 | 2020-11-25 | Automatic winding displacement conveyor of screw for aircraft skin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214242858U true CN214242858U (en) | 2021-09-21 |
Family
ID=77734167
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022767089.8U Active CN214242858U (en) | 2020-11-25 | 2020-11-25 | Automatic winding displacement conveyor of screw for aircraft skin |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214242858U (en) |
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2020
- 2020-11-25 CN CN202022767089.8U patent/CN214242858U/en active Active
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