CN217345152U - Self-discharging formula list cylinder positioning mechanism - Google Patents
Self-discharging formula list cylinder positioning mechanism Download PDFInfo
- Publication number
- CN217345152U CN217345152U CN202220376118.4U CN202220376118U CN217345152U CN 217345152 U CN217345152 U CN 217345152U CN 202220376118 U CN202220376118 U CN 202220376118U CN 217345152 U CN217345152 U CN 217345152U
- Authority
- CN
- China
- Prior art keywords
- assembly
- rotating disc
- self
- positioning mechanism
- dumping
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Automatic Assembly (AREA)
Abstract
The utility model relates to a self-discharging formula single cylinder positioning mechanism, including horizontal direction's rotary disk, pivot, drive assembly, coupling assembling, spacing subassembly and terminal surface locating component, the pivot is passed the rotary disk and is rotated rather than rotating along vertical direction and link to each other, and one side of rotary disk is located to drive assembly for drive rotary disk revolutes the axis of axle and rotates, and coupling assembling's quantity is two, and both set up relatively and lie in same one side of rotary disk. Can control the fixed subassembly of terminal surface of two relative settings through the single cylinder to the location process of unmanned aerial vehicle wing body, the drive mode of single cylinder for this positioning mechanism carries out quick location to unmanned aerial vehicle wing body, thereby satisfies the rapid Assembly and the interchangeability requirement of product, improves the efficiency in the technology course of working.
Description
Technical Field
The utility model relates to an industrial technology field specifically is a self-discharging formula list cylinder positioning mechanism.
Background
In recent years, unmanned aerial vehicles are applied to civil use and national defense in many fields; based on the requirements of use occasions and multiple functions, the requirements of the modern unmanned aerial vehicle on quick and accurate assembly and interchangeability of product parts are gradually improved. The wing body of the unmanned aerial vehicle is rapidly positioned and supported in an auxiliary mode, so that the requirements of rapid assembly and interchangeability of products are met, and the efficiency in the process of processing is improved.
SUMMERY OF THE UTILITY MODEL
Not enough to prior art, the utility model provides a self-discharging formula list cylinder positioning mechanism has solved the problem of the unable quick centering of unmanned aerial vehicle wing body and location.
In order to achieve the above object, the utility model provides a following technical scheme: a self-unloading single-cylinder positioning mechanism comprises a rotating disc, a rotating shaft, a driving assembly, two groups of connecting assemblies, a limiting assembly corresponding to the connecting assemblies and an end face positioning assembly corresponding to the limiting assembly in the horizontal direction;
the rotating shaft coaxially penetrates through the rotating disc along the vertical direction and is connected with the rotating disc in a rotating mode;
the driving assembly is in transmission connection with the rotating disc and drives the rotating disc to rotate around the rotating shaft;
the two groups of connecting components are oppositely arranged on the periphery of the rotating disc and are respectively in transmission connection with the rotating disc;
the limiting assembly and the connecting assembly are arranged on the same vertical plane at different heights and used for limiting the movement of the end face positioning assembly corresponding to the limiting assembly and enabling the end face positioning assembly to slide along the length direction of the limiting assembly;
and one end of the connecting assembly, which is far away from the rotating disc, is connected with the end face positioning assembly, and the rotating disc rotates to enable the two end face positioning assemblies to be close to each other through the connecting assembly so as to position the wing body.
As an optimal technical scheme of the utility model, drive assembly includes cylinder, cylinder block and joint bearing, the tip of the piston rod of cylinder passes through joint bearing with the avris of rotary disk links to each other, the tip of the cylinder body of cylinder with the cylinder block is articulated.
As a preferred technical scheme of the utility model, coupling assembling includes that the hexagonal is turned over tooth bolt and fisheye connects, the both ends of the hexagonal is turned over tooth bolt with the fisheye connects continuously.
As an optimal technical scheme of the utility model, spacing subassembly includes mounting panel and slider, the slider is located one side of mounting panel.
As an optimal technical scheme of the utility model, the terminal surface locating component includes slip unit and centre gripping unit, the centre gripping unit is located the slip unit is kept away from the one end of rotary disk.
As a preferred technical scheme of the utility model, the slip unit includes guide rail and guide rail seat, the guide rail seat is located the guide rail is close to the one end of rotary disk.
As the utility model discloses a preferred technical scheme, the centre gripping unit includes support frame and locating pin, the locating pin is located the support frame upper end is close to the carousel side.
As an optimal technical scheme of the utility model, in set up the adjustment tank of a vertical direction on the support frame, locating pin sliding connection in on the adjustment tank.
As a preferred technical scheme of the utility model, the locating pin with the support frame is detachable to be connected.
As an optimized technical scheme of the utility model, seted up one on the support frame with guide rail longitudinal section assorted mounting groove.
Compared with the prior art, the utility model has following beneficial effect:
can control the fixed subassembly of terminal surface of two relative settings through the single cylinder to the location process of unmanned aerial vehicle wing body, the drive mode of single cylinder for this positioning mechanism carries out quick location to unmanned aerial vehicle wing body, thereby satisfies the rapid Assembly and the interchangeability requirement of product, improves the efficiency in the technology course of working.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:
fig. 1 is one of the overall structural schematic diagrams of the present invention;
fig. 2 is a second schematic view of the overall structure of the present invention;
fig. 3 is a specific usage state diagram of the present invention;
in the figure: 1. rotating the disc; 2. a rotating shaft; 3. a drive assembly; 31. a cylinder; 32. a cylinder block; 33. a knuckle bearing; 4. a connection assembly; 41. a hexagonal inverted-tooth bolt; 42. a fisheye joint; 5. a sliding unit; 51. a guide rail; 52. a guide rail seat; 6. a limiting component; 61. mounting a plate; 62. a slider; 7. a clamping unit; 71. a support frame; 710. mounting grooves; 711. an adjustment groove; 72. and positioning pins.
Detailed Description
It should be noted that, in the description of the present invention, the terms "lateral", "longitudinal", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, which is only for the convenience of description and simplification of description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.
As shown in fig. 1-3, the utility model provides a self-discharging single cylinder positioning mechanism, which comprises a rotating disk 1, a rotating shaft 2, a driving component 3, two groups of connecting components 4, a limiting component 6 corresponding to the connecting components 4 and an end surface positioning component corresponding to the limiting component 6;
the rotating shaft 2 coaxially penetrates through the rotating disc 1 along the vertical direction and is connected with the rotating disc in a rotating mode;
the driving component 3 is in transmission connection with the rotating disc 1 and drives the rotating disc 1 to rotate around the rotating shaft 2;
the two groups of connecting components 4 are oppositely arranged on the periphery of the rotating disc 1 and are respectively in transmission connection with the rotating disc 1;
the limiting component 6 and the connecting component 4 are arranged on the same vertical plane with different heights, and the limiting component 6 is used for limiting the movement of the end face positioning component corresponding to the limiting component and enabling the end face positioning component to slide along the length direction of the limiting component 6;
the end, far away from the rotating disc 1, of the connecting assembly 4 is connected with the end face positioning assembly, and the rotating disc 1 rotates to enable the two end face positioning assemblies to be close to each other through the connecting assembly 4 so as to position the wing body.
The specific working process is as follows:
referring to the structure shown in fig. 3, after the wing body is placed, the driving assembly 3 is started to work, the piston rod of the driving assembly 3 extends out to drive the rotating disk 1 to rotate around the axis of the rotating shaft 2, because the connecting assembly 4 is fixed at a certain position on the rotating disk 1, in the process that the rotating disk 1 starts to rotate, the rotating disk 1, the connecting assembly 4 and the end face positioning assembly form a crank-slider structure, the connecting assembly 4 is equivalent to a crank in the motion process, the end face positioning assembly serves as a 'slider' in the crank-slider structure, the extending process of the rotating shaft 2 drives the two end face positioning assemblies to be away from each other (the wing body is put down), the retracting process of the rotating shaft 2 drives the two end face positioning assemblies to be close to each other (the wing body is clamped).
Two relative end face positioning components that set up under 1's drive effect, can guarantee the synchronization degree of the two.
Further, the driving assembly 3 comprises a cylinder 31, a cylinder seat 32 and a joint bearing 33, wherein the end of the piston rod of the cylinder 31 is connected with the side of the rotating disc 1 through the joint bearing 33, and the end of the cylinder body of the cylinder 31 is hinged with the cylinder seat 32.
In a specific structural embodiment of the driving assembly 3, the structure of the driving assembly 3 is composed of three parts, namely a cylinder 31, a cylinder seat 32 and a joint bearing 33, wherein the cylinder body end of the cylinder 31 is hinged to the cylinder seat 32, and the piston rod end of the cylinder 31 is connected with the rotating disc 1 through the joint bearing 33, so that the rotating disc 1 is driven to rotate during the retraction/extension process of the piston rod of the cylinder 31, and the subsequent clamping and positioning processes are performed on the wing body.
The connecting assembly 4 comprises a hexagonal reverse threaded bolt 41 and a fisheye joint 42, and both ends of the hexagonal reverse threaded bolt 41 are connected with the fisheye joint 42.
In a specific structural embodiment of the connecting assembly 4, the connecting assembly 4 is composed of two parts, namely a hexagonal reversed-tooth bolt 41 and a fisheye joint 42, wherein both ends of the hexagonal reversed-tooth bolt 41 are provided with threaded ends, and the threaded ends are connected with the fisheye joint 42.
Spacing subassembly 6 includes mounting panel 61 and slider 62, and one side of mounting panel 61 is located to slider 62.
The end face positioning assembly comprises a sliding unit 5 and a clamping unit 7, and the clamping unit 7 is arranged at one end, far away from the rotating disc 1, of the sliding unit 5.
The slide unit 5 includes a guide rail 51 and a rail housing 52, and the rail housing 52 is provided at one end of the guide rail 51 near the rotating disk 1.
The clamping unit 7 comprises a supporting frame 71 and a positioning pin 72, wherein the positioning pin 72 is arranged at the upper end of the supporting frame 71 close to the side of the rotating disk 1.
In an embodiment as a specific structure of the clamping unit 7, the clamping unit 7 is composed of two parts, namely a supporting frame 71 and a positioning pin 72, the positioning pin 72 is arranged at the upper end of the supporting frame 71, and when the supporting frame 71 moves in the process of rotating the rotating disk 1, the positioning pin 72 will finally clamp the wing body.
A vertical adjusting groove 711 is formed in the supporting frame 71, and the positioning pin 72 is slidably connected to the adjusting groove 711.
As an embodiment of a connection manner of the support frame 71 and the positioning pin 72, in this embodiment, the positioning pin 72 is slidably disposed on the support frame 71, and the sliding connection of the positioning pin 72 is realized through the adjusting groove 711 on the support frame 71, so that the wing body positioning holes with different heights can be well adjusted.
The positioning pin 72 is detachably connected with the supporting frame 71.
In an embodiment of the connection manner of the support frame 71 and the positioning pin 72, in this embodiment, the positioning pin 72 and the support frame 71 are detachably connected, and in the actual production process, the size of the positioning pin 72 is preferably changed according to the size of the positioning hole of the wing body.
The supporting frame 71 is provided with an installation groove 710 matched with the longitudinal section of the guide rail 51.
In an embodiment of the structure of the supporting frame 71, the lower end of the supporting frame 71 is further provided with an installation groove 710 matched with the guide rail 51, the guide rail 51 passes through the installation groove 710, and the guide rail 51 is installed in the installation groove 710 through a screw, so that the position of the supporting frame 71 and the position of the guide rail 51 are fixed.
This press from both sides tight positioning mechanism can control the fixed subassembly of terminal surface of two relative settings to the location process of unmanned aerial vehicle wing body through the single cylinder, the drive mode of single cylinder for this positioning mechanism carries out quick location to unmanned aerial vehicle wing body, thereby satisfies the rapid Assembly and the interchangeability requirement of product, improves the efficiency in the technology course of working.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (10)
1. The utility model provides a self-discharging formula list cylinder positioning mechanism which characterized in that: the device comprises a rotating disk (1) in the horizontal direction, a rotating shaft (2), a driving assembly (3), two groups of connecting assemblies (4), a limiting assembly (6) corresponding to the connecting assemblies (4) and an end face positioning assembly corresponding to the limiting assembly (6);
the rotating shaft (2) coaxially penetrates through the rotating disc (1) along the vertical direction and is connected with the rotating disc in a rotating mode;
the driving assembly (3) is in transmission connection with the rotating disc (1) and drives the rotating disc (1) to rotate around the rotating shaft (2);
the two groups of connecting components (4) are oppositely arranged on the periphery of the rotating disc (1) and are respectively in transmission connection with the rotating disc (1);
the limiting assembly (6) and the connecting assembly (4) are arranged on the same vertical plane at different heights, and the limiting assembly (6) is used for limiting the movement of the end face positioning assembly corresponding to the limiting assembly and enabling the end face positioning assembly to slide along the length direction of the limiting assembly (6);
one end, far away from the rotating disc (1), of the connecting assembly (4) is connected with the end face positioning assembly, and the rotating disc (1) rotates to enable the two end face positioning assemblies to be close to each other through the connecting assembly (4) so as to position the wing body.
2. The self-dumping single cylinder positioning mechanism according to claim 1, wherein: the driving assembly (3) comprises an air cylinder (31), an air cylinder seat (32) and a joint bearing (33), the end of a piston rod of the air cylinder (31) is connected with the side of the rotating disc (1) through the joint bearing (33), and the end of a cylinder body of the air cylinder (31) is hinged with the air cylinder seat (32).
3. The self-dumping single-cylinder positioning mechanism according to claim 1, wherein: the connecting assembly (4) comprises a hexagonal reverse-tooth bolt (41) and a fisheye joint (42), and two ends of the hexagonal reverse-tooth bolt (41) are connected with the fisheye joint (42).
4. The self-dumping single cylinder positioning mechanism according to claim 1, wherein: spacing subassembly (6) include mounting panel (61) and slider (62), slider (62) are located one side of mounting panel (61).
5. The self-dumping single cylinder positioning mechanism according to any one of claims 1 to 4, wherein: the end face positioning assembly comprises a sliding unit (5) and a clamping unit (7), wherein the clamping unit (7) is arranged at one end, far away from the rotating disc (1), of the sliding unit (5).
6. The self-dumping single cylinder positioning mechanism according to claim 5, wherein: the sliding unit (5) comprises a guide rail (51) and a guide rail seat (52), wherein the guide rail seat (52) is arranged at one end, close to the rotating disc (1), of the guide rail (51).
7. The self-dumping single cylinder positioning mechanism according to claim 6, wherein: the clamping unit (7) comprises a supporting frame (71) and a positioning pin (72), wherein the positioning pin (72) is arranged at the upper end of the supporting frame (71) close to the side of the rotating disc (1).
8. The self-dumping single cylinder positioning mechanism of claim 7, wherein: a vertical adjusting groove (711) is formed in the supporting frame (71), and the positioning pin (72) is connected to the adjusting groove (711) in a sliding mode.
9. The self-dumping single cylinder positioning mechanism of claim 7, wherein: the positioning pin (72) is detachably connected with the supporting frame (71).
10. The self-dumping single cylinder positioning mechanism according to any one of claims 7 to 9, wherein: the supporting frame (71) is provided with an installation groove (710) matched with the longitudinal section of the guide rail (51).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220376118.4U CN217345152U (en) | 2022-02-24 | 2022-02-24 | Self-discharging formula list cylinder positioning mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220376118.4U CN217345152U (en) | 2022-02-24 | 2022-02-24 | Self-discharging formula list cylinder positioning mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217345152U true CN217345152U (en) | 2022-09-02 |
Family
ID=83047268
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220376118.4U Active CN217345152U (en) | 2022-02-24 | 2022-02-24 | Self-discharging formula list cylinder positioning mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217345152U (en) |
-
2022
- 2022-02-24 CN CN202220376118.4U patent/CN217345152U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205989169U (en) | A kind of automobile axle leaf spring assemble mechanism | |
| CN210524383U (en) | Automatic fastening harness of screwing up of cabin cover | |
| CN217345152U (en) | Self-discharging formula list cylinder positioning mechanism | |
| CN109434357A (en) | A kind of spot welding ring flange tooling for axle shell | |
| CN210678528U (en) | Electric pre-tightening device for triangular arm of passenger car | |
| CN217345402U (en) | Controllable multi-angle positioning platform of single cylinder | |
| CN210552419U (en) | Shaping jig for automotive interior trim panel | |
| CN215239126U (en) | Automatic tightening device for hydraulic oil cylinder guide sleeve | |
| CN217345243U (en) | Single cylinder linkage rocking rod subassembly anchor clamps | |
| CN208992060U (en) | Trailer axle positioning device for welding | |
| CN112428232A (en) | Sealing ring press-connection machine | |
| CN220243414U (en) | Assembling and transferring carrier for automobile door | |
| CN219444322U (en) | Positioning device for machining automobile parts | |
| CN219925070U (en) | Intelligent continuous truss welding structure | |
| CN215788011U (en) | Automatic upper and lower cover assembling riveting machine | |
| CN219599185U (en) | Motor frock positioning mechanism | |
| CN215586874U (en) | Rotatable processing tool | |
| CN220739961U (en) | Positioning device for automobile part production | |
| CN115106227B (en) | Series-parallel mechanism for coating automobile bumper | |
| CN219521741U (en) | Auxiliary fixing equipment easy to adjust and used for processing piston rod | |
| CN218364288U (en) | Automobile parts fixture | |
| CN218344983U (en) | Vehicle body lifting appliance wheel base adjusting device | |
| CN214642732U (en) | Pneumatic electrode cap grinding device | |
| CN219074983U (en) | Workpiece clamping rotating head | |
| CN210592229U (en) | Auxiliary clamp for integral assembly of automobile front-end module |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |