Multifunctional mounted high-altitude single-soldier reconnaissance unmanned aerial vehicle and use method thereof

Abstract

The invention discloses a multifunctional mounted high-altitude individual reconnaissance unmanned aerial vehicle and a use method thereof.The multifunctional mounted high-altitude individual reconnaissance unmanned aerial vehicle comprises a shell and a fourth support, one side of the top of the shell is fixedly connected with a first support, the top of the first support is fixedly connected with a conductive slip ring, and the movable end of the conductive slip ring is fixedly connected with a second support; second fan blades are movably connected to the upper end of the inner surface of the second support, a second rotor is fixedly connected to the tail ends of the second fan blades, and a second stator is arranged on the outer side of the second rotor. The high-definition camera, the fifth support, the first wireless signal transceiver, the fourth motor and the third motor are arranged, the third motor is controlled to rotate through the external second wireless signal transceiver, the high-definition camera can be driven to rotate horizontally, the fourth motor is controlled to rotate, and the high-definition camera can be driven to conduct inclination adjustment. And the high-definition camera can transmit a shooting result through the first wireless signal transceiver.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles (UAVs), and in particular to a multifunctional mounted high-altitude individual reconnaissance UAV and a method for using the same. Background Art

[0002] Drones, with their maneuverability, high resolution, low cost, and high timeliness, have unparalleled advantages in remote sensing measurement and are widely used in aerial photography, agriculture, plant protection, micro selfies, express delivery, disaster relief, wildlife observation, infectious disease monitoring, surveying and mapping, news reporting, power inspections, disaster relief, film and television shooting, etc. In some high-altitude areas, due to the harsh environment, traditional manual inspections are extremely difficult, the work quality and efficiency are low, and there are certain threats to personal safety. Drones are often needed for reconnaissance missions, but the existing drones lack self-generating mechanisms, resulting in a short overall flight time, which brings inconvenience to people's use. Summary of the Invention

[0003] The purpose of the present invention is to provide a multifunctional mounted high-altitude individual reconnaissance drone and a method of using the same to solve the problems raised in the above-mentioned background technology.

[0004] To achieve the above-mentioned objectives, the present invention provides the following technical solutions: a multifunctional mounted high-altitude individual reconnaissance drone, comprising a casing and a fourth bracket, wherein one side of the top of the casing is fixedly connected to the first bracket, and the top of the first bracket is fixedly connected to a conductive slip ring, the movable end of the conductive slip ring is fixedly connected to the second bracket, and the upper end of the inner surface of the second bracket is movably connected to the second fan blade, the end of the second fan blade is fixedly connected to the second rotor, and a second stator is provided on the outside of the second rotor, the outside of the bottom of the fourth bracket is fixedly connected to the second motor, the output shaft of the second motor is connected to the first rotor through a single-sided tooth synchronous belt drive, and the outside of the first rotor is provided with a first stator.

[0005] Preferably, the front and rear ends of the top of the casing are fixedly connected to a third sleeve, the top of the inner cavity of the third sleeve is fixedly connected to a first spring and a damping shock absorber, the first spring is located on the outside of the damping shock absorber, the bottom of the first spring and the damping shock absorber is fixedly connected to a buffer rod, and the bottom of the buffer rod is fixedly connected to a pad.

[0006] Preferably, a third motor is fixedly connected to the middle end of the bottom of the casing, the output shaft of the third motor is fixedly connected to the fifth bracket, the outer side of the fifth bracket is fixedly connected to the fourth motor, and the output shaft of the fourth motor is fixedly connected to the high-definition camera.

[0007] Preferably, a battery is fixedly connected to the top of the inner cavity of the casing, a first wireless signal transceiver is fixedly connected to the bottom of the inner cavity of the casing, and a charging socket is provided at the bottom of the casing.

[0008] Preferably, a second sleeve is fixedly connected to the outer side of the second stator, the second sleeve is fixedly connected to the upper end of the outer side of the second bracket, and the outer surface of the second blade is fixedly connected to the limiting teeth.

[0009] Preferably, the second bracket is fixedly connected to a fixing block on one side of the second fan blade, the inner side of the fixing block is movably connected to a limiting rod through a second spring, and the lower end of the limiting rod is movably connected to the surface of the second bracket.

[0010] Preferably, the top of the casing is movably connected to a first gear, there are four first gears, every two adjacent first gears are meshed together, and the outermost first gear is meshed together with a toothed plate, the outer side of the top of the first bracket is fixedly connected to a first motor, and the output shaft of the first motor is fixedly connected to the outermost first gear.

[0011] Preferably, a sliding groove is provided on the inner surface of the tooth plate, and a slider is slidably connected to the inner side of the sliding groove, and the slider is fixedly connected to the upper end of the outer side of the casing. The upper ends of the left and right sides of the casing are fixedly connected to the third bracket, and the outer side of the inner surface of the third bracket is movably connected to the second gear, and the second gear is meshed with the tooth plate.

[0012] Preferably, the bottom of the second gear is fixedly connected to a fourth bracket, the outer side of the first stator is fixedly connected to a first sleeve, the first sleeve is fixedly connected to the bottom of the fourth bracket, and the output shaft of the second motor is fixedly connected to the first fan blade.

[0013] A method for using a multifunctional mounted high-altitude individual reconnaissance drone comprises the following steps:

[0014] A. The external second wireless signal transceiver controls the rotation of the third motor to drive the HD camera to rotate horizontally, and controls the rotation of the fourth motor to drive the HD camera to adjust the tilt. The HD camera can also transmit the shooting results through the first wireless signal transceiver.

[0015] B. When the second motor rotates, it drives the first rotor to rotate through a single-sided toothed synchronous belt, and in cooperation with the first stator, it can generate electricity and store the electricity in the battery, achieving the purpose of self-generating electricity during flight;

[0016] C. During the drone's launch, the limiting teeth, limiting rod, fixing block, and second spring cooperate to keep the second blade rotating in one direction. The conductive slip ring cooperates to keep the wind from blowing the second blade, thereby driving the second rotor to rotate. The second stator cooperates to generate electrical energy, which is then stored in a battery, achieving wind power generation.

[0017] D. When the drone lands, the buffer rod, pad, first spring and damping shock absorber can buffer the impact force, thereby improving landing safety;

[0018] E. Controlling the first motor to rotate can drive the outermost first gear to rotate, and drive the other first gears to rotate synchronously. With the cooperation of the slider and the slide groove, the gear plate can be driven to move synchronously, and the second gear can be driven to rotate, so that the fourth bracket can be folded and stored to reduce the overall volume.

[0019] Compared with the prior art, the present invention has the following beneficial effects:

[0020] The present invention is provided with a high-definition camera, a fifth bracket, a first wireless signal transceiver, a fourth motor and a third motor. The rotation of the third motor is controlled by an external second wireless signal transceiver to drive the high-definition camera to rotate horizontally. The rotation of the fourth motor is controlled to drive the high-definition camera to adjust the tilt, and the high-definition camera can transmit the shooting results through the first wireless signal transceiver. A first rotor, a first stator, a fourth bracket, a second motor and a first sleeve are provided. When the second motor rotates, the first rotor can be driven to rotate by a single-sided toothed synchronous belt, and with the cooperation of the first stator, electric energy can be generated and stored in a battery, so as to achieve the purpose of self-generating electricity during flight. A second bracket, a conductive slip ring, a limit tooth, a limit rod, a fixed block, a second spring, a second sleeve, a second stator and a second rotor are provided. During the launch of the UAV, with the cooperation of the limit tooth, the limit rod, the fixed block and the second spring The second fan blade is made to rotate in one direction at all times. With the cooperation of the conductive slip ring, the wind can always blow the second fan blade to rotate, thereby driving the second rotor to rotate, and with the cooperation of the second stator, electrical energy can be generated and stored in the battery, thereby achieving the purpose of wind power generation. A buffer rod, a third sleeve, a pad, a first spring and a damping shock absorber are provided. When the UAV lands, the buffer rod, the pad, the first spring and the damping shock absorber can buffer the impact force, thereby improving the safety during landing. A first gear, a tooth plate, a first bracket, a first motor, a slider, a second gear, a third bracket and a slide are provided. The rotation of the first motor is controlled to drive the outermost first gear to rotate and drive the other first gears to rotate synchronously. With the cooperation of the slider and the slide, the tooth plate can be driven to move synchronously and the second gear can be driven to rotate, so that the fourth bracket can be folded and stored to reduce the overall volume. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Figure 1 This is a schematic diagram of the three-dimensional structure of the present invention in the first viewing angle state;

[0022] Figure 2 This is a schematic diagram of the three-dimensional structure of the present invention in a second viewing angle state;

[0023] Figure 3 This is a schematic diagram of the three-dimensional structure of the present invention in the third viewing angle state;

[0024] Figure 4 Schematic diagram of the limiting tooth structure of the present invention;

[0025] Figure 5 This is a schematic diagram of the second rotor structure of the present invention;

[0026] Figure 6 This is a schematic diagram of the first stator structure of the present invention;

[0027] Figure 7 This is a schematic diagram of the third motor structure of the present invention;

[0028] Figure 8 This is a schematic diagram of the first spring structure of the present invention.

[0029] In the figure: casing 1, buffer rod 2, third sleeve 3, first gear 4, second bracket 5, second sleeve 6, second motor 7, charging jack 8, pad 9, conductive slip ring 10, first bracket 11, first fan blade 12, first motor 13, second fan blade 14, limiting tooth 15, limiting rod 16, fixing block 17, second spring 18, second stator 19, second rotor 20, slider 21, second gear 22, third bracket 23, first rotor 24, first stator 25, fourth bracket 26, slide 27, high-definition camera 28, fifth bracket 29, fourth motor 30, first wireless signal transceiver 31, battery 32, third motor 33, first spring 34, damping shock absorber 35, first sleeve 36, tooth plate 37. DETAILED DESCRIPTION

[0030] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0031] See also Figures 1-8A multifunctional mounted high-altitude individual reconnaissance drone includes a casing 1 and a fourth bracket 26. A first bracket 11 is fixedly connected to one side of the top of the casing 1, and a conductive slip ring 10 is fixedly connected to the top of the first bracket 11. The movable end of the conductive slip ring 10 is fixedly connected to the second bracket 5, and the upper end of the inner surface of the second bracket 5 is movably connected to the second fan blade 14. The end of the second fan blade 14 is fixedly connected to the second rotor 20, and a second stator 19 is provided on the outside of the second rotor 20. The outside of the bottom of the fourth bracket 26 is fixedly connected to the second motor 7. The output shaft of the second motor 7 is connected to the first rotor 24 through a single-sided tooth synchronous belt drive, and a first stator 25 is provided on the outside of the first rotor 24.

[0032] The front and rear ends of the top of the casing 1 are fixedly connected to the third sleeve 3, the top of the inner cavity of the third sleeve 3 is fixedly connected to the first spring 34 and the damping shock absorber 35, the first spring 34 is located on the outside of the damping shock absorber 35, the bottom of the first spring 34 and the damping shock absorber 35 is fixedly connected to the buffer rod 2, and the bottom of the buffer rod 2 is fixedly connected to the pad 9, the middle end of the bottom of the casing 1 is fixedly connected to the third motor 33, the output shaft of the third motor 33 is fixedly connected to the fifth bracket 29, and the outer side of the fifth bracket 29 is fixedly connected to the fourth motor 30, and The output shaft of the fourth motor 30 is fixedly connected to a high-definition camera 28, the top of the inner cavity of the casing 1 is fixedly connected to a battery 32, the bottom of the inner cavity of the casing 1 is fixedly connected to a first wireless signal transceiver 31, and a charging socket 8 is provided at the bottom of the casing 1. The outer side of the second stator 19 is fixedly connected to a second sleeve 6, the second sleeve 6 is fixedly connected to the upper end of the outer side of the second bracket 5, and the outer surface of the second fan blade 14 is fixedly connected to the limiting tooth 15, the second bracket 5 is located on one side of the second fan blade 14 and is fixedly connected to a fixing block 17, the inner side of the fixing block 17 is fixedly connected to the fixing block 17. The side is movably connected to the limit rod 16 through the second spring 18, and the lower end of the limit rod 16 is movably connected to the surface of the second bracket 5. The top of the housing 1 is movably connected to the first gear 4. The number of the first gears 4 is four. Every two adjacent first gears 4 are meshed and connected, and the outermost first gear 4 is meshed and connected with a tooth plate 37. The outer side of the top of the first bracket 11 is fixedly connected to the first motor 13, and the output shaft of the first motor 13 is fixedly connected to the outermost first gear 4. The inner surface of the tooth plate 37 is provided with a slide groove 27. The slide groove 27 The inner side is slidably connected to the slider 21, the slider 21 is fixedly connected to the upper end of the outer side of the casing 1, and the upper ends of the left and right sides of the casing 1 are fixedly connected to the third bracket 23. The outer side of the inner surface of the third bracket 23 is movably connected to the second gear 22, and the second gear 22 is meshed with the tooth plate 37. The bottom of the second gear 22 is fixedly connected to the fourth bracket 26, the outer side of the first stator 25 is fixedly connected to the first sleeve 36, the first sleeve 36 is fixedly connected to the bottom of the fourth bracket 26, and the output shaft of the second motor 7 is fixedly connected to the first fan blade 12.

[0033] A method for using a multifunctional mounted high-altitude individual reconnaissance drone comprises the following steps:

[0034] A. The external second wireless signal transceiver controls the rotation of the third motor 33 to drive the HD camera 28 to rotate horizontally, and controls the rotation of the fourth motor 30 to drive the HD camera 28 to adjust the tilt. The HD camera 28 can transmit the shooting results through the first wireless signal transceiver 31;

[0035] B. When the second motor 7 rotates, it can drive the first rotor 24 to rotate through the single-sided toothed synchronous belt, and with the cooperation of the first stator 25, it can generate electrical energy and store the electrical energy in the battery 32, thereby achieving the purpose of self-generating electricity during flight;

[0036] C. During the drone's launch, the limiting teeth 15, limiting rod 16, fixing block 17, and second spring 18 cooperate to keep the second blades 14 rotating in one direction. The conductive slip ring 10 cooperates to keep the wind from blowing the second blades 14 to rotate, thereby driving the second rotor 20 to rotate. The second stator 19 cooperates to generate electrical energy, which is stored in the battery 32, thereby achieving the purpose of wind power generation.

[0037] D. When the drone lands, the buffer rod 2, the pad 9, the first spring 34 and the damping shock absorber 35 can buffer the impact force, thereby improving the safety during landing;

[0038] E. Controlling the first motor 13 to rotate can drive the outermost first gear 4 to rotate, and drive the other first gears 4 to rotate synchronously. With the cooperation of the slider 21 and the slide groove 27, the tooth plate 37 can be driven to move synchronously, and the second gear 22 can be driven to rotate, so that the fourth bracket 26 can be folded and stored to reduce the overall volume.

[0039] While embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions, and variations may be made to these embodiments without departing from the principles and spirit of the invention, and that the scope of the invention is defined by the appended claims and their equivalents.

Claims

1. A multifunctional mounted high-altitude individual reconnaissance drone, comprising a housing (1) and a fourth bracket (26), characterized in that: A first bracket (11) is fixedly connected to one side of the top of the housing (1), and a conductive slip ring (10) is fixedly connected to the top of the first bracket (11), a movable end of the conductive slip ring (10) is fixedly connected to the second bracket (5), and the upper end of the inner surface of the second bracket (5) is movably connected to the second fan blade (14), the end of the second fan blade (14) is fixedly connected to the second rotor (20), and a second stator (19) is provided on the outer side of the second rotor (20), the outer side of the bottom of the fourth bracket (26) is fixedly connected to the second motor (7), the output shaft of the second motor (7) is connected to the first rotor (24) through a single-sided toothed synchronous belt transmission, and a first stator (25) is provided on the outer side of the first rotor (24).

2. The multifunctional mounted high-altitude individual reconnaissance drone according to claim 1, characterized in that: The front and rear ends of the top of the housing (1) are both fixedly connected to a third sleeve (3); the top of the inner cavity of the third sleeve (3) is fixedly connected to a first spring (34) and a damping shock absorber (35); the first spring (34) is located outside the damping shock absorber (35); the bottoms of the first spring (34) and the damping shock absorber (35) are fixedly connected to a buffer rod (2); and the bottom of the buffer rod (2) is fixedly connected to a cushion block (9).

3. The multifunctional mounted high-altitude individual reconnaissance drone according to claim 1, characterized in that: A third motor (33) is fixedly connected to the middle end of the bottom of the housing (1), an output shaft of the third motor (33) is fixedly connected to a fifth bracket (29), a fourth motor (30) is fixedly connected to the outer side of the fifth bracket (29), and an output shaft of the fourth motor (30) is fixedly connected to a high-definition camera (28).

4. The multifunctional high-altitude individual reconnaissance drone according to claim 1, characterized in that: The top of the inner cavity of the housing (1) is fixedly connected to a battery (32), the bottom of the inner cavity of the housing (1) is fixedly connected to a first wireless signal transceiver (31), and a charging socket (8) is provided at the bottom of the housing (1).

5. The multifunctional mounted high-altitude individual reconnaissance drone according to claim 1, characterized in that: The outer side of the second stator (19) is fixedly connected to a second sleeve (6), the second sleeve (6) is fixedly connected to the upper end of the outer side of the second bracket (5), and the outer surface of the second blade (14) is fixedly connected to the limiting teeth (15).

6. The multifunctional mounted high-altitude individual reconnaissance drone according to claim 1, characterized in that: The second bracket (5) is located on one side of the second fan blade (14) and is fixedly connected to a fixing block (17). The inner side of the fixing block (17) is movably connected to a limiting rod (16) via a second spring (18), and the lower end of the limiting rod (16) is movably connected to the surface of the second bracket (5).

7. The multifunctional mounted high-altitude individual reconnaissance drone according to claim 1, characterized in that: The top of the housing (1) is movably connected to a first gear (4), the number of the first gears (4) is four, every two adjacent first gears (4) are meshed and connected, and the outermost first gear (4) is meshed and connected to a toothed plate (37), the outer side of the top of the first bracket (11) is fixedly connected to a first motor (13), and the output shaft of the first motor (13) is fixedly connected to the outermost first gear (4).

8. The multifunctional high-altitude individual reconnaissance drone according to claim 1, characterized in that: The inner surface of the tooth plate (37) is provided with a slide groove (27), the inner side of the slide groove (27) is slidably connected to a slider (21), the slider (21) is fixedly connected to the upper end of the outer side of the housing (1), the upper ends of the left and right sides of the housing (1) are fixedly connected to the third bracket (23), the outer side of the inner surface of the third bracket (23) is movably connected to the second gear (22), and the second gear (22) is meshed with the tooth plate (37).

9. The multifunctional mounted high-altitude individual reconnaissance drone according to claim 1, characterized in that: The bottom of the second gear (22) is fixedly connected to a fourth bracket (26), the outer side of the first stator (25) is fixedly connected to a first sleeve (36), the first sleeve (36) is fixedly connected to the bottom of the fourth bracket (26), and the output shaft of the second motor (7) is fixedly connected to the first fan blade (12).

10. A method for using a multifunctional mounted high-altitude individual reconnaissance drone, characterized by: The following steps are involved: A. The third motor (33) is controlled to rotate by the external second wireless signal transceiver, which can drive the high-definition camera (28) to rotate horizontally, and the fourth motor (30) is controlled to rotate, which can drive the high-definition camera (28) to adjust the tilt, and the high-definition camera (28) can transmit the shooting result through the first wireless signal transceiver (31); B. When the second motor (7) rotates, the first rotor (24) can be driven to rotate through the single-sided toothed synchronous belt, and in cooperation with the first stator (25), electric energy can be generated and stored in the battery (32), thereby achieving the purpose of self-generating electricity during flight; C. During the process of the drone taking off, the second blade (14) is always rotated in one direction under the cooperation of the limiting tooth (15), the limiting rod (16), the fixing block (17) and the second spring (18). The wind force is always blown to rotate the second blade (14) under the cooperation of the conductive slip ring (10), thereby driving the second rotor (20) to rotate. Electric energy is generated under the cooperation of the second stator (19) and stored in the battery (32), thereby achieving the purpose of wind power generation. D. When the UAV lands, the buffer rod (2), the pad (9), the first spring (34) and the damping shock absorber (35) can buffer the impact force, thereby improving the safety during landing; E. Controlling the first motor (13) to rotate can drive the outermost first gear (4) to rotate, and drive the other first gears (4) to rotate synchronously, and under the cooperation of the slider (21) and the slide groove (27), can drive the tooth plate (37) to move synchronously, and can drive the second gear (22) to rotate, so that the fourth bracket (26) can be folded and stored to reduce the overall volume.

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