Water and soil conservation monitoring unmanned aerial vehicle with protection function

Abstract

The utility model discloses a water and soil conservation monitoring unmanned aerial vehicle with a protection function, and belongs to the technical field of unmanned aerial vehicles. Comprising a machine frame and a machine top cover, the machine top cover is installed at the top end of the machine frame, supporting columns are symmetrically installed on the side wall of the machine top cover, circular protection rings are installed at the ends, away from the machine top cover, of the supporting columns correspondingly, arc-shaped protection rings are arranged outside the circular protection rings correspondingly, and rotating protection rings are arranged inside the circular protection rings correspondingly; and a probe is installed at the center position of the bottom end of the rack, and servo motors are installed on the sides, close to the circular protection ring, of the supporting columns correspondingly. According to the unmanned aerial vehicle, multi-position self-protection of the unmanned aerial vehicle is achieved, the service life of the unmanned aerial vehicle is prolonged, the convenience of multi-directional protection of the unmanned aerial vehicle is improved, convenient and safe landing of the unmanned aerial vehicle is achieved, the shaking amplitude of the unmanned aerial vehicle is reduced, and the stability of safe landing of the unmanned aerial vehicle is improved.

Description

TECHNICAL FIELD

[0001] The utility model relates to the technical field of unmanned plane with protection function, concretely is a kind of unmanned plane with protection function for water and soil conservation monitoring. BACKGROUND

[0002] Unmanned plane is the aircraft that is not loaded person using radio remote control equipment and self-provided program control device to manipulate, or by on-board computer completely or intermittently autonomously operates, unmanned plane is the general term of unmanned aerial vehicle, including near space aircraft (such as stratosphere airship, high-altitude balloon, solar unmanned plane etc.), it can complete complex aerial flight task and various load task under the condition of unmanned, therefore also be called "air robot".

[0003] As the authorized announcement No. CN221874354U discloses a kind of unmanned plane with protection function, including main part, the top of the main part is fixedly connected with fixed block, the inside of the fixed block is slidably connected with slide bar, the outer wall of the slide bar is slidably connected with movable block, the outer wall of the main part is provided with protection structure, the protection structure includes buffer seat, the outer wall of the main part is fixedly connected with buffer seat.

[0004] It is realized that the fixed seat drives the sliding block to slide on the slide bar, the sliding block pushes the movable block to move, the protection box moves with the camera to the inside of the body, improves the protection ability of the camera, the fixing bolt and the limiting plate are fixedly installed, so that the arm is limited to move on the buffer seat, and at the same time, the propellers on the two arms will not collide, and the protection ability of the arm and the propeller is improved.

[0005] But it does not solve the problem that the existing unmanned plane with protection function is not conducive to the self-protection of unmanned plane in multiple positions when in use, which affects the service life of unmanned plane, and is not convenient for the safe landing of unmanned plane, which greatly affects the amplitude of shaking of unmanned plane and the stability of safe landing of unmanned plane. UTILITY MODEL CONTENT

[0006] The utility model aims at providing a kind of unmanned plane with protection function for water and soil conservation monitoring to solve the problem that the unmanned plane with protection function is not convenient for the self-protection of unmanned plane in multiple positions in the above background art, which affects the service life of unmanned plane, and is not convenient for the safe landing of unmanned plane, which greatly affects the amplitude of shaking of unmanned plane and the stability of safe landing of unmanned plane.

[0007] Further, the rotating shaft extends through the circular protection ring to its inside, the rotating shaft is connected with the rotating protection ring, the rotating protection ring is installed with movable shaft at the end away from the rotating shaft, and the movable shaft is movably connected with the circular protection ring.

[0008] Further, the inner wall of the arc-shaped protective ring is provided with a plurality of groups of equal-interval damping springs, and the arc-shaped protective ring is connected with the circular protective ring through the damping springs.

[0009] Further, the outer portion of the rack is provided with four groups of special-shaped plates, and the bottom end of the rack is symmetrically provided with support rods.

[0010] Further, the two ends of the support rod are both provided with support plates, and the support plates are connected with the special-shaped plates.

[0011] Further, the outer portion of the support plate is provided with a bottom plate, and the top end of the bottom plate is provided with a U-shaped plate.

[0012] Further, the outer portion of the U-shaped plate is provided with two groups of support arms, and the side close to the U-shaped plate of the support arm is movably provided with a first shaft.

[0013] Further, the support arm is movably connected with the U-shaped plate through the first shaft, and the end away from the first shaft of the support arm is movably provided with a second shaft.

[0014] Further, the support arm is movably connected with the special-shaped plate through the second shaft, and the inner portion of the U-shaped plate is movably provided with a damping shock absorber.

[0015] Further, the end away from the U-shaped plate of the damping shock absorber is movably provided with a rotating shaft, and the rotating shaft is movably connected with the special-shaped plate.

[0016] Compared with the prior art, the unmanned aerial vehicle with the protection function not only realizes self-protection of the unmanned aerial vehicle in multiple positions, increases the service life of the unmanned aerial vehicle, and improves the convenience of multi-directional protection of the unmanned aerial vehicle, but also realizes convenient and safe landing of the unmanned aerial vehicle, reduces the amplitude of shaking of the unmanned aerial vehicle, and improves the stability of safe landing of the unmanned aerial vehicle.

[0017] The servo motor drives the rotor to rotate, the unmanned aerial vehicle is lifted to the air, the probe detects the surrounding water and soil, the stepping motor drives the rotating shaft to rotate, under the support of the movable shaft, the rotating shaft drives the rotating protective ring to rotate by a certain angle, so as to prevent the top end of the rotor from colliding with the obstacle, when the side wall collides with the obstacle, the obstacle collides with the arc-shaped protective ring first, under the buffering of the damping spring, the circular protective ring, the rotor and the unmanned aerial vehicle slightly shake, to a certain extent, the unmanned aerial vehicle is greatly protected, self-protection of the unmanned aerial vehicle in multiple positions is realized, the service life of the unmanned aerial vehicle is increased, and the convenience of multi-directional protection of the unmanned aerial vehicle is improved.

[0018] When the unmanned aerial vehicle falls to the ground, the rotor drives the support column, the machine top cover, the machine frame, the support rod, the support plate and the bottom plate to descend, when the bottom plate contacts the ground, the bottom plate offsets the reaction force bounced back by the ground through the U-shaped plate and the damping shock absorber, under the action of the U-shaped plate, the support arm, the first shaft, the second shaft, the special-shaped plate and the support plate, the unmanned aerial vehicle reduces the shaking range, realizes convenient and safe landing of the unmanned aerial vehicle, reduces the shaking range of the unmanned aerial vehicle, and improves the stability of safe landing of the unmanned aerial vehicle. BRIEF DESCRIPTION OF DRAWINGS

[0019] The accompanying drawings, which form a part of this application, are included to provide a further understanding of the application and are incorporated in and constitute a part of this application. The drawings illustrate embodiments of the application and, together with the description, serve to explain the application.

[0020] In addition, throughout the drawings, same or similar reference numerals are used to represent same or similar elements. It should be understood that the drawings are schematic, and elements and elements are not necessarily drawn to scale.

[0021] In the drawings:

[0022] Figure 1 is a three-dimensional structure schematic view of the utility model;

[0023] Figure 2 is a front view structure schematic view of the utility model;

[0024] Figure 3 is a three-dimensional structure schematic view of the circular protective ring of the utility model;

[0025] Figure 4 is a three-dimensional structure schematic view of the machine frame of the utility model;

[0026] Figure 5 is a three-dimensional structure schematic view of the special-shaped plate of the utility model.

[0027] Reference numerals:

[0028] 1, machine frame, 2, machine top cover, 3, support column, 4, circular protective ring, 5, arc-shaped protective ring, 6, rotating protective ring, 7, probe, 8, special-shaped plate, 9, damping spring, 10, servo motor, 11, rotor, 12, stepping motor, 13, rotating shaft, 14, movable shaft, 15, support plate, 16, rotating shaft, 17, bottom plate, 18, support rod, 19, U-shaped plate, 20, support arm, 21, first shaft, 22, second shaft, 23, damping shock absorber. DETAILED DESCRIPTION

[0029] Embodiments of the present disclosure will be described in more detail below with reference to the drawings. Although certain embodiments of the present disclosure are shown in the drawings, it is understood that the present disclosure can be implemented in various forms and should not be interpreted as being limited to the embodiments set forth herein. Rather, these embodiments are provided so that the present disclosure can be more thoroughly and completely understood. It should be understood that the drawings and embodiments of the present disclosure are only for exemplary purposes and are not intended to limit the scope of protection of the present disclosure.

[0030] In addition, it should be further noted that only parts related to the present application are shown in the drawings for ease of description. The embodiments in the present disclosure and the features in the embodiments can be combined with each other without conflict.

[0031] It should be noted that the concepts of "first", "second", etc. mentioned in the present disclosure are only used to distinguish different devices, modules or units, and are not used to limit the order or interdependence of the functions performed by these devices, modules or units.

[0032] It should be noted that the adjectives "one" and "multiple" mentioned in the present disclosure are illustrative and not limiting, and those skilled in the art should understand that unless the context clearly indicates otherwise, it should be understood as "one or more".

[0033] Please refer to Figures 1-5 The utility model provides an embodiment: a soil and water conservation monitoring unmanned plane with protection function, including frame 1 and roof 2, the top of frame 1 is installed with roof 2, the lateral wall of roof 2 is installed with support column 3 symmetrically, the end away from roof 2 of support column 3 all is installed with round protective ring 4, the outside of round protective ring 4 all is provided with arc protective ring 5, the inside of round protective ring 4 all is provided with rotation protective ring 6, the bottom center position of frame 1 is installed with probe 7, the side close to round protective ring 4 of support column 3 all is installed with servo motor 10, the output of servo motor 10 all is installed with rotor 11, the lateral wall of round protective ring 4 all is installed with step motor 12, the output of step motor 12 all is installed with rotating shaft 13, rotating shaft 13 extends to its inside through round protective ring 4, rotating shaft 13 is connected with rotation protective ring 6, the end away from rotating shaft 13 of rotation protective ring 6 is installed with movable shaft 14, movable shaft 14 is movably connected with round protective ring 4, the inner wall of arc protective ring 5 is provided with multiple groups of equal-interval shock absorber springs 9, arc protective ring 5 is connected with round protective ring 4 through shock absorber spring 9.

[0034] When the unmanned aerial vehicle is used, a plurality of groups of servo motors 10 are opened, under the support of the support column 3, the servo motor 10 drives the rotor 11 to rotate, and the unmanned aerial vehicle is lifted to the air, the surrounding water and soil are detected through the probe 7, the stepper motor 12 is opened, under the support of the circular protective ring 4, the stepper motor 12 drives the rotating shaft 13 to rotate, under the support of the movable shaft 14, the rotating shaft 13 drives the rotating protective ring 6 to rotate by a certain angle, preventing the top end of the rotor 11 from colliding with the obstacle, when the side wall collides with the obstacle, the obstacle collides with the arc-shaped protective ring 5 first, under the buffering of the damping spring 9, the circular protective ring 4, the rotor 11 and the unmanned aerial vehicle are slightly shaken, to a certain extent, the unmanned aerial vehicle is greatly protected, the service life of the unmanned aerial vehicle is increased, and the convenience of multi-directional protection of the unmanned aerial vehicle is improved.

[0035] The outer part of the rack 1 is provided with four groups of special-shaped plates 8, the bottom end of the rack 1 is symmetrically provided with support rods 18, both ends of the support rod 18 are provided with support plates 15, and the support plates 15 are connected with the special-shaped plates 8.

[0036] The outer part of the support plate 15 is provided with a bottom plate 17, the top end of the bottom plate 17 is provided with a U-shaped plate 19, the outer part of the U-shaped plate 19 is provided with two groups of support arms 20, and the side, close to the U-shaped plate 19, of the support arm 20 is movably provided with a first shaft 21.

[0037] The support arm 20 is movably connected with the U-shaped plate 19 through the first shaft 21, the end, away from the first shaft 21, of the support arm 20 is movably provided with a second shaft 22, the support arm 20 is movably connected with the special-shaped plate 8 through the second shaft 22, the inner part of the U-shaped plate 19 is movably provided with a damping shock absorber 23, the end, away from the U-shaped plate 19, of the damping shock absorber 23 is movably provided with a rotating shaft 16, and the rotating shaft 16 is movably connected with the special-shaped plate 8.

[0038] When the unmanned aerial vehicle falls to the ground, the rotor 11 drives the support column 3, the machine top cover 2, the rack 1, the support rod 18, the support plate 15 and the bottom plate 17 to descend, when the bottom plate 17 contacts the ground, the bottom plate 17 offsets the reaction force bounced back by the ground through the U-shaped plate 19 and the damping shock absorber 23, under the action of the U-shaped plate 19, the support arm 20, the first shaft 21, the second shaft 22, the special-shaped plate 8 and the support plate 15, the shaking range of the unmanned aerial vehicle is reduced, the unmanned aerial vehicle is safely landed conveniently, the shaking range of the unmanned aerial vehicle is reduced, and the stability of safe landing of the unmanned aerial vehicle is improved.

[0039] Working principle: when using the soil and water conservation monitoring unmanned aerial vehicle with protection function, the servo motor 10 drives the rotor 11 to rotate, and the unmanned aerial vehicle rises to the air, and the probe 7 detects the surrounding water and soil, the stepping motor 12 drives the rotating shaft 13 to rotate, under the support of the movable shaft 14, the rotating shaft 13 drives the rotating protective ring 6 to rotate by a certain angle, which prevents the top of the rotor 11 from colliding with the obstacle, when the side wall collides with the obstacle, the obstacle collides with the arc-shaped protective ring 5 first, under the buffering of the damping spring 9, the circular protective ring 4, the rotor 11 and the unmanned aerial vehicle are slightly shaken, which greatly protects the unmanned aerial vehicle to a certain extent, when the unmanned aerial vehicle falls to the ground, the rotor 11 drives the support column 3, the top cover 2, the rack 1, the support rod 18, the support plate 15 and the bottom plate 17 to descend, when the bottom plate 17 contacts with the ground, the bottom plate 17 offsets the reaction force of the ground rebound through the U-shaped plate 19 and the damping shock absorber 23, under the action of the U-shaped plate 19, the support arm 20, the first shaft 21, the second shaft 22, the special-shaped plate 8 and the support plate 15, the unmanned aerial vehicle reduces the shaking amplitude, to complete the use of the unmanned aerial vehicle with protection function.

[0040] The above description is only some of the preferred embodiments of the present disclosure and the explanation of the applied technical principles. Those skilled in the art should understand that the scope of the application involved in the embodiments of the present disclosure is not limited to the technical solutions formed by the specific combinations of the above technical features, and should also cover other technical solutions formed by any combination of the above technical features or their equivalent features without departing from the above inventive concept. For example, the above features are replaced with the technical features with similar functions disclosed in the embodiments of the present disclosure (but not limited to) to form technical solutions.

Claims

1. A soil and water conservation monitoring drone with a protection function, characterized in that: The utility model provides a kind of probe, including frame and machine top cover, the top end of the frame is equipped with machine top cover, the sidewall of the machine top cover is symmetrically equipped with support column, the end of the support column away from machine top cover is equipped with circular guard ring, the outside of the circular guard ring is provided with arc guard ring, the inside of the circular guard ring is provided with rotation guard ring, the bottom end center position of the frame is equipped with probe, the side of the support column close to circular guard ring is equipped with servo motor, the output of the servo motor is equipped with rotor, the sidewall of the circular guard ring is equipped with step motor, the output of the step motor is equipped with rotating shaft, the rotating shaft extends to its inside through circular guard ring.

2. The unmanned aerial vehicle for soil and water conservation monitoring with a protection function according to claim 1, characterized in that: The rotating shaft is connected with rotation guard ring, the end of the rotation guard ring away from rotating shaft is equipped with movable shaft, the movable shaft is movably connected with circular guard ring. 3.The soil and water conservation monitoring UAV with a protection function according to claim 2, characterized in that: The inner wall of the arc guard ring is provided with a plurality of groups of equal-interval shock-absorbing springs, and the arc guard ring is connected with the circular guard ring by the shock-absorbing springs. 4.The soil and water conservation monitoring UAV with a protection function according to claim 3, characterized in that: The outside of the frame is provided with four groups of special-shaped plates, and the bottom end of the frame is symmetrically equipped with support rod. 5.The soil and water conservation monitoring UAV with a protection function according to claim 4, characterized in that: The both ends of the support rod are equipped with support plate, and the support plate is connected with the special-shaped plate. 6.The soil and water conservation monitoring UAV with a protection function according to claim 5, characterized in that: The outside of the support plate is provided with bottom plate, and the top end of the bottom plate is equipped with U-shaped plate. 7.The soil and water conservation monitoring UAV with a protection function according to claim 6, characterized in that: The outside of the U-shaped plate is provided with two groups of support arms, and the side close to the U-shaped plate of the support arm is movably equipped with first shaft. 8.The soil and water conservation monitoring drone with a protection function of claim 7, characterized in that: The support arm is movably connected with the U-shaped plate by the first shaft, and the end away from the first shaft of the support arm is movably equipped with second shaft. 9.The soil and water conservation monitoring drone with a protection function of claim 8, characterized in that: The support arm is movably connected with the special-shaped plate by the second shaft, and the inside of the U-shaped plate is movably equipped with damping shock absorber. 10.The soil and water conservation monitoring UAV with a protection function according to claim 9, characterized in that: The end away from the U-shaped plate of the damping shock absorber is movably equipped with rotating shaft, and the rotating shaft is movably connected with the special-shaped plate.

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