CN220842980U - Unmanned aerial vehicle can multi-angle check out test set - Google Patents
Unmanned aerial vehicle can multi-angle check out test set Download PDFInfo
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- CN220842980U CN220842980U CN202322515956.2U CN202322515956U CN220842980U CN 220842980 U CN220842980 U CN 220842980U CN 202322515956 U CN202322515956 U CN 202322515956U CN 220842980 U CN220842980 U CN 220842980U
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- 238000001514 detection method Methods 0.000 claims abstract description 63
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- 230000033001 locomotion Effects 0.000 abstract description 6
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 230000001276 controlling effect Effects 0.000 description 5
- 230000009286 beneficial effect Effects 0.000 description 3
- 230000002349 favourable effect Effects 0.000 description 3
- 230000001360 synchronised effect Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 2
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Abstract
The utility model discloses unmanned aerial vehicle multi-angle detection equipment, which relates to the technical field of unmanned aerial vehicle production detection equipment and comprises a device main body and an adjusting mechanism arranged on the outer wall of the device main body, wherein the adjusting mechanism comprises a sliding component, an adjusting plate is arranged, when the unmanned aerial vehicle is detected through detection equipment, in order to improve the multi-azimuth detection effect on the top of the unmanned aerial vehicle, the condition of detecting blind areas of the unmanned aerial vehicle is reduced, a control servo motor can be opened, a driving threaded rod is driven to rotate through rotation of a driving belt pulley, the driving threaded rod is driven to rotate, the adjusting plate is driven to slide along the inner wall of a fixed groove, meanwhile, the adjusting servo motor can be opened, the sliding plate is driven to slide along the outer wall of the device through rotation of the driving threaded rod, and under the connection of a connecting groove block, the movement track of an adjusting detection head body is driven to be in a cross shape, so that the multi-azimuth detection effect on the top of the unmanned aerial vehicle is achieved.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle production detection equipment, in particular to unmanned aerial vehicle multi-angle detection equipment.
Background
Unmanned aerial vehicle is abbreviated as "unmanned aerial vehicle", and english abbreviation "UAV", is unmanned aerial vehicle that utilizes radio remote control equipment and self-contained program control device to operate, or by on-vehicle computer totally or intermittently independently, and in unmanned aerial vehicle's production and processing, in order to improve unmanned aerial vehicle's quality in the follow-up use, often detect the operation to unmanned aerial vehicle through check out test set.
But this unmanned aerial vehicle multi-angle check out test set is when using, often comparatively fixed to unmanned aerial vehicle's detection angle, and is not high to unmanned aerial vehicle top and unmanned aerial vehicle lateral wall detection's synchronism, and the condition of blind area appears in easy unmanned aerial vehicle detection reduces the problem to unmanned aerial vehicle detection data precision.
Accordingly, in view of the above, research and improvement are being made to solve the existing structural shortcomings, and a multi-angle detection device for unmanned aerial vehicles is proposed.
Disclosure of utility model
The utility model aims to provide multi-angle detection equipment for an unmanned aerial vehicle, which aims to solve the problem that the synchronism of detection of the top of the unmanned aerial vehicle and the side wall of the unmanned aerial vehicle is not high in the background technology.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the unmanned aerial vehicle multi-angle detection equipment comprises a device main body and an adjusting mechanism arranged on the outer wall of the device main body, wherein the adjusting mechanism comprises a sliding component;
The utility model provides a device, including the device main part, the device main part is connected with the device main part, the slip subassembly includes regulating plate, fixed slot, sliding plate and spread groove piece, unmanned aerial vehicle body has been placed to the outer wall of device main part, the top fixedly connected with control servo motor of device main part, control servo motor's output fixedly connected with and device main part outer wall swivelling joint's drive pulley, drive pulley's rotation center is through pivot fixedly connected with and device main part outer wall swivelling joint's drive threaded rod, drive threaded rod's outer wall threaded connection has the regulating plate, the fixed slot has been seted up to the junction of device main part's outer wall and regulating plate, the top swivelling joint of device main part has the control threaded rod, the one end fixedly connected with of control threaded rod adjusts servo motor, control threaded rod's outer wall threaded connection has the sliding plate with device main part outer wall swivelling joint, the outer wall swivelling joint of sliding plate has the spread groove piece with regulating plate outer wall fixed connection.
Further, the one end of drive belt pulley is through pivot fixedly connected with and device main part outer wall swivelling joint's connection belt pulley, the one end of connection belt pulley is through pivot fixedly connected with and device main part outer wall swivelling joint's connection threaded rod, the outer wall threaded connection of connection threaded rod has the reciprocal head body that detects that is located unmanned aerial vehicle body one side, the spout has been seted up with the junction of reciprocal head body to the outer wall of device main part, the outer wall fixedly connected with of spread groove piece is located the regulation of unmanned aerial vehicle body top and detects the head body.
Further, the driving threaded rod forms a rotating structure through controlling the servo motor and the driving belt pulley.
Further, the adjusting plate forms a sliding structure between the driving threaded rod and the fixed groove.
Further, the sliding plate forms a sliding structure with the device main body through the control threaded rod.
Furthermore, the connecting groove blocks form a reciprocating sliding structure through the adjusting plate and the sliding plate, and the outline of the outer wall of the connecting part of the adjusting plate and the sliding plate is in a cross shape.
Further, the connection threaded rod forms a rotating structure through between the driving belt pulley and the connection belt pulley, the connection threaded rod is provided with two groups, and the position distribution of the two groups of connection threaded rods is symmetrical with respect to the central shaft of the connection belt pulley.
Furthermore, the reciprocating detection head body forms a reciprocating sliding structure with the unmanned aerial vehicle body through a connecting threaded rod and a sliding groove.
Compared with the prior art, the utility model has the beneficial effects that:
1. According to the utility model, through the arrangement of the adjusting plate, when the unmanned aerial vehicle is detected through the detection equipment, in order to improve the multi-azimuth detection effect on the top of the unmanned aerial vehicle and reduce the situation of detection blind areas on the unmanned aerial vehicle, the control servo motor can be opened, the driving threaded rod is driven to rotate through the rotation of the driving belt pulley, the threaded rod is driven to rotate, the adjusting plate is driven to slide along the inner wall of the fixed groove, meanwhile, the adjusting servo motor can be opened, the sliding plate is driven to slide along the outer wall of the device through the rotation of the control threaded rod, and the movement track of the adjusting detection head body is driven to be in a cross shape under the connection of the connecting groove blocks, so that the multi-azimuth detection effect on the top of the unmanned aerial vehicle is achieved;
2. According to the utility model, through the arrangement of the connecting threaded rod, when the unmanned aerial vehicle is detected through the detection equipment, in order to improve the effect of synchronously detecting the two sides of the unmanned aerial vehicle, the connecting belt pulley is driven to rotate by the rotation of the driving belt pulley, the connecting belt pulley is driven to slide along the inner wall of the sliding groove by the rotation of the connecting belt pulley through the connection of the connecting threaded rod, so that the synchronous detection motion of the reciprocating detection head body along the two sides of the unmanned aerial vehicle is realized, and the effect of multi-range multi-angle detection of the unmanned aerial vehicle is realized.
Drawings
FIG. 1 is a schematic perspective view of a detection apparatus;
FIG. 2 is a schematic perspective view of another direction of the detecting device;
FIG. 3 is a schematic view of a three-dimensional structure of an adjusting plate and a sliding plate under connection and cooperation;
Fig. 4 is a schematic perspective view of the connection pulley in cooperation with the connection screw.
In the figure: 1. a device body; 11. an unmanned body; 12. adjusting the detection head body; 2. an adjusting mechanism; 21. a sliding assembly; 211. controlling a servo motor; 212. a drive pulley; 213. driving a threaded rod; 214. an adjusting plate; 215. a fixing groove; 216. controlling a threaded rod; 217. adjusting a servo motor; 218. a sliding plate; 219. connecting the groove blocks; 3. connecting a belt pulley; 31. connecting a threaded rod; 32. a reciprocating detection head body; 33. and a sliding groove.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Embodiment one: as shown in fig. 1 to 3, the multi-angle detection device of the unmanned aerial vehicle comprises a device main body 1 and an adjusting mechanism 2 arranged on the outer wall of the device main body 1, wherein the adjusting mechanism 2 comprises a sliding component 21;
the sliding component 21 comprises an adjusting plate 214, a fixing groove 215, a sliding plate 218 and a connecting groove block 219, the unmanned aerial vehicle body 11 is placed on the outer wall of the device main body 1, a control servo motor 211 is fixedly connected to the top of the device main body 1, a driving belt pulley 212 is fixedly connected to the output end of the control servo motor 211 and is rotationally connected with the outer wall of the device main body 1, a driving threaded rod 213 is fixedly connected to the rotation center of the driving belt pulley 212 through a rotating shaft and is rotationally connected with the outer wall of the device main body 1, the adjusting plate 214 is connected with the outer wall of the driving threaded rod 213 in a threaded manner, the fixing groove 215 is formed in the connecting part between the outer wall of the device main body 1 and the adjusting plate 214, a control threaded rod 216 is rotationally connected to the top of the device main body 1, one end of the control threaded rod 216 is fixedly connected with the adjusting servo motor 217, the outer wall of the control threaded rod 216 is rotationally connected with the sliding plate 218 which is rotationally connected with the outer wall of the adjusting plate 214.
Further, the driving threaded rod 213 forms a rotating structure between the control servo motor 211 and the driving pulley 212, which is beneficial to controlling the driving of the servo motor 211 to rotate through the driving pulley 212, so as to drive the driving threaded rod 213 to rotate, thereby realizing the sliding control operation of the adjusting plate 214.
Further, the adjusting plate 214 forms a sliding structure between the driving threaded rod 213 and the fixing groove 215, which is favorable for driving the threaded rod 213 to rotate, and drives the adjusting plate 214 to slide along the inner wall of the fixing groove 215, thereby realizing the control operation of adjusting the position of the connecting groove block 219.
Further, the sliding plate 218 forms a sliding structure between the control threaded rod 216 and the device main body 1, which is favorable for controlling the rotation of the threaded rod 216, and drives the sliding plate 218 to slide along the outer wall of the device main body 1, so as to realize the adjustment movement of the adjustment detection head 12 in the horizontal direction.
Further, the connecting groove block 219 forms a reciprocating sliding structure between the adjusting plate 214 and the sliding plate 218, the outline of the outer wall of the connecting part of the adjusting plate 214 and the sliding plate 218 is in a cross shape, the sliding of the adjusting plate 214 drives the connecting groove block 219 to slide through the connection of the sliding plate 218, and the effect of multi-direction detection on the top of the unmanned aerial vehicle is achieved.
Embodiment two: as shown in fig. 1, fig. 2 and fig. 4, compared with the first embodiment, the multi-angle detection device for the unmanned aerial vehicle according to the present utility model is provided, as another implementation manner of the present utility model, one end of the driving pulley 212 is fixedly connected with the connection pulley 3 rotatably connected to the outer wall of the device main body 1 through a rotating shaft, one end of the connection pulley 3 is fixedly connected with the connection threaded rod 31 rotatably connected to the outer wall of the device main body 1 through a rotating shaft, the outer wall of the connection threaded rod 31 is in threaded connection with the reciprocating detection head 32 located at one side of the unmanned aerial vehicle body 11, a sliding groove 33 is formed at the connection position between the outer wall of the device main body 1 and the reciprocating detection head 32, the outer wall of the connection groove block 219 is fixedly connected with the adjustment detection head 12 located above the unmanned aerial vehicle body 11, and in operation, by providing the connection threaded rod 31 is beneficial to the rotation of the driving pulley 212, the connection pulley 3 through the connection threaded rod 31, the connection threaded connection of the connection pulley 31, the connection pulley 3 drives the reciprocating detection head 32 to slide along the inner wall of the sliding groove 33, and the reciprocating detection head 32 moves along the inner wall of the unmanned aerial vehicle to perform multi-angle detection for detecting the unmanned aerial vehicle.
Further, the connection threaded rod 31 forms a rotating structure through the driving belt pulley 212 and the connection belt pulley 3, the connection threaded rod 31 is provided with two groups, the position distribution of the two groups of connection threaded rods 31 is symmetrical about the central axis of the connection belt pulley 3, the rotation of the driving belt pulley 212 is facilitated, the connection threaded rod 31 is driven to rotate through the connection of the connection belt pulley 3, and the reciprocating sliding control operation of the reciprocating detection head 32 is realized.
Further, the reciprocating detection head 32 forms a reciprocating sliding structure with the unmanned aerial vehicle 11 through the connection threaded rod 31 and the sliding groove 33, is favorable for the rotation of the connection threaded rod 31, and drives the reciprocating detection head 32 to slide along the outer wall of the unmanned aerial vehicle 11 through the connection of the sliding groove 33, so as to achieve the effect of multi-range and multi-angle detection of the unmanned aerial vehicle.
Working principle: when using this unmanned aerial vehicle multi-angle check out test set, first of all, when detecting unmanned aerial vehicle through check out test set, in order to improve the diversified detection effect in unmanned aerial vehicle top, reduce the condition to unmanned aerial vehicle detection blind area, can open control servo motor 211, through the rotation of drive pulley 212, drive threaded rod 213 and rotate, drive threaded rod 213's rotation, drive regulating plate 214 and slide along the inner wall of fixed slot 215, simultaneously, can open and adjust servo motor 217, through the rotation of control threaded rod 216, drive sliding plate 218 and slide along the outer wall of device, and under the connection of spread groove piece 219, the motion trail that the head body 12 was detected in the drive is "ten" font, play the effect that carries out diversified detection to unmanned aerial vehicle top.
Finally, when detecting unmanned aerial vehicle through check out test set, in order to improve the effect to unmanned aerial vehicle both sides synchronous detection, the rotation of drive pulley 212 drives and connects belt pulley 3 and rotate, and the rotation of connecting belt pulley 3 passes through the connection of connecting threaded rod 31, drives to reciprocate the detection head body 32 and slides along the inner wall of spout 33, plays to reciprocate the detection head body 32 and carry out synchronous detection motion along unmanned aerial vehicle's both sides, plays the effect to unmanned aerial vehicle multi-range multi-angle detection.
This is the theory of operation of this unmanned aerial vehicle multi-angle check out test set.
The embodiments of the utility model have been presented for purposes of illustration and description, and are not intended to be exhaustive or limited to the utility model in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art. The embodiments were chosen and described in order to best explain the principles of the utility model and the practical application, and to enable others of ordinary skill in the art to understand the utility model for various embodiments with various modifications as are suited to the particular use contemplated.
Claims (8)
1. The multi-angle detection equipment of the unmanned aerial vehicle comprises a device main body (1) and an adjusting mechanism (2) arranged on the outer wall of the device main body (1), and is characterized in that the adjusting mechanism (2) comprises a sliding component (21);
The utility model provides a device, including slip subassembly (21), including regulating plate (214), fixed slot (215), sliding plate (218) and spread groove piece (219), unmanned aerial vehicle body (11) have been placed to the outer wall of device main part (1), the top fixedly connected with control servo motor (211) of device main part (1), the output fixedly connected with of control servo motor (211) and device main part (1) outer wall swivelling joint's drive pulley (212), the rotation center of drive pulley (212) through pivot fixedly connected with device main part (1) outer wall swivelling joint's drive threaded rod (213), the outer wall threaded connection of drive threaded rod (213) has regulating plate (214), fixed slot (215) have been seted up at the junction of the outer wall of device main part (1) and regulating plate (214), the top swivelling joint of device main part (1) has control servo motor (216), the one end fixedly connected with of control threaded rod (216) adjusts servo motor (217), the outer wall threaded connection of control threaded rod (216) has sliding plate (218) with device main part (1) outer wall swivelling joint's, outer wall threaded connection of sliding plate (218) has regulating plate (219).
2. The unmanned aerial vehicle multi-angle detection device according to claim 1, wherein one end of the driving belt pulley (212) is fixedly connected with a connecting belt pulley (3) rotationally connected with the outer wall of the device main body (1) through a rotating shaft, one end of the connecting belt pulley (3) is fixedly connected with a connecting threaded rod (31) rotationally connected with the outer wall of the device main body (1) through the rotating shaft, the outer wall of the connecting threaded rod (31) is in threaded connection with a reciprocating detection head body (32) positioned on one side of the unmanned aerial vehicle body (11), a connecting position between the outer wall of the device main body (1) and the reciprocating detection head body (32) is provided with a sliding groove (33), and an adjusting detection head body (12) positioned above the unmanned aerial vehicle body (11) is fixedly connected with the outer wall of the connecting groove block (219).
3. The unmanned aerial vehicle multi-angle detection apparatus according to claim 1, wherein the drive threaded rod (213) is configured to rotate between the drive pulley (212) and the control servo motor (211).
4. The unmanned aerial vehicle multi-angle detection apparatus according to claim 1, wherein the adjustment plate (214) forms a sliding structure between the driving threaded rod (213) and the fixing groove (215).
5. The unmanned aerial vehicle multi-angle detection apparatus according to claim 1, wherein the sliding plate (218) forms a sliding structure with the device body (1) through a control threaded rod (216).
6. The unmanned aerial vehicle multi-angle detection device according to claim 1, wherein the connecting groove block (219) forms a reciprocating sliding structure between the adjusting plate (214) and the sliding plate (218), and the outer wall profile of the connecting part of the adjusting plate (214) and the sliding plate (218) is in a cross shape.
7. The unmanned aerial vehicle multi-angle detection device according to claim 2, wherein the connection threaded rod (31) forms a rotating structure with the connection belt pulley (3) through a driving belt pulley (212), the connection threaded rod (31) is provided with two groups, and the position distribution of the two groups of connection threaded rods (31) is symmetrical with respect to the central axis of the connection belt pulley (3).
8. The unmanned aerial vehicle multi-angle detection device according to claim 2, wherein the reciprocating detection head body (32) forms a reciprocating sliding structure with the unmanned aerial vehicle body (11) through a connecting threaded rod (31) and a sliding groove (33).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322515956.2U CN220842980U (en) | 2023-09-15 | 2023-09-15 | Unmanned aerial vehicle can multi-angle check out test set |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322515956.2U CN220842980U (en) | 2023-09-15 | 2023-09-15 | Unmanned aerial vehicle can multi-angle check out test set |
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| Publication Number | Publication Date |
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| CN220842980U true CN220842980U (en) | 2024-04-26 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322515956.2U Active CN220842980U (en) | 2023-09-15 | 2023-09-15 | Unmanned aerial vehicle can multi-angle check out test set |
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| CN (1) | CN220842980U (en) |
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- 2023-09-15 CN CN202322515956.2U patent/CN220842980U/en active Active
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