Unmanned aerial vehicle protection structure for geological exploration

Abstract

The unmanned aerial vehicle protection structure for geological exploration comprises an unmanned aerial vehicle body, unmanned aerial vehicle supports are symmetrically and fixedly installed at the lower end of the unmanned aerial vehicle body, and a first protection frame and a second protection frame are symmetrically arranged on the left side and the right side of the unmanned aerial vehicle body; two inserting plates are symmetrically and fixedly mounted on the side, making contact with the second protection frame, of the first protection frame, and two inserting grooves used for being matched with the inserting plates are symmetrically formed in one side of the second protection frame; the upper end of the first protection frame and the upper end of the second protection frame are provided with protection assemblies used for preventing impurities or foreign matter from touching the propellers. The protection frame and the protection net form a complete protection structure, all-directional protection is provided for the unmanned aerial vehicle, effective buffering is provided for the unmanned aerial vehicle during landing through the buffering supporting feet, damage of landing impact to the unmanned aerial vehicle is reduced, and the service life of the unmanned aerial vehicle is prolonged.

Description

TECHNICAL FIELD

[0001] The utility model relates to an unmanned plane protection structure technical field especially relates to an unmanned plane protection structure for geological exploration. BACKGROUND

[0002] With the continuous development of unmanned plane technology, the application of unmanned plane in the field of geological exploration is increasingly widespread. Geological exploration usually needs to be carried out in complex and changeable environment, which puts high requirements on the stability and protection performance of unmanned plane. The traditional unmanned plane design often lacks sufficient protection structure, so that the unmanned plane is easily disturbed and damaged by the external environment during flight, especially when encountering accidental collision or impact, the damage risk of unmanned plane significantly increases.

[0003] In addition, the landing process of unmanned plane is also one of the links that it is easily damaged. The traditional unmanned plane landing mode often lacks sufficient buffer structure, so that the unmanned plane is easily impacted and vibrated when landing, and further causes damage. SUMMARY

[0004] The utility model aims at solving the shortcomings in the prior art and provides an unmanned plane protection structure for geological exploration, which forms a complete protection structure by using the protection frame and the protection net, provides all-round protection for the unmanned plane, and provides effective buffer for the unmanned plane when landing through the buffer foot, reduces the damage of landing impact to the unmanned plane, and prolongs the service life of the unmanned plane.

[0005] In order to realize the above-mentioned purpose, the utility model adopts the following technical scheme:

[0006] An unmanned plane protection structure for geological exploration, comprising an unmanned plane main body, the lower end of the unmanned plane main body is symmetrically fixedly installed with an unmanned plane support, the left and right sides of the unmanned plane main body are symmetrically provided with a protection frame one and a protection frame two, the side in contact with the protection frame one and the protection frame two is symmetrically fixedly installed with two plug-in plates, and the side of the protection frame two is symmetrically provided with two plug-in grooves matched with the plug-in plates.

[0007] The upper end of the protection frame one and the protection frame two is provided with a protection assembly for preventing impurities or foreign matters from touching the propeller.

[0008] The protection frame one and the protection frame two are detachably connected with the unmanned plane main body through the mounting assembly.

[0009] Preferably, the protection frame one and the protection frame two are both composed of a circular arc plate and a horizontal plate arranged at both ends of the circular arc plate, and the outer surface of the circular arc plate is fixedly installed with a buffer air bag.

[0010] Preferably, the protection assembly comprises two protection net mounting racks fixedly mounted at one upper end of the protection frame, and the protection net mounting racks are internally fixedly mounted with protection nets.

[0011] Preferably, the mounting assembly comprises a mounting column fixedly mounted on a side wall of the protection frame, and the mounting column is rotationally connected with a mounting plate at a lower end thereof, and the mounting plate is detachably connected with the unmanned aerial vehicle body through mounting bolts.

[0012] Preferably, the mounting plate is fixedly mounted with a fixing cylinder at a lower end thereof, and a buffer leg is slidably connected in the fixing cylinder, and the buffer leg and the fixing cylinder are elastically connected through a spring.

[0013] Preferably, two reinforcing frames are fixedly mounted between the protection frame one, the protection frame two and the protection net mounting rack, so as to reinforce the stability of the protection net mounting rack.

[0014] The utility model has the following beneficial effects:

[0015] 1. By setting up protection frame one and protection frame two, and the design of the insertion plate and the insertion slot between them, a complete protection structure is formed, which provides all-round protection for the unmanned aerial vehicle. This design significantly enhances the ability of the unmanned aerial vehicle to resist accidental collision or impact during geological exploration, reducing damage caused by collision;

[0016] 2. The buffer air bag fixedly mounted on the outer surface of the arc plate on the protection frame further improves the protection performance of the unmanned aerial vehicle. In the event of a collision, the buffer air bag can absorb and disperse the impact force, providing additional buffer protection for the unmanned aerial vehicle and reducing the risk of damage;

[0017] 3. The design of the protection assembly, especially the protection net mounting rack and the protection net inside it, effectively prevents impurities or foreign objects from touching the propeller of the unmanned aerial vehicle. This not only protects the propeller from damage, but also ensures the safety of the unmanned aerial vehicle in flight, avoiding flight accidents caused by damaged propellers;

[0018] 4. The spring elastic connection between the buffer leg and the fixing cylinder in the mounting assembly provides effective cushioning for the unmanned aerial vehicle during landing. This design reduces the damage to the unmanned aerial vehicle caused by landing impact, prolonging the service life of the unmanned aerial vehicle;

[0019] 5. The entire protection structure is detachably connected with the unmanned aerial vehicle body through mounting bolts. This design makes the installation, disassembly and maintenance of the protection structure simple and fast. This not only improves work efficiency, but also reduces maintenance costs. BRIEF DESCRIPTION OF DRAWINGS

[0020] Fig. 1 The utility model provides a kind of unmanned aerial vehicle protection structure for geological exploration structure schematic view.

[0021] Fig. 2 The bottom structure schematic view of the unmanned aerial vehicle protection structure for geological exploration is provided in the utility model;

[0022] Fig. 3 The combination schematic view of the protection frame one and the protection frame two of the unmanned aerial vehicle protection structure for geological exploration is provided in the utility model.

[0023] In the drawing: 1 unmanned aerial vehicle main body, 2 protection frame one, 3 protection frame two, 4 buffer air bag, 5 protection net mounting frame, 6 mounting column, 7 mounting plate, 8 protection net, 9 unmanned aerial vehicle support, 10 reinforcing frame, 11 fixed cylinder, 12 buffer supporting leg, 13 mounting bolt, 14 plug-in plate. DETAILED DESCRIPTION

[0024] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments.

[0025] In the description of the utility model, it should be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer" and the like indicate the orientation or positional relationship shown in the drawings, and are only for the convenience of describing the utility model and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as a limitation on the utility model.

[0026] Referring to Figs. 1-3 The unmanned aerial vehicle protection structure for geological exploration comprises an unmanned aerial vehicle main body 1, the lower end of the unmanned aerial vehicle main body 1 is symmetrically fixedly provided with an unmanned aerial vehicle support 9, the left and right sides of the unmanned aerial vehicle main body 1 are symmetrically provided with a protection frame one 2 and a protection frame two 3, the side, in contact with the protection frame two 3, of the protection frame one 2 is symmetrically fixedly provided with two plug-in plates 14, the side of the protection frame two 3 is symmetrically provided with two plug-in grooves matched with the plug-in plates 14, the protection frame one 2 and the protection frame two 3 can be combined together to form a complete protection structure, and this design is convenient for installation and dismounting;

[0027] The protection frame one 2 and the protection frame two 3 are both composed of a circular arc plate and a horizontal plate arranged at the two ends of the circular arc plate, the outer surface of the circular arc plate is fixedly provided with a buffer air bag 4, and the buffer air bag 4 is used for providing additional buffer protection when the unmanned aerial vehicle collides;

[0028] The upper ends of the protection frame one 2 and the protection frame two 3 are provided with a protection assembly for preventing impurities or foreign matters from touching the propeller, the protection assembly comprises two protection net mounting racks 5 fixedly installed on the upper end of the protection frame one 2, two reinforcing racks 10 are fixedly installed between the protection frame one 2, the protection frame two 3 and the protection net mounting rack 5, for reinforcing the stability of the protection net mounting rack 5, the protection net mounting rack 5 is fixedly installed with a protection net 8 inside, for preventing impurities or foreign matters from touching the propeller of the unmanned aerial vehicle, so as to protect the propeller from being damaged, and meanwhile, the flight safety of the unmanned aerial vehicle is ensured;

[0029] The protection frame one 2 and the protection frame two 3 are detachably connected with the unmanned aerial vehicle body 1 through the mounting assembly, the mounting assembly comprises a mounting column 6 fixedly installed on the side wall of the protection frame one 2, the lower end of the mounting column 6 is rotatably connected with a mounting plate 7, and the mounting plate 7 is detachably connected with the unmanned aerial vehicle body 1 through mounting bolts 13.

[0030] The lower end of the mounting plate 7 is fixedly installed with a fixed cylinder 11, and a buffer leg 12 is slidably connected in the fixed cylinder 11, and the buffer leg 12 and the fixed cylinder 11 are elastically connected through a spring, so that the stability of the unmanned aerial vehicle is increased, and meanwhile, the buffer leg 12 can provide buffering when the unmanned aerial vehicle lands, so that the damage of landing impact to the unmanned aerial vehicle is reduced.

[0031] Working principle:

[0032] When the unmanned aerial vehicle body 1 flies in the geological exploration process, the protection frame one 2, the protection frame two 3 and the buffer air bag 4 thereon provide effective protection for the unmanned aerial vehicle body 1, and the damage caused by accidental collision or impact is reduced.

[0033] The protection net mounting rack 5 and the protection net 8 inside the protection net mounting rack 5 prevent impurities or foreign matters from touching the propeller, so that the flight safety of the unmanned aerial vehicle body 1 is ensured, when the unmanned aerial vehicle body 1 lands, the buffer leg 12 provides buffering through the elastic connection of the spring, so that the damage of landing impact to the unmanned aerial vehicle body 1 is reduced, and the whole protection structure is detachably connected with the unmanned aerial vehicle body 1 through the mounting bolts 13, so that the installation, dismounting and maintenance are facilitated.

[0034] The above is only a preferred specific implementation manner of the utility model, but the protection scope of the utility model is not limited to this, any skilled person in the art can make equivalent replacement or change according to the technical scheme and the utility model concept of the utility model within the technical range disclosed by the utility model, which should be covered in the protection scope of the utility model.

Claims

1. A drone protection structure for geological exploration, characterized by: Including unmanned aerial vehicle body (1), the lower end of unmanned aerial vehicle body (1) is symmetrically fixedly installed with unmanned aerial vehicle support (9), the left and right sides of unmanned aerial vehicle body (1) are symmetrically provided with guard frame one (2) and guard frame two (3), the side of guard frame one (2) and guard frame two (3) is symmetrically fixedly installed with two plug-in plates (14), one side of guard frame two (3) is symmetrically provided with two plug-in slots for plug-in plate (14) matched with each other; The upper end of the guard frame one (2) and the guard frame two (3) is provided with a protection assembly for preventing impurities or foreign matters from touching the propeller. The guard frame one (2) and the guard frame two (3) are detachably connected with the unmanned aerial vehicle body (1) through the mounting assembly.

2. The unmanned aerial vehicle shielding structure for geological exploration of claim 1, wherein, The guard frame one (2) and the guard frame two (3) are both composed of an arc plate and a horizontal plate arranged on both ends of the arc plate, and a buffer air bag (4) is fixedly installed on the outer surface of the arc plate.

3. The unmanned aerial vehicle shielding structure for geological exploration of claim 1, wherein, The protection assembly includes two protection net mounting racks (5) fixedly installed on the upper end of the guard frame one (2), and a protection net (8) is fixedly installed in the protection net mounting rack (5).

4. The unmanned aerial vehicle shielding structure for geological exploration of claim 1, wherein, The mounting assembly includes a mounting column (6) fixedly installed on the side wall of the guard frame one (2), a mounting plate (7) rotatably connected to the lower end of the mounting column (6), and the mounting plate (7) is detachably connected with the unmanned aerial vehicle body (1) through mounting bolts (13).

5. The unmanned aerial vehicle shielding structure for geological exploration of claim 4, wherein, The lower end of the mounting plate (7) is fixedly installed with a fixing cylinder (11), the inside of the fixing cylinder (11) is slidably connected with a buffer supporting leg (12), and the buffer supporting leg (12) and the fixing cylinder (11) are elastically connected through a spring.

6. The unmanned aerial vehicle shielding structure for geological exploration of claim 1, wherein, Two reinforcing frames (10) are fixedly installed between the guard frame one (2), the guard frame two (3) and the protection net mounting rack (5) for reinforcing the stability of the protection net mounting rack (5).

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