Double-unmanned-aerial-vehicle cooperative equipment carrying ground penetrating radar

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and discloses a double unmanned aerial vehicle cooperation device carrying a ground penetrating radar, which comprises a host main body and a slave main body, the top of the host main body and the top of the slave main body are respectively provided with a protective shell, an insertion block is inserted into the protective shell, a shock absorber is fixedly mounted in the insertion block, and the shock absorber is fixedly connected with the host main body and the slave main body. A mounting rod is fixedly mounted at the telescopic end of the shock absorber; during use, the ground penetrating radar receiver and the ground penetrating radar transmitter are used in cooperation, efficient detection of a geologic structure can be achieved, and in the flying process, once an obstacle is touched by mistake, the protective shell can firstly touch the obstacle to protect the host machine body and the slave machine body; and meanwhile, when the buffer plate on the protective shell is subjected to impact force, the buffer plate can extrude the shock absorber through the mounting rod, and the shock absorber can be stressed and contracted to buffer the borne force.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a dual-unmanned aerial vehicle cooperative device equipped with a ground-penetrating radar. Background Art

[0002] Geological radar detection technology is a high-tech geophysical method developed in the past decade. Compared with traditional geophysical methods, it has the advantages of high resolution, light weight, accurate positioning, fast and economical, flexible and convenient. As a new type of observation platform, drones have strong maneuverability, flexible operation, and small detection area restrictions. Therefore, the combination of drones and ground penetrating radar can better play the advantages of both.

[0003] The utility model with the existing announcement number CN218567879U discloses a dual-UAV cooperative device equipped with a ground-penetrating radar, including a host body and a slave body placed at a predetermined interval; wherein the host body and the slave body are both provided with a controller and an information acquisition unit; the host also includes a ground-penetrating radar transmitter, and the slave also includes a ground-penetrating radar receiver, and the ground-penetrating radar receiver is adapted to the ground-penetrating radar transmitter. The utility model combines the UAV with the ground-penetrating radar, is less restricted by the terrain, and can realize detection work under complex terrain conditions.

[0004] In the above technical solution, the inventors found that there are at least the following problems: the UAV is flexible to operate and has a high speed. When encountering an obstacle that cannot be avoided, it is likely to be damaged due to the lack of an anti-collision structure. Therefore, how to design a dual-UAV collaborative device equipped with a ground-penetrating radar has become a problem that we currently need to solve. Utility Model Content

[0005] 1. Technical issues to be solved

[0006] In view of the deficiencies in the prior art, the utility model provides a dual-UAV cooperative device equipped with a ground-penetrating radar to solve the problems mentioned in the above background technology.

[0007] (II) Technical solution

[0008] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a dual-UAV cooperative device equipped with a ground-penetrating radar, comprising a host body and a slave body, the top of each of the host body and the slave body is provided with a protective shell, a plug-in block is plugged into the interior of the protective shell, a shock absorber is fixedly installed inside the plug-in block, a mounting rod is fixedly installed at the telescopic end of the shock absorber, a buffer plate is fixedly installed at one end of the mounting rod, a tension spring is fixedly installed inside the protective shell, a connecting block is fixedly installed on one side of the tension spring, a card block is fixedly installed on one side of the connecting block, and a card slot matched with the card block is provided inside the plug-in block.

[0009] Preferably, a rubber pad is fixedly mounted on the outer side of the buffer plate.

[0010] Preferably, a ground-penetrating radar transmitter is fixedly mounted on the bottom of the host body, and a ground-penetrating radar receiver matched with the ground-penetrating radar transmitter is fixedly mounted on the bottom of the slave body.

[0011] Preferably, sliders are fixedly mounted on opposite sides of the mounting rod, and a sliding groove matched with the slider is provided inside the protective shell.

[0012] Preferably, a hand pull ring is fixedly mounted on a side of the connecting block away from the tension spring.

[0013] Preferably, the bottom of the host body and the slave body are both fixedly mounted with supporting feet, and the bottom of the supporting feet are fixedly mounted with soft cushions.

[0014] (III) Beneficial effects

[0015] The utility model provides a dual-UAV cooperative device equipped with a ground-penetrating radar, which has the following beneficial effects:

[0016] First: When in use, the ground penetrating radar receiver is used in conjunction with the ground penetrating radar transmitter to achieve efficient detection of geological structures. During flight, if an obstacle is accidentally touched, the protective shell can first touch the obstacle to protect the host body and the slave body, preventing the host body and the slave body from directly touching the obstacle. At the same time, when the buffer plate on the protective shell is subjected to impact force, the buffer plate can squeeze the shock absorber through the mounting rod, and the shock absorber can contract under force to buffer the force received.

[0017] Second: When the buffer shock-absorbing assembly is damaged by force, the staff can pull the connecting block to move it through the hand pull ring. The connecting block can drive the tension spring upward to extend and at the same time drive the card block and the card slot on the plug-in block to separate from each other, so that the staff can quickly remove the plug-in block from the protective shell to replace the new shock absorber and buffer plate. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 This is a schematic diagram of the front cross-sectional structure of the utility model;

[0019] Figure 2 This is a schematic diagram of the protective shell structure of the utility model;

[0020] Figure 3 For this utility model Figure 2 Enlarged structural diagram at A in the middle.

[0021] In the figure: 1. Host body; 2. Slave body; 3. Protective shell; 4. Plug block; 5. Shock absorber; 6. Mounting rod; 7. Buffer plate; 8. Tension spring; 9. Connecting block; 10. Card block; 11. Rubber pad; 12. Ground penetrating radar transmitter; 13. Ground penetrating radar receiver; 14. Slider; 15. Hand pull ring; 16. Support foot. DETAILED DESCRIPTION

[0022] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0023] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as a limitation on the present invention.

[0024] In addition, the terms "first" and "second" are used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance or implicitly indicating the number of technical features indicated. Therefore, the features defined as "first" and "second" may explicitly or implicitly include one or more of such features. In the description of the present utility model, "multiple" means two or more, unless otherwise clearly and specifically defined.

[0025] like Figure 1-3 As shown, the utility model provides a technical solution: a dual-UAV cooperative device equipped with a ground-penetrating radar, comprising a host body 1 and a slave body 2, the bottom of the host body 1 and the slave body 2 are fixedly installed with a support foot 16, the bottom of the support foot 16 is fixedly installed with a soft pad, which can play a buffering role during landing.

[0026] Please refer to Figure 2 and Figure 3The top of the host body 1 and the slave body 2 are both provided with a protective shell 3, a plug-in block 4 is plugged into the protective shell 3, a shock absorber 5 is fixedly installed inside the plug-in block 4, a mounting rod 6 is fixedly installed at the telescopic end of the shock absorber 5, and sliders 14 are fixedly installed on the opposite sides of the mounting rod 6. A slide groove adapted to the slider 14 is provided inside the protective shell 3, and the slider 14 and the slide groove can limit the moving range of the mounting rod 6 and make the mounting rod 6 more stable when moving. A buffer plate 7 is fixedly installed at one end of the mounting rod 6, and a rubber pad 11 is fixedly installed on the outer side of the buffer plate 7, and the rubber pad 11 can play the role of elastic protection of the buffer plate 7.

[0027] Please refer to Figure 2 and Figure 3 A tension spring 8 is fixedly installed inside the protective shell 3, a connecting block 9 is fixedly installed on one side of the tension spring 8, a clamping block 10 is fixedly installed on one side of the connecting block 9, and a clamping slot adapted to the clamping block 10 is provided inside the plug-in block 4. A hand pull ring 15 is fixedly installed on the side of the connecting block 9 away from the tension spring 8, and the hand pull ring 15 can facilitate the staff to pull the connecting block 9 to move.

[0028] Please refer to Figure 1 and Figure 2 A ground-penetrating radar transmitter 12 is fixedly installed at the bottom of the host body 1, and a ground-penetrating radar receiver 13 adapted to the ground-penetrating radar transmitter 12 is fixedly installed at the bottom of the slave body 2. The ground-penetrating radar receiver 13 is used in conjunction with the ground-penetrating radar transmitter 12 to achieve efficient detection of geological structures. When working, the ground-penetrating radar transmitter 12 emits electromagnetic wave signals, and after receiving the electromagnetic wave signals emitted back, the ground-penetrating radar receiver 13 sends the data to the staff for analysis through the transmission antenna to complete the geological condition detection of the location.

[0029] The working process of the utility model is as follows: when in use, the ground penetrating radar receiver 13 is used in conjunction with the ground penetrating radar transmitter 12 to achieve efficient detection of geological structures. During flight, once an obstacle is accidentally touched, the protective shell 3 can first touch the obstacle to protect the host body 1 and the slave body 2, thereby preventing the host body 1 and the slave body 2 from directly touching the obstacle. At the same time, when the buffer plate 7 on the protective shell 3 is subjected to impact force, the buffer plate 7 can squeeze the shock absorber 5 through the mounting rod 6, and the shock absorber 5 can shrink under the force to buffer the force received; when the buffer shock absorbing component is damaged by force, the staff can pull the connecting block 9 to move through the hand pull ring 15, and the connecting block 9 can drive the tension spring 8 to extend upward and at the same time drive the card block 10 to separate from the card slot on the plug-in block 4, so that the staff can quickly remove the plug-in block 4 from the protective shell 3 to replace the new shock absorber 5 and buffer plate 7.

[0030] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device.

[0031] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A dual-UAV cooperative device equipped with a ground-penetrating radar, comprising a host body (1) and a slave body (2), characterized in that: A protective shell (3) is provided on the top of the host body (1) and the slave body (2), a plug-in block (4) is plugged into the interior of the protective shell (3), a shock absorber (5) is fixedly installed inside the plug-in block (4), a mounting rod (6) is fixedly installed at the telescopic end of the shock absorber (5), a buffer plate (7) is fixedly installed at one end of the mounting rod (6), a tension spring (8) is fixedly installed inside the protective shell (3), a connecting block (9) is fixedly installed on one side of the tension spring (8), a card block (10) is fixedly installed on one side of the connecting block (9), and a card slot matching the card block (10) is provided inside the plug-in block (4).

2. The dual-UAV cooperative device equipped with a ground-penetrating radar according to claim 1, characterized in that: A rubber pad (11) is fixedly mounted on the outer side surface of the buffer plate (7).

3. The dual-UAV cooperative device equipped with a ground-penetrating radar according to claim 1, characterized in that: A ground-penetrating radar transmitter (12) is fixedly mounted on the bottom of the host body (1), and a ground-penetrating radar receiver (13) adapted to the ground-penetrating radar transmitter (12) is fixedly mounted on the bottom of the slave body (2).

4. The dual-UAV cooperative device equipped with a ground-penetrating radar according to claim 1, characterized in that: Slide blocks (14) are fixedly mounted on opposite sides of the mounting rod (6), and a sliding groove matching the slide blocks (14) is provided inside the protective shell (3).

5. The dual-UAV cooperative device equipped with a ground-penetrating radar according to claim 1, characterized in that: A hand pull ring (15) is fixedly mounted on the side of the connection block (9) away from the tension spring (8).

6. The dual-UAV cooperative device equipped with a ground-penetrating radar according to claim 1, characterized in that: The bottoms of the host body (1) and the slave body (2) are both fixedly mounted with supporting feet (16), and the bottoms of the supporting feet (16) are fixedly mounted with soft pads.

Images