Hyperspectral geological survey device

By designing protective components in hyperspectral geological survey devices, and using protective discs and threaded rod systems to block the ground object spectrometer before the drone lands, the problem of easy damage to the device during landing is solved, and the safe landing of the equipment and the service life are extended.

CN222780594UActive Publication Date: 2025-04-22QINGHAI PROVINCIAL GEOLOGICAL SURVEY (QINGHAI PROVINCIAL INST OF GEOLOGY & MINERAL RESOURCES QINGHAI PROVINCIAL GEOLOGICAL REMOTE SENSING CENT)
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Patent Information

Application Number
CN202421759288.6
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-07-24
Publication Date
2025-04-22
Estimated Expiration
2034-07-24

AI Technical Summary

Technical Problem

When existing hyperspectral remote sensing geological survey devices land, the geotechnical spectrometer is susceptible to hard contact by obstacles such as rock protrusions, resulting in damage and increasing maintenance costs.

Method used

A hyperspectral geological survey device was designed, using protective components, including protective discs and threaded rod systems, which could completely block the ground object spectrometer before the drone landed to avoid contact with obstacles.

Benefits of technology

It effectively avoids damage caused by obstacles when landing, reduces unnecessary maintenance costs, extends the service life of the equipment, and improves its practicality.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of geological survey, and provides a hyperspectral geological survey device which comprises an unmanned aerial vehicle body, a ground object spectrometer is fixedly connected to the middle position of the bottom end of the unmanned aerial vehicle body, supporting legs are fixedly connected to the periphery of the bottom end of the unmanned aerial vehicle body, and a sliding block is fixedly connected to the bottom end of a damper. A damping spring is wound on the surface of the damper at the top end of the sliding block, the bottom end of the sliding block is fixedly connected with a damping rod extending to the outside of the supporting leg, the bottom end of the damping rod is fixedly connected with a mounting seat, and the bottom end of the mounting seat is movably connected with a buffer seat. When the unmanned aerial vehicle body lands, the micro servo motor is started to enable the protection disc to slide to completely expose the ground object spectrometer, when the unmanned aerial vehicle body is not used, the protection disc slides to completely shield and protect the bottom end of the ground object spectrometer, damage to the ground object spectrometer caused by obstacles such as rock protrusions when the unmanned aerial vehicle body lands is avoided, and the service life of the unmanned aerial vehicle body is prolonged.
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Description

Technical Field

[0001] The utility model relates to the technical field of geological survey, in particular to a high-spectrum geological survey device. Background Art

[0002] Geological exploration is a process of studying and detecting geological information such as the earth's internal structure, geological structure, mineral resources, groundwater and energy through various methods and techniques. It is an important means to ensure national energy security. With the development of science and technology, remote sensing surveys are now commonly used for geological surveys. UAVs are usually combined with ground spectrometers to greatly improve the work efficiency of geological surveys.

[0003] After searching, the existing patent (Announcement No.: CN216269912U) discloses a hyperspectral remote sensing geological survey device, including an unmanned aerial vehicle body, propellers are arranged around the unmanned aerial vehicle body, a ground object spectrometer is arranged at the bottom of the unmanned aerial vehicle body, bolts are installed around the ground object spectrometer, and the ground object spectrometer is fixed to the bottom of the unmanned aerial vehicle body by bolts. The hyperspectral remote sensing geological survey device is provided with a support spring and a buffer column installed inside the support column, so that after the buffer rubber pad contacts the ground, the buffer column squeezes the support spring to play a buffering role in the landing of the device, and four groups of push rods are installed around the positioning member, and four groups of support rods are installed around the connecting member, so that when the buffer column is contracted, the support rod drives the push rod to gradually expand from the contracted state, thereby ensuring the stability of the device when it lands, thereby solving the problem that the pressure generated by the descent easily causes damage to the ground object spectrometer.

[0004] However, in the above scheme, the drone can be well cushioned and shock-absorbed during landing, but the ground object spectrometer is still in an exposed state. If there are rock protrusions on the landing ground, it is easy for the protruding rocks to come into hard contact and collide with the ground object spectrometer, which will cause certain damage to it and result in unnecessary maintenance costs.

[0005] In view of this, the utility model proposes a hyperspectral geological survey device. Utility Model Content

[0006] The utility model provides a high-spectral geological survey device, which solves the problem in the related art that if there are rock protrusions at the landing site, the ground object spectrometer is easily damaged.

[0007] The technical solution of the utility model is as follows: a high-spectral geological survey device, comprising an unmanned aerial vehicle body, propellers are arranged around the top of the unmanned aerial vehicle body, a ground feature spectrometer is fixedly connected to the middle position of the bottom of the unmanned aerial vehicle body, a protective component is arranged on one side of the bottom of the unmanned aerial vehicle body, legs are fixedly connected to the bottom of the unmanned aerial vehicle body, a fixing groove is opened at the lower end of the inner part of the leg, a damper is fixedly connected to the inner top wall of the fixing groove, a slider is fixedly connected to the bottom end of the damper, a shock-absorbing spring is wound around the damper surface at the top of the slider, the top of the shock-absorbing spring is fixedly connected to the top wall of the fixing groove, a shock-absorbing rod extending to the outside of the leg is fixedly connected to the bottom end of the slider, a mounting seat is fixedly connected to the bottom end of the shock-absorbing rod, a mounting seat is arranged at one end of the mounting seat, and a mounting component is movably connected to the bottom end of the mounting seat.

[0008] Preferably, the cross-sectional area of ​​the protection plate is larger than the cross-sectional area of ​​the ground object spectrometer, and the cross-sectional diameter of the protection plate is smaller than the spacing between the legs.

[0009] Preferably, the reserved groove and the cross-section of the threaded block are inverted convex, and one side of the threaded block is fixedly connected to the surface of the protective plate by bolts.

[0010] Preferably, a slide bar is fixedly connected to the other side of the bottom end of the drone body, a connecting block is slidably connected to the surface of the slide bar, and one side of the connecting block is fixedly connected to the surface of the protective plate by bolts.

[0011] Preferably, the mounting assembly includes a card slot, which is opened at the bottom end of the mounting seat, a sliding slot is opened on one side of the mounting seat above the card slot, the inner top wall of the sliding slot is fixedly connected with a fixed spring, the bottom end of the fixed spring is fixedly connected with a sliding block, one side of the sliding block is fixedly connected with a limit plate extending to the outside of the sliding slot, and the top of the buffer seat is fixedly connected with a card block.

[0012] Preferably, a locking structure is formed between the clamping block and the inside of the clamping slot, and the cross-sections of the clamping block and the clamping slot are inverted convex shapes.

[0013] Preferably, friction ridges are fixedly connected to one side of the limiting plate at equal intervals, and the cross-section of the friction ridges is rectangular.

[0014] Preferably, one side of the limiting plate is in close contact with one side of the slot, and the other side of the limiting plate and one side of the sliding block are welded to form an integrated structure.

[0015] Preferably, the bottom end of the buffer seat is provided with anti-skid grooves at equal angles, and the shape of the anti-skid grooves in a top view is arc-shaped.

[0016] Preferably, a sliding structure is formed between the slider and the interior of the fixing groove, and the slider and the fixing groove are in a cross shape in a top view.

[0017] The working principle and beneficial effects of the utility model are:

[0018] 1. The utility model provides a protective assembly. When the ground object spectrometer needs to be used, the micro servo motor is started to drive the threaded rod to rotate, so that the threaded block slides and drives the protective plate to slide until the ground object spectrometer is fully opened, which is convenient for geological survey operations of the ground object spectrometer. When the drone body is about to land on the ground, the protective plate can slide to completely shield the bottom of the ground object spectrometer to prevent the ground object spectrometer from being damaged by collision with obstacles such as rock protrusions during landing, thereby reducing unnecessary maintenance costs, extending its service life, and improving its practicality.

[0019] 2. In the utility model, an installation component is set up, and the engagement between the card block and the inside of the card slot is utilized, and the elastic force of the fixed spring can be utilized to make the limit plate descend to limit and clamp one side of the card block, thereby avoiding the separation between the card block and the card slot, and realizing rapid disassembly and assembly between the mounting seat and the buffer seat, so as to facilitate the replacement of the buffer seat that is severely worn or damaged, thereby avoiding the unstable landing and placement of the drone body due to untimely replacement, thereby improving its practicality. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] The utility model is further described in detail below in conjunction with the accompanying drawings and specific implementation methods.

[0021] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0022] Figure 2 This is a schematic diagram of the structure of the utility model when viewed from above;

[0023] Figure 3 This is a schematic diagram of the structure of the utility model when the legs are removed and viewed from above;

[0024] Figure 4 It is a schematic diagram of the enlarged cross-section structure of the support leg of the utility model;

[0025] Figure 5 This is a schematic diagram of the enlarged structure of a local explosion at a protective component of the utility model;

[0026] Figure 6 It is a schematic diagram of a partially exploded and enlarged structure of the installation component of the utility model.

[0027] In the figure: 1. outrigger; 2. mounting assembly; 201. fixing spring; 202. clamping block; 203. friction convex strip; 204. limit plate; 205. clamping slot; 206. sliding slot; 207. sliding block; 3. mounting seat; 4. buffer seat; 5. drone body; 6. propeller; 7. protection assembly; 701. protection plate; 702. threaded rod; 703. sliding rod; 704. fixing bracket; 705. micro servo motor; 706. reserved slot; 707. threaded block; 708. connecting block; 8. anti-skid pattern; 9. shock absorbing rod; 10. ground feature spectrometer; 11. slider; 12. fixing slot; 13. damper; 14. shock absorbing spring. DETAILED DESCRIPTION

[0028] The following will be combined with 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 of 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.

[0029] Example 1

[0030] The preferred embodiment of the hyperspectral geological survey device provided by the utility model is as follows: Figures 1 to 6 As shown: a hyperspectral geological survey device, including an unmanned aerial vehicle body 5, propellers 6 are arranged around the top of the unmanned aerial vehicle body 5, a ground feature spectrometer 10 is fixedly connected to the middle position of the bottom of the unmanned aerial vehicle body 5, a protective component 7 is arranged on one side of the bottom of the unmanned aerial vehicle body 5, and a support leg 1 is fixedly connected to the bottom of the unmanned aerial vehicle body 5. A fixing groove 12 is opened at the lower end of the inner part of the support leg 1, and a damper 13 is fixedly connected to the inner top wall of the fixing groove 12. A slider 11 is fixedly connected to the bottom end of the damper 13, and a shock-absorbing spring 14 is wound around the surface of the damper 13 at the top of the slider 11. The top of the shock-absorbing spring 14 is fixedly connected to the inner top wall of the fixing groove 12, and the bottom end of the slider 11 is fixedly connected to a shock-absorbing rod 9 extending to the outside of the support leg 1, and the bottom end of the shock-absorbing rod 9 is fixedly connected to a mounting seat 3, one end of the mounting seat 3 is provided with a mounting component 2, and the bottom end of the mounting seat 3 is movably connected to a buffer seat 4.

[0031] The protection component 7 includes a fixing frame 704, which is fixedly connected to one side of the bottom end of the UAV body 5. A reserved groove 706 is opened at the lower end of one side of the fixing frame 704. A micro servo motor 705 is fixedly connected to one end of the fixing frame 704. The output end of the micro servo motor 705 extends to the inside of the reserved groove 706 and is fixedly connected to a threaded rod 702 through a coupling. A threaded block 707 is threadedly connected to the surface of the threaded rod 702. One side of the threaded block 707 extends to the outside of the reserved groove 706 and is fixedly connected to a protection plate 701. By starting the micro servo motor 705 to drive the threaded rod 702 to rotate, the threaded block 707 slides and drives the protection plate 701 to slide until the ground object spectrometer 10 is fully opened, which is convenient for the geological survey operation of the ground object spectrometer 10. When the UAV body 5 is about to land on the ground, the protection plate 701 can slide to completely block and protect the bottom end of the ground object spectrometer 10 to avoid damage to the ground object spectrometer 10 caused by obstacles such as rock protrusions during landing.

[0032] In this embodiment, the cross-sectional area of ​​the protective plate 701 is larger than the cross-sectional area of ​​the ground object spectrometer 10, and the cross-sectional diameter of the protective plate 701 is smaller than the spacing between the legs 1. By using a protective plate 701 of appropriate size, it is convenient to fully shield and protect the ground object spectrometer 10, and the protective plate 701 can be slid open between the legs 1.

[0033] In this embodiment, the cross-section of the reserved groove 706 and the threaded block 707 is inverted convex, and one side of the threaded block 707 is fixedly connected to the surface of the protective plate 701 by bolts. The sliding of the inverted convex threaded block 707 and the reserved groove 706 is utilized to improve the movement stability of the threaded block 707 on the surface of the threaded rod 702.

[0034] In this embodiment, a slide bar 703 is fixedly connected to the other side of the bottom end of the drone body 5, and a connecting block 708 is slidably connected to the surface of the slide bar 703. One side of the connecting block 708 is fixedly connected to the surface of the protective plate 701 by bolts. The sliding of the connecting block 708 on the surface of the slide bar 703 improves the smoothness of the sliding of the protective plate 701.

[0035] Example 2

[0036] On the basis of Example 1, a preferred embodiment of the hyperspectral geological survey device provided by the utility model is as follows: Figures 1 to 6As shown: the mounting assembly 2 includes a card slot 205, the card slot 205 is opened at the bottom end of the mounting seat 3, a sliding slot 206 is opened on one side of the mounting seat 3 above the card slot 205, the inner top wall of the sliding slot 206 is fixedly connected with a fixing spring 201, the bottom end of the fixing spring 201 is fixedly connected with a sliding block 207, one side of the sliding block 207 is fixedly connected with a limiting plate 204 extending to the outside of the sliding slot 206, and the top of the buffer seat 4 is fixedly connected with a card block 202, by utilizing the card block 202 and the inside of the card slot 205, and the elastic force of the fixing spring 201, the limiting plate 204 is lowered to limit and clamp one side of the card block 202, thereby realizing rapid disassembly and assembly between the mounting seat 3 and the buffer seat 4, and facilitating the replacement of the buffer seat 4 that is severely worn or damaged.

[0037] In this embodiment, a locking structure is formed between the block 202 and the inside of the slot 205. The cross-sections of the block 202 and the slot 205 are inverted convex. The locking between the inverted convex block 202 and the inside of the slot 205 is used to improve the stability of the initial locking installation of the mounting seat 3 and the buffer seat 4.

[0038] In this embodiment, friction ridges 203 are fixedly connected to one side of the limit plate 204 at equal intervals. The cross-section of the friction ridges 203 is rectangular. The rectangular friction ridges 203 are used to increase the contact friction between the user's fingers and the limit plate 204, thereby facilitating the sliding of the limit plate 204.

[0039] In this embodiment, one side of the limit plate 204 is in close contact with one side of the slot 205, and the other side of the limit plate 204 and one side of the sliding block 207 are welded into an integrated structure. The close contact with one side of the slot 205 ensures that the block 202 is tightly and firmly engaged with the inside of the slot 205.

[0040] Furthermore, the bottom of the buffer seat 4 is provided with anti-skid grooves 8 at equal angles. The shape of the anti-skid grooves 8 in a top view is arc-shaped. The arc-shaped anti-skid grooves 8 are used to improve the anti-skid stability between the bottom of the buffer seat 4 and the ground.

[0041] In addition, a sliding structure is formed between the slider 11 and the interior of the fixed groove 12. The shape of the slider 11 and the fixed groove 12 in the top view is a cross. The sliding of the cross-shaped slider 11 and the interior of the fixed groove 12 is utilized to improve the stability of the up and down sliding of the shock-absorbing rod 9, thereby facilitating the smooth buffering and shock absorption of the drone body 5.

[0042] The working principle and use process of the utility model are as follows: first, the propeller 6 is rotated to make the drone body 5 rise, and when the ground object spectrometer 10 needs to be used, the micro servo motor 705 is started to drive the threaded rod 702 to rotate, and the threaded rod 702 and the threaded block 707 are matched with each other, so that the threaded block 707 slides and drives the protective plate 701 to slide until the ground object spectrometer 10 is fully opened, which is convenient for the geological survey operation of the ground object spectrometer 10. When the drone body 5 is about to land on the ground, the micro servo motor 705 can be started again to make the protective plate 701 slide to completely cover the bottom of the ground object spectrometer 10 for protection, so as to avoid damage to the ground object spectrometer 10 caused by obstacles such as rock protrusions during landing, thereby extending its service life;

[0043] At the same time, when the drone body 5 descends, the buffer seat 4 first contacts the ground. At this time, the arc-shaped anti-skid pattern 8 is used to improve the anti-skid stability between the bottom end of the buffer seat 4 and the ground. At the same time, the buffer seat 4 will rise and drive the mounting seat 3 to rise, thereby causing the shock absorbing rod 9 and the slider 11 to slide and compress the damper 13 and the shock absorbing spring 14. At this time, the shock absorbing spring 14 is used to absorb the impact energy generated by the external descent, and the damper 13 is used to consume the elastic potential energy absorbed by the shock absorbing spring 14. Then, the damper 13 and the shock absorbing spring 14 can be used to achieve buffering and shock absorption when the drone body 5 descends, thereby avoiding damage to the ground object spectrometer 10 caused by the descending impact.

[0044] When the bottom end of the buffer seat 4 is severely worn or damaged, resulting in unstable support for the drone body 5, the limit plate 204 can be moved to drive the sliding block 207 to slide inside the sliding groove 206 to compress the fixed spring 201 until the slot 205 is fully opened, and then the buffer seat 4 is pushed hard to make the block 202 completely disengage from the inside of the slot 205, thereby realizing the disassembly of the buffer seat 4. During installation, the limit plate 204 is first moved to open the slot 205, and then the block 202 is slid into the slot 205, and then the limit plate 204 is released. The elastic force of the fixed spring 201 is used to make the sliding block 207 slide and drive the limit plate 204 to return to its original position to limit and tighten one side of the block 202, thereby preventing the limit plate 204 from disengaging from the inside of the slot 205, thereby realizing a firm installation between the buffer seat 4 and the mounting seat 3.

[0045] The above are only preferred embodiments of the present invention and are not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. A hyperspectral geological survey device, comprising an unmanned aerial vehicle body (5), characterized in that: The top of the drone body (5) is provided with propellers (6) around it, a ground spectrometer (10) is fixedly connected to the middle position of the bottom of the drone body (5), a protective component (7) is provided on one side of the bottom of the drone body (5), and legs (1) are fixedly connected to the bottom of the drone body (5), a fixing groove (12) is provided at the lower end of the leg (1), a damper (13) is fixedly connected to the inner top wall of the fixing groove (12), and the bottom end of the damper (13) is fixedly connected to the bottom end of the damper (13). A slider (11) is fixedly connected, a damper (13) at the top of the slider (11) is wound with a shock absorbing spring (14), the top of the shock absorbing spring (14) is fixedly connected to the top wall of the fixing groove (12), the bottom of the slider (11) is fixedly connected to a shock absorbing rod (9) extending to the outside of the support leg (1), the bottom of the shock absorbing rod (9) is fixedly connected to a mounting seat (3), one end of the mounting seat (3) is provided with a mounting assembly (2), and the bottom of the mounting seat (3) is movably connected to a buffer seat (4); The protective component (7) comprises a fixing frame (704), wherein the fixing frame (704) is fixedly connected to one side of the bottom end of the drone body (5), a reserved groove (706) is provided at the lower end of one side of the fixing frame (704), one end of the fixing frame (704) is fixedly connected to a micro servo motor (705), an output end of the micro servo motor (705) extends to the inside of the reserved groove (706) and is fixedly connected to a threaded rod (702) via a coupling, a threaded block (707) is threadedly connected to the surface of the threaded rod (702), and one side of the threaded block (707) extends to the outside of the reserved groove (706) and is fixedly connected to a protective plate (701).

2. A hyperspectral geological survey device according to claim 1, characterized in that: The cross-sectional area of ​​the protection plate (701) is greater than the cross-sectional area of ​​the ground object spectrometer (10), and the cross-sectional diameter of the protection plate (701) is less than the spacing between the legs (1).

3. A hyperspectral geological survey device according to claim 1, characterized in that: The cross-sections of the reserved groove (706) and the threaded block (707) are inverted convex shapes, and one side of the threaded block (707) is fixedly connected to the surface of the protective plate (701) by bolts.

4. A hyperspectral geological survey device according to claim 1, characterized in that: A slide bar (703) is fixedly connected to the other side of the bottom end of the drone body (5), and a connecting block (708) is slidably connected to the surface of the slide bar (703), and one side of the connecting block (708) is fixedly connected to the surface of the protective plate (701) through bolts.

5. A hyperspectral geological survey device according to claim 1, characterized in that: The mounting assembly (2) comprises a card slot (205), wherein the card slot (205) is provided at the bottom end of the mounting seat (3), a sliding slot (206) is provided on one side of the mounting seat (3) above the card slot (205), a fixing spring (201) is fixedly connected to the inner top wall of the sliding slot (206), a sliding block (207) is fixedly connected to the bottom end of the fixing spring (201), a limiting plate (204) extending to the outside of the sliding slot (206) is fixedly connected to one side of the sliding block (207), and a card block (202) is fixedly connected to the top end of the buffer seat (4).

6. A hyperspectral geological survey device according to claim 5, characterized in that: A locking structure is formed between the locking block (202) and the inside of the locking slot (205); the cross-sections of the locking block (202) and the locking slot (205) are inverted convex shapes.

7. A hyperspectral geological survey device according to claim 5, characterized in that: One side of the limiting plate (204) is fixedly connected with friction convex strips (203) at equal intervals, and the cross-section of the friction convex strips (203) is rectangular.

8. A hyperspectral geological survey device according to claim 5, characterized in that: One side of the limiting plate (204) is in close contact with one side of the slot (205), and the other side of the limiting plate (204) and one side of the sliding block (207) are welded together to form an integrated structure.

9. A hyperspectral geological survey device according to claim 1, characterized in that: The bottom end of the buffer seat (4) is provided with anti-skid patterns (8) at equal angles, and the anti-skid patterns (8) are arc-shaped in a top view.

10. A hyperspectral geological survey device according to claim 1, characterized in that: A sliding structure is formed between the slider (11) and the interior of the fixing groove (12); the slider (11) and the fixing groove (12) are in a cross shape in a top view.

Citation Information

Patent Citations

  • Hyperspectral remote sensing geological survey device

    CN216269912U