Novel unmanned aerial vehicle device for geological exploration

Abstract

A novel unmanned aerial vehicle device for geological exploration comprises an unmanned aerial vehicle body, an inclination angle adjusting ring, a cleaning liquid storage tank, a driving air pump, a storage tank connecting cover, an inclination angle adjusting motor, an inclination angle adjusting screw rod, an air supply hose, a gas ejector, a hose transition connecting block, a transition connecting pipe, a driving water pump, a rear liquid supply pipe and a front liquid supply pipe. The bottom of the unmanned aerial vehicle body is provided with a surveying camera and a rock cleaning nozzle, the rock cleaning nozzle is located on the upper portion of the surveying camera, the bottom of the unmanned aerial vehicle body is fixedly connected with a cleaning liquid storage tank, the cleaning liquid storage tank is located on the side opposite to a lens of the surveying camera, and the bottom of the cleaning liquid storage tank is provided with a connecting cover mounting table. The connecting cover mounting table is matched with the storage box connecting cover, the connecting cover mounting table is connected with the storage box connecting cover, and the storage box connecting cover sleeves the outer side of the connecting cover mounting table.

Description

Technical Field

[0001] The utility model relates to the field of geological exploration, in particular to a new type of unmanned aerial vehicle device for geological exploration. Background Art

[0002] The existing patent (publication number: CN219590188U) proposes a new type of unmanned aerial vehicle device for geological exploration, including an unmanned aerial vehicle body, a camera probe, an installation mechanism, including a cleaning component arranged below the unmanned aerial vehicle body. The cleaning component includes a water tank, an installation pipe, a docking pipe and a high-pressure cleaning head. The adjusting mechanism includes an installation plate arranged on one side surface of the water tank. When the unmanned aerial vehicle body uses the camera probe to take pictures and samples of the rock surface attached with sediment and dust, at this time, the staff uses a remote control device to drive a pump. However, for this device, "the cleaning liquid in the water tank is sent to the high-pressure cleaning head, and then the high-pressure cleaning head is used to clean the dust and soil on the rock surface". The water splashed when the high-pressure cleaning head cleans the rock surface may splash on the lens surface of the probe, affecting the survey effect of this device. Summary of the Invention

[0003] In view of the above deficiencies of the prior art, the utility model provides a new type of unmanned aerial vehicle device for geological exploration. The inclination angle adjusting motor drives the inclination angle adjusting screw to rotate to control the movement of the inclination angle adjusting ring, so as to control the inclination angle of the gas injector through the inclination angle traction slider, thereby changing the angle of the gas ejected by the gas injector. At the same time, through the annular arrangement of the gas injectors, the cleaning range of the gas is increased, avoiding the sewage for cleaning the rock from polluting the lens and affecting the survey, and ensuring the survey effect of this device.

[0004] The purpose of the utility model is realized through the following technical solutions:

[0005] A new type of unmanned aerial vehicle (UAV) device for geological exploration, comprising a UAV main body, an inclination adjustment ring, a cleaning liquid storage tank, a driving air pump, a storage tank connection cover, an inclination adjustment motor, an inclination adjustment screw, a gas supply hose, a gas injector, a hose transition connection block, a transition connection pipe, a driving water pump, a rear liquid supply pipe, and a front liquid supply pipe. The bottom of the UAV main body is provided with a survey camera and a rock cleaning nozzle. The rock cleaning nozzle is located above the survey camera. The bottom of the UAV main body is fixedly connected to the cleaning liquid storage tank, and the cleaning liquid storage tank is located on the side opposite to the lens of the survey camera. The bottom of the cleaning liquid storage tank has a connection cover mounting platform, which is adapted to the storage tank connection cover. The connection cover mounting platform is connected to the storage tank connection cover, and the storage tank connection cover is sleeved outside the connection cover mounting platform. The bottom of the UAV main body is fixedly connected to the driving air pump and the driving water pump. The driving air pump and the driving water pump are both located on the side of the cleaning liquid storage tank close to the survey camera. The driving air pump is in the middle position, and the driving water pumps are distributed on both sides of the driving air pump. The driving water pump is connected to the cleaning liquid storage tank through the rear liquid supply pipe, and the rock cleaning nozzle is connected to the driving water pump through the front liquid supply pipe. A hose transition connection block is fixedly connected to the side of the survey camera facing the driving air pump, and the hose transition connection block is connected to the driving air pump through the transition connection pipe. The survey camera is adapted to the inclination adjustment ring, and the survey camera is connected to the inclination adjustment ring. The inclination adjustment ring slides outside the survey camera, and one side of the inclination adjustment ring has an inclination traction slide bar.

[0006] One side of the inclination traction slide bar has an inclination traction slider. The side of the survey camera has a traction rod connection platform. Multiple groups of traction rod connection platforms are evenly arranged around the survey camera. The end of the traction rod connection platform has a traction rod connection groove, which is adapted to the inclination traction slide bar. The traction rod connection groove is connected to the inclination traction slide bar, and the inclination traction slide bar slides inside the traction rod connection groove. One side of the survey camera has a fixed rotation connection platform, and one side of the gas injector has a cleaning liquid nozzle.

[0007] Beneficial effects: 1. When the present utility model conducts geological exploration operations, the rock is cleaned through the rock cleaning nozzle. When sewage splashes on the lens of the survey camera during the cleaning process, the driving air pump presses air into the transition connection pipe. Finally, the gas is ejected from the gas injector surrounding the side of the survey camera through the transition connection pipe, the hose transition connection block, and the gas supply hose to clean the lens of the survey camera. The inclination adjustment motor drives the inclination adjustment screw to rotate to control the movement of the inclination adjustment ring, thereby controlling the inclination angle of the gas injector through the traction of the inclination traction slider, so as to change the angle of the gas ejected by the gas injector. At the same time, through the annular arrangement of the gas injectors, the cleaning range of the gas is increased, avoiding the sewage from cleaning the rock from contaminating the lens and affecting the survey, and ensuring the survey effect of this device.

[0008] 2. The survey camera, driving air pump, driving water pump, and cleaning liquid storage tank of the present utility model are arranged in a straight line, thereby reducing the overall cross-sectional area of this device during forward flight, decreasing the flight air resistance of this device, and increasing the flight speed and endurance of this device.

[0009] 3. The air supply hose of the present utility model is positioned by a hose positioning platform, ensuring that the air supply hose does not move randomly during the flight of this device, avoiding the soft air supply hose from breaking due to random movement under the influence of air flow during the flight of this device, and ensuring the safety of the air supply hose during flight.

[0010] 4. The inclination adjustment screw groove and the adjustment screw of the present utility model are connected by threads. Threaded connection has good self-locking property, making it difficult for the inclination adjustment screw to be affected by external forces when driving the inclination adjustment ring to move, and ensuring the accuracy and stability when the gas injector changes the inclination. Description of the Drawings

[0011] Figure 1 It is a schematic structural diagram of the novel unmanned aerial vehicle device for geological exploration described in the present utility model.

[0012] Figure 2 It is a side view of the novel unmanned aerial vehicle device for geological exploration described in the present utility model.

[0013] Figure 3 For the present utility model Figure 2 Partial enlarged view A.

[0014] Figure 4 For the present utility model Figure 2 Partial enlarged view B.

[0015] Figure 5 It is a partial structural diagram of the novel unmanned aerial vehicle device for geological exploration described in the present utility model.

[0016] Figure 6 It is a schematic structural diagram of the inclination adjustment ring described in the present utility model.

[0017] Figure 7 It is a schematic structural diagram of the gas injector described in the present utility model. Detailed Description of the Preferred Embodiment

[0018] The present utility model will be further described in detail below with reference to the drawings and embodiments:

[0019] Embodiment 1:

[0020] A new type of unmanned aerial vehicle (UAV) device for geological exploration, including a UAV main body 1, an inclination adjustment ring 3, a cleaning liquid storage tank 4, a driving air pump 5, a storage tank connection cover 6, an inclination adjustment motor 7, an inclination adjustment screw 8, a gas supply hose 10, a gas injector 19, a hose transition connection block 24, a transition connection pipe 25, a driving water pump 26, a rear liquid supply pipe 27, and a front liquid supply pipe 28. The bottom of the UAV main body 1 is provided with a survey camera 2 and a rock cleaning nozzle 29. The rock cleaning nozzle 29 is located above the survey camera 2. During geological exploration operations, the rock is cleaned through the rock cleaning nozzle 29. When sewage splashes on the lens of the survey camera 2 during the cleaning process, the driving air pump 5 presses air into the interior of the transition connection pipe 25. Finally, the gas passes through the transition connection pipe 25, the hose transition connection block 24, and the gas supply hose 10, and is finally ejected from the gas injector 19 surrounding the side of the survey camera 2 to clean the lens of the survey camera 2. The inclination adjustment motor 7 drives the inclination adjustment screw 8 to rotate to control the movement of the inclination adjustment ring 3, thereby controlling the inclination angle of the gas injector 19 through the inclination traction slider 18, so as to change the angle of the gas ejected by the gas injector 19. At the same time, through the annular arrangement of the gas injector 19, the cleaning range of the gas is increased, avoiding the sewage from cleaning the rock from polluting the lens and affecting the survey, and ensuring the survey effect of this device. The bottom of the UAV main body 1 is fixedly connected with a cleaning liquid storage tank 4. The cleaning liquid storage tank 4 is located on the side opposite to the lens of the survey camera 2. The bottom of the cleaning liquid storage tank 4 has a connection cover mounting table 14, which is adapted to the storage tank connection cover 6. The connection cover mounting table 14 is connected to the storage tank connection cover 6, and the storage tank connection cover 6 is sleeved outside the connection cover mounting table 14. The bottom of the UAV main body 1 is fixedly connected with a driving air pump 5 and a driving water pump 26. The driving air pump 5 and the driving water pump 26 are both located on the side of the cleaning liquid storage tank 4 close to the survey camera 2. The driving air pump 5 is in the middle position, and the driving water pumps 26 are distributed on both sides of the driving air pump 5. The driving water pump 26 is connected to the cleaning liquid storage tank 4 through the rear liquid supply pipe 27. The rock cleaning nozzle 29 is connected to the driving water pump 26 through the front liquid supply pipe 28. The side of the survey camera 2 facing the driving air pump 5 is fixedly connected with a hose transition connection block 24, and the hose transition connection block 24 is connected to the driving air pump 5 through the transition connection pipe 25. The survey camera 2 is adapted to the inclination adjustment ring 3. The survey camera 2 is connected to the inclination adjustment ring 3, and the inclination adjustment ring 3 slides outside the survey camera 2. The survey camera 2, the driving air pump 5, the driving water pump 26, and the cleaning liquid storage tank 4 are arranged in a straight line, so as to reduce the overall cross-sectional area of this device during forward flight, reduce the flight air resistance of this device, and increase the flight speed and endurance of this device. One side of the inclination adjustment ring 3 has an inclination traction slide bar 17.

[0021] Embodiment 2:

[0022] On one side of the inclination traction slide bar 17 of the present utility model, there is an inclination traction slider 18. On the side of the survey camera 2, there is a traction rod connection platform 15. A plurality of traction rod connection platforms 15 are evenly arranged around the survey camera 2. At the end of the traction rod connection platform 15, there is a traction rod connection groove 16. The traction rod connection groove 16 is adapted to the inclination traction slide bar 17. The traction rod connection groove 16 is connected to the inclination traction slide bar 17. The inclination traction slide bar 17 slides inside the traction rod connection groove 16. On one side of the survey camera 2, there is a fixed rotation connection platform 23. On one side of the gas injector 19, there is a cleaning liquid nozzle 20.

[0023] Embodiment 3:

[0024] On the side of the gas injector 19 of the present utility model, there are a moving rotation connection platform 21 and a traction block connection groove 22. The moving rotation connection platform 21 is in the central position. The traction block connection groove 22 is located on one side of the moving rotation connection platform 21. The moving rotation connection platform 21 is rotationally connected to the fixed rotation connection platform 23. The inclination traction slider 18 is adapted to the traction block connection groove 22. The inclination traction slider 18 is connected to the traction block connection groove 22. The inclination traction slider 18 slides inside the traction block connection groove 22.

[0025] Embodiment 4:

[0026] On the side surface of the inclination adjustment ring 3 of the present utility model, there is a hose positioning platform 9. The hose positioning platform 9 is adapted to the air supply hose 10. The hose positioning platform 9 is connected to the air supply hose 10. The air supply hose 10 slides inside the hose positioning platform 9. One side of the air supply hose 10 is fixedly connected to the gas injector 19. The other side of the air supply hose 10 is fixedly connected to the hose transition connection block 24. The air supply hose 10 is positioned by the hose positioning platform 9, ensuring that the air supply hose 10 will not move randomly during the flight of this device, avoiding the soft air supply hose 10 from breaking due to being affected by the airflow and moving randomly during the flight of this device, and ensuring the safety of the air supply hose 10 during the flight process.

[0027] Embodiment 5:

[0028] At the bottom of the inclination adjustment ring 3 of the present utility model, there is a screw rod connection platform 13. Inside the screw rod connection platform 13, there is an inclination adjustment screw groove 12. The bottom of the survey camera 2 is fixedly connected to the inclination adjustment motor 7. The transmission shaft of the inclination adjustment motor 7 is fixedly connected to the inclination adjustment screw rod 8. The inclination adjustment screw rod 8 is threadedly connected to the inclination adjustment screw groove 12. The inclination adjustment screw groove 12 and the adjustment screw rod 8 adopt a threaded connection. The threaded connection has good self-locking property, making it difficult for the inclination adjustment screw rod 8 to be affected by external forces when driving the inclination adjustment ring 3 to move, ensuring the accuracy and stability of the inclination change of the gas injector 19.

[0029] Embodiment 6:

[0030] Installation steps of the utility model: Fix the cleaning liquid storage tank 4 and the driving air pump 5 at the bottom of the UAV body 1, fixedly connect the cleaning liquid storage tank 4 and the driving air pump 5, fixedly connect the rear part of the survey camera 2 with the hose transition block 24, connect the hose transition block 24 and the driving air pump 5 through the transition connecting pipe 25, sleeved the inclination adjustment ring 3 on the outside of the survey camera 2, fixedly connect the bottom of the survey camera 2 with the inclination adjustment motor 7, fixedly connect the transmission shaft of the inclination adjustment motor 7 with the inclination adjustment screw rod 8, threadedly connect the inclination adjustment screw groove 12 of the inclination adjustment ring 3 with the inclination adjustment screw rod 8, rotatably connect the moving rotating connection table 21 of the gas injector 19 with the fixed rotating connection table 23 of the survey camera 2, insert the inclination traction slide bar 17 of the inclination adjustment ring 3 into the traction bar connection groove 16 of the survey camera 2, insert the inclination traction slider 18 of the inclination traction slide bar 17 into the traction block connection groove 22 of the gas injector 19, insert the air supply hose 10 into the hose positioning table 9 of the inclination adjustment ring 3, fixedly connect one side of the air supply hose 10 with the gas injector 19, and fixedly connect the other side of the air supply hose 10 with the hose transition block 24. The installation of this device is completed.

[0031] The above are only the preferred embodiments of the utility model and are not used to limit the utility model. It should be pointed out that for those of ordinary skill in the art in this technical field, without departing from the technical principle of the utility model, several improvements and modifications can be made, and these improvements and modifications should also be regarded as the protection scope of the utility model.

Claims

1. A new type of UAV device for geological exploration, characterized by The invention comprises an unmanned aerial vehicle (UAV) body (1), an inclination adjustment ring (3), a cleaning liquid storage tank (4), a driving air pump (5), a storage tank connection cover (6), an inclination adjustment motor (7), an inclination adjustment screw (8), an air supply hose (10), a gas injector (19), a hose transition connection block (24), a transition connection pipe (25), a driving water pump (26), a rear liquid supply pipe (27), and a front liquid supply pipe (28). The bottom of the UAV body (1) is provided with a survey camera (2) and a rock cleaning nozzle (29), the rock cleaning nozzle (29) being located on the upper part of the survey camera (2). The bottom of the UAV body (1) is fixedly connected to the cleaning liquid storage tank (4), the cleaning liquid storage tank (4) being located on the side opposite to the lens of the survey camera (2), the bottom of the cleaning liquid storage tank (4) is provided with a connection cover mounting platform (14), the connection cover mounting platform (14) is adapted to the storage tank connection cover (6), the connection cover mounting platform (14) is connected to the storage tank connection cover (6), and the storage tank connection cover (6) is sleeved on the connection cover mounting platform (14). ), the bottom of the drone body (1) is fixedly connected to a driving air pump (5) and a driving water pump (26), the driving air pump (5) and the driving water pump (26) are both located on the side of the cleaning liquid storage tank (4) close to the survey camera (2), the driving air pump (5) is in the center, the driving water pump (26) is distributed on both sides of the driving air pump (5), the driving water pump (26) and the cleaning liquid storage tank (4) are connected through a rear liquid supply pipe (27), and the rock cleaning nozzle (29) and the driving water pump (26) are connected through a rear liquid supply pipe (27). The survey camera (2) is connected through a front liquid supply pipe (28), and a side of the survey camera (2) facing the driving air pump (5) is fixedly connected to a hose transition connection block (24). The hose transition connection block (24) and the driving air pump (5) are connected through a transition connection pipe (25). The survey camera (2) is adapted to the inclination adjustment ring (3), and the survey camera (2) is connected to the inclination adjustment ring (3). The inclination adjustment ring (3) slides on the outside of the survey camera (2), and one side of the inclination adjustment ring (3) has an inclination traction slide bar (17).

2. The novel unmanned aerial vehicle device for geological survey according to claim 1 is characterized in that The tilt traction slide bar (17) has a tilt traction slider (18) on one side, the survey camera (2) has a traction rod connection platform (15) on the side, multiple groups of traction rod connection platforms (15) are evenly arranged around the survey camera (2), the end of the traction rod connection platform (15) has a traction rod connection groove (16), the traction rod connection groove (16) is adapted to the tilt traction slide bar (17), the traction rod connection groove (16) is connected to the tilt traction slide bar (17), the tilt traction slide bar (17) slides inside the traction rod connection groove (16), the survey camera (2) has a fixed rotation connection platform (23) on one side, and the gas injector (19) has a cleaning liquid nozzle (20) on one side.

3. The novel geological survey drone device according to claim 2 is characterized in that The gas injector (19) has a movable rotating connection platform (21) and a traction block connection groove (22) on its side. The movable rotating connection platform (21) is located in the center. The traction block connection groove (22) is located on one side of the movable rotating connection platform (21). The movable rotating connection platform (21) is rotatably connected to the fixed rotating connection platform (23). The inclination traction slider (18) is adapted to the traction block connection groove (22). The inclination traction slider (18) is connected to the traction block connection groove (22). The inclination traction slider (18) slides inside the traction block connection groove (22).

4. The novel geological survey drone device according to claim 1 is characterized in that The side surface of the inclination adjustment ring (3) has a hose positioning platform (9), the hose positioning platform (9) is adapted to the air supply hose (10), the hose positioning platform (9) is connected to the air supply hose (10), the air supply hose (10) slides inside the hose positioning platform (9), one side of the air supply hose (10) is fixedly connected to the gas injector (19), and the other side of the air supply hose (10) is fixedly connected to the hose transition connection block (24).

5. The novel unmanned aerial vehicle device for geological survey according to claim 1 is characterized in that The bottom of the inclination adjustment ring (3) is provided with a screw connection platform (13), the screw connection platform (13) has an inclination adjustment screw groove (12) inside, the bottom of the survey camera (2) is fixedly connected to the inclination adjustment motor (7), the transmission shaft of the inclination adjustment motor (7) is fixedly connected to the inclination adjustment screw (8), and the inclination adjustment screw (8) is threadedly connected to the inclination adjustment screw groove (12).

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