Position-adjustable aerial survey phase control target for unmanned aerial vehicle

Abstract

The utility model discloses a position adjustable unmanned aerial vehicle aerial survey phase control target which comprises a control base, two sets of supporting plates are fixedly installed at the bottom of the control base, the front face and the back face of the control base are both connected with installation plates in a sliding mode, and target mechanisms are fixedly installed on the inner walls of the installation plates. Two sets of mounting plates are fixedly mounted on the control seat, magnetic sliding grooves are formed in the opposite faces of the two sets of mounting plates, magnetic attraction blocks are fixedly mounted on the front face and the back face of the control seat, connecting frames are fixedly mounted on the two sides of the control seat, and supporting frames are fixedly mounted on the tops of the connecting frames. The sliding adjustment of the magnetic structure drives the mounting plate and the target mechanism to adjust and control the proper height positions, the magnetic attraction mode of the device, the quick positioning of the connected and slid positions, the quick stabilization of the use of the target mechanism, and the cooperation with the sandwich type external equipment mounting space of the device can greatly improve the operation and use corners of the device.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle (UAV) aerial survey equipment, and in particular to a position-adjustable UAV aerial survey phased-control target. Background Art

[0002] A drone is an unmanned aircraft that is controlled by a radio remote control device and its own program control device. The equipment requires multiple mechanical tests before use. For example, its aerial survey and phased control work requires the use of related target structures. In order to meet more usage needs, this application proposes a new drone aerial survey and phased control target device.

[0003] Patent document CN219532075U discloses a target for placing image control points on an aerial survey drone, "including a mark plate and a supporting assembly for supporting the mark plate, and a fixing assembly arranged at the bottom of the supporting assembly and used to fix the mark plate to the ground, wherein the first end of the supporting assembly is hinged to the mark plate, and the second end is fixedly connected to the fixing assembly; the target for placing image control points on an aerial survey drone also includes a first locking assembly, which is arranged on the supporting assembly and / or the mark plate, and is used to lock the mark plate. The target for placing image control points on an aerial survey drone provided by the utility model has a simple structure, a reasonable design, and can be folded for easy storage and transportation."

[0004] When in use, the above-mentioned device has the characteristics of simple structure, reasonable design, foldability, and easy storage and transportation. However, during use, the setting position of the target is affected by the structure of the device after installation and forming. The installation position is fixed. When used for navigation work, the installation position needs to be appropriately adjusted in height. Therefore, there are still certain shortcomings in the use of the device. Utility Model Content

[0005] The purpose of the utility model is to overcome the deficiencies in the prior art and provide a position-adjustable UAV aerial survey phased control target;

[0006] In order to achieve the above purpose, the utility model provides the following technical solutions:

[0007] It includes a control seat, two groups of support plates are fixedly installed on the bottom of the control seat, the front and back sides of the control seat are slidably connected with mounting plates, the inner walls of the mounting plates are fixedly installed with target mechanisms, the facing surfaces of the two groups of mounting plates are provided with magnetic slide grooves, the front and back sides of the control seat are fixedly installed with magnetic suction blocks, connecting frames are fixedly installed on both sides of the control seat, a supporting frame is fixedly installed on the top of the connecting frame, a positioning plate is fixedly installed on the front end of the supporting frame, and a placement seat is embedded on the top of the control seat.

[0008] As an optional technical solution, both sides of the support plate are rotatably connected to a limiting sleeve, the inner wall of the limiting sleeve is slidably connected to a resistance rod, the bottom of the outer surface of the limiting sleeve is slidably connected to a control bolt, and the control bolt thread passes through the interior of the resistance rod.

[0009] As an optional technical solution, an extrusion plate is fixedly installed at the front end of the control bolt, and an anti-slip layer is provided on the outer surface of the extrusion plate, and the anti-slip layer is in close contact with the inner wall of the limiting sleeve.

[0010] As an optional technical solution, the front and back sides of the support plate are rotatably connected to a bottom plate, and a positioning angle cone is provided through the top of the bottom plate.

[0011] As an optional technical solution, positioning sliders are fixedly installed on both sides of the base plate, and the positioning sliders are slidably connected to the inner wall of the support plate. Limiting bolts are threaded through both sides of the support plate, and the front end of the limiting bolts is threadedly connected to the inner wall of the positioning slider.

[0012] As an optional technical solution, an inclined groove is provided at the bottom of the support plate, and the groove is provided to facilitate the rotation and unfolding of the bottom plate.

[0013] The technical solution provided by the utility model has the following technical effects:

[0014] 1. The utility model provides a position-adjustable UAV aerial survey phased control target. By adopting the setting of a magnetic connection structure on the control seat and the sliding adjustment of the magnetic structure, the mounting plate and the target mechanism are driven to adjust the appropriate height position. The magnetic suction method can quickly locate the position after connection and sliding, and the use of the target mechanism can be quickly and stably used. With its sandwich-type external equipment installation space, the corners of the device operation can be greatly improved.

[0015] 2. The utility model provides a position-adjustable UAV aerial survey phased control target. Through the bottom plate and the limit sleeve structure that are rotated and unfolded on the support plate, a bottom fixed structure can be formed around the support plate to achieve a relatively stable support effect on the bottom. The flexible unfolding and positioning structure setting can greatly improve the convenience of outdoor use of the device, so that the device can be quickly placed and installed. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] In order to more clearly illustrate the specific implementation methods of the present utility or the technical solutions in the prior art, the drawings required for use in the specific implementation methods or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are some implementation methods of the present utility. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.

[0017] Figure 1 It is a structural stereogram of the utility model;

[0018] Figure 2 It is a cross-sectional schematic diagram of the limit sleeve structure of the utility model;

[0019] Figure 3 It is a cross-sectional schematic diagram of the mounting plate structure of the utility model;

[0020] Figure 4 It is a cross-sectional schematic diagram of the bottom plate structure of the utility model;

[0021] Figure 5 It is a schematic cross-sectional view of the positioning slider structure of the utility model.

[0022] In the figure: 1. control seat; 2. support plate; 3. mounting plate; 4. target mechanism; 5. magnetic slide; 6. magnetic suction block; 7. connecting frame; 8. support frame; 9. positioning plate; 10. limit sleeve; 11. resistance rod; 12. control bolt; 13. extrusion plate; 14. anti-slip layer; 15. bottom plate; 16. positioning angle cone; 17. positioning slider; 18. limit bolt; 19. placement seat. DETAILED DESCRIPTION

[0023] See also Figures 1 to 5 , a position-adjustable UAV aerial survey phased-control target;

[0024] It includes a control seat 1, two groups of support plates 2 are fixedly installed at the bottom of the control seat 1, the front and back of the control seat 1 are slidably connected with mounting plates 3, the inner wall of the mounting plate 3 is fixedly installed with a target mechanism 4, the facing surfaces of the two groups of mounting plates 3 are provided with magnetic slide grooves 5, the front and back of the control seat 1 are fixedly installed with magnetic suction blocks 6, both sides of the control seat 1 are fixedly installed with connecting frames 7, the top of the connecting frame 7 is fixedly installed with a supporting frame 8, the front end of the supporting frame 8 is fixedly installed with a positioning plate 9, and the top of the control seat 1 is embedded with a placing seat 19;

[0025] When the device is used for phased control target work in drone aerial survey, the device is placed for use through the support structure composed of the support plate 2 structure at the bottom of the control seat 1, and its mounting plate 3 can be used for the installation of the target mechanism 4, so that it can be used outwardly, and through the magnetic connection between the magnetic block 6 and the magnetic slide 5, the position of the mounting plate 3 can be relatively slid on the control seat 1 through the magnetic sliding of the magnetic block 6, and the magnetic connection relationship can also achieve timely positioning after movement, increasing the flexibility of its adjustment structure, and the spacing space between the placement seat 19 and the positioning plate 9 can be used for the placement of external equipment, and cooperate with the installation structure of the target mechanism 4 to assist in the integrated installation of external equipment required when the device is used.

[0026] Wherein both sides of the support plate 2 are rotatably connected to the limit sleeve 10, the inner wall of the limit sleeve 10 is slidably connected to the contact rod 11, the bottom of the outer surface of the limit sleeve 10 is slidably connected to the control bolt 12, and the control bolt 12 thread penetrates the inside of the contact rod 11, and the front end of the control bolt 12 is fixedly installed with an extrusion plate 13, the outer surface of the extrusion plate 13 is provided with an anti-skid layer 14, and the anti-skid layer 14 is in close contact with the inner wall of the limit sleeve 10;

[0027] By placing and installing the device, the limit sleeve 10 can be rotated and unfolded on the support plate 2, and the resistance rod 11 inside it can be slid to contact the installation ground. The control bolt 12 can be rotated to push the extrusion plate 13 and the anti-skid layer 14, and then make them contact the inner wall of the limit sleeve 10. The anti-skid contact can achieve a stopping effect, and then achieve a positioning effect on the position of the resistance rod 11 after adjustment, which assists in the stable placement of the device.

[0028] The front and back sides of the support plate 2 are both rotatably connected to a bottom plate 15, and a positioning angle cone 16 is provided through the top of the bottom plate 15;

[0029] By rotating and unfolding the bottom plate 15, the bottom plate 15 is plugged into and contacted with the installation ground through the surface positioning cone 16, which can assist in supporting the contact stem 11 and increase the stability of the device when installed outdoors.

[0030] The bottom plate 15 is fixedly provided with positioning slide blocks 17 on both sides, and the positioning slide blocks 17 are slidably connected to the inner wall of the support plate 2. The support plate 2 is threadedly connected with limit bolts 18 on both sides, and the front end of the limit bolts 18 is threadedly connected to the inner wall of the positioning slide blocks 17.

[0031] Through the sliding property of the positioning slider 17, the bottom plate 15 can be slid and retracted after being rotated and closed, so as to facilitate its retraction and deployment. When it is unfolded and used, it can be connected with the positioning slider 17 through the limit bolt 18, and then the position of the unfolded bottom plate 15 can be fixed, so as to facilitate its stable unfolding and supporting work.

[0032] The bottom of the support plate 2 is provided with an inclined groove, and the groove is provided to facilitate the rotation and unfolding of the bottom plate 15;

[0033] The inclined grooves are provided to facilitate the rotation adjustment of the bottom plate 15 structure and avoid interference at the corners during rotation.

[0034] Working principle: When the device is in use, it is supported by the positioning of the bottom plate 15 on the support plate 2 and the auxiliary support in the limit sleeve 10 to achieve stable installation of the device. Then, the target mechanism 4 required for the work can be installed inside the mounting plate 3. The position of the mounting plate 3 and the target mechanism 4 can be flexibly and quickly adjusted through the magnetic adjustment structure to meet the actual work needs. The use of the device provides a wrapped and protected installation position for the installation of external devices, which can greatly assist the device in performing drone aerial survey work.

[0035] It is obvious to those skilled in the art that the present invention is not limited to the details of the exemplary embodiments described above, and that the present invention can be implemented in other specific forms without departing from the spirit or essential features of the present invention. Therefore, the embodiments should be regarded as exemplary and non-restrictive from any point of view, and the scope of the present invention is defined by the appended claims rather than the above description, and it is intended that all changes falling within the meaning and scope of the equivalent elements of the claims be included in the present invention. Any reference numeral in a claim should not be regarded as limiting the claim to which it relates.

Claims

1. A position-adjustable UAV aerial survey phased control target, comprising a control seat (1), characterized in that: Two groups of support plates (2) are fixedly installed at the bottom of the control seat (1), the front and back sides of the control seat (1) are slidably connected with mounting plates (3), the inner wall of the mounting plate (3) is fixedly installed with a target mechanism (4), the facing surfaces of the two groups of mounting plates (3) are provided with magnetic slide grooves (5), the front and back sides of the control seat (1) are fixedly installed with magnetic suction blocks (6), the two sides of the control seat (1) are fixedly installed with connecting frames (7), the top of the connecting frame (7) is fixedly installed with a supporting frame (8), the front end of the supporting frame (8) is fixedly installed with a positioning plate (9), and the top of the control seat (1) is embedded with a placement seat (19).

2. The position-adjustable UAV aerial survey phased control target according to claim 1, characterized in that: Both sides of the support plate (2) are rotatably connected to a limit sleeve (10), the inner wall of the limit sleeve (10) is slidably connected to a resistance rod (11), the bottom of the outer surface of the limit sleeve (10) is slidably connected to a control bolt (12), and the control bolt (12) is threadedly inserted into the interior of the resistance rod (11).

3. The position-adjustable UAV aerial survey phased control target according to claim 2, characterized in that: An extrusion plate (13) is fixedly mounted on the front end of the control bolt (12); an anti-slip layer (14) is provided on the outer surface of the extrusion plate (13), and the anti-slip layer (14) is in close contact with the inner wall of the limiting sleeve (10).

4. The position-adjustable UAV aerial survey phased control target according to claim 1, characterized in that: The front and back sides of the support plate (2) are both rotatably connected to a bottom plate (15), and a positioning angle cone (16) is provided through the top of the bottom plate (15).

5. The position-adjustable UAV aerial survey phased control target according to claim 4, characterized in that: Positioning slide blocks (17) are fixedly mounted on both sides of the base plate (15), and the positioning slide blocks (17) are slidably connected to the inner wall of the support plate (2). Limiting bolts (18) are threadedly penetrated and connected to both sides of the support plate (2), and the front ends of the limiting bolts (18) are threadedly connected to the inner wall of the positioning slide blocks (17).

6. The position-adjustable UAV aerial survey phased control target according to claim 1, characterized in that: The bottom of the support plate (2) is provided with an inclined groove, and the groove is provided to facilitate the rotation and unfolding of the bottom plate (15).

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