Electronic communication unmanned aerial vehicle for complex environment monitoring

Abstract

The invention relates to the field of unmanned aerial vehicles, and discloses an electronic communication unmanned aerial vehicle for complex environment monitoring, the electronic communication unmanned aerial vehicle comprises an unmanned aerial vehicle body, the upper surface of the unmanned aerial vehicle body is fixedly connected with a fixed plate, the upper surface of the fixed plate is fixedly connected with rotating seats, and the interiors of the plurality of rotating seats are rotatably connected with main antennas; a first rotating ring is fixedly connected to the upper end of the outer surface of the main antenna, an adjusting assembly is fixedly connected to the center of the fixing plate, a wind-resistant assembly is arranged outside the main antenna, a first wing arm is fixedly connected to the outer side of the unmanned aerial vehicle body, and a telescopic assembly is arranged on the outer surface of the first wing arm. A first carrying plate is mounted in the unmanned aerial vehicle body. The angle of the main antenna is changed and signal receiving is enhanced through extension or contraction of the electric telescopic rod and cooperation of the rotating ring and the connecting rod; when the main antenna fails, the emergency antenna increases the contact range with the base station, ensures communication, and improves the reliability of the unmanned aerial vehicle in a complex communication environment.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles, and specifically to an electronic communication unmanned aerial vehicle for complex environment monitoring. Background Art

[0002] In the field of complex environment monitoring today, unmanned aerial vehicles play an increasingly important role, especially electronic communication unmanned aerial vehicles. It is widely used in many aspects such as geographical mapping, environmental monitoring, disaster warning, etc. However, there are many problems with existing electronic communication unmanned aerial vehicles when performing complex environment monitoring tasks.

[0003] In terms of communication, obstacles in complex environments are likely to block signals, resulting in communication interruption or unstable signals. The existing antenna designs of unmanned aerial vehicles are difficult to effectively cope with, and cannot ensure a stable communication connection; in terms of flight, in narrow spaces, the wings of unmanned aerial vehicles are easily damaged by collisions, and their sizes are difficult to flexibly adjust to adapt to different space environments; in terms of equipment protection and data collection, vibrations and interferences during flight will affect the accuracy of monitoring equipment, and the existing collection components have complex structures and low collection efficiency, unable to meet the needs of efficient data collection. These problems limit the application effect and monitoring accuracy of electronic communication unmanned aerial vehicles in complex environment monitoring. Summary of the Invention

[0004] Aiming at the deficiencies of the prior art, the present invention provides an electronic communication unmanned aerial vehicle for complex environment monitoring, which solves the problems that the communication signal of the unmanned aerial vehicle is easily blocked in complex environments, the unmanned aerial vehicle is difficult to cross in narrow spaces, and the monitoring equipment is easily interfered during flight.

[0005] To achieve the above objectives, the present invention is realized through the following technical solutions: An electronic communication unmanned aerial vehicle for complex environment monitoring, including an unmanned aerial vehicle body. A fixed plate is fixedly connected to the upper surface of the unmanned aerial vehicle body. A rotating seat is fixedly connected to the upper surface of the fixed plate. A main antenna is rotatably connected inside a plurality of the rotating seats. A first rotating ring is fixedly connected to the upper end of the outer surface of the main antenna. An adjusting component is fixedly connected to the center of the fixed plate. An anti-wind component is arranged outside the main antenna. A first wing arm is fixedly connected to the outside of the unmanned aerial vehicle body. A telescopic component is arranged on the outer surface of the first wing arm. A first mounting plate is installed inside the unmanned aerial vehicle body. A mounting rack is slidably connected to the outer surface of the first mounting plate. A protection component is arranged inside the mounting rack. A second mounting plate is installed inside the unmanned aerial vehicle body. The second mounting plate is located below the mounting rack. A first motor is installed inside the second mounting plate. A wire collecting wheel is fixedly connected to the output end of the first motor. A thin rope is fixedly connected to the inside of the wire collecting wheel. The wire collecting wheel is fixedly connected to a collecting component through the thin rope.

[0006] Preferably, the adjusting assembly includes an electric telescopic rod which is fixedly connected to the center of the upper surface of the fixed plate. A second rotating ring is fixedly connected to the outer surface of the output end of the electric telescopic rod. A connecting rod is rotatably connected between the first rotating ring and the second rotating ring. An emergency antenna is fixedly connected to the top of the output end of the electric telescopic rod.

[0007] Preferably, the wind resistance assembly includes a wind resistance net which is fixedly connected to the edge of the upper surface of the fixed plate. The wind resistance net surrounds the main antenna and the emergency antenna. Ventilation holes are formed in the outer surface of the wind resistance net, and the outer surface of the wind resistance net is streamlined.

[0008] Preferably, the telescopic assembly includes a first mounting ring which is fixedly connected to the outer surface of the first wing arm. A second motor is installed inside the first mounting ring. A threaded rod is fixedly connected to the output end of the second motor. The first mounting ring is rotatably connected to a second mounting ring through the threaded rod. A second wing arm is fixedly connected inside the second mounting ring. A wing is installed at one end of the second wing arm. A limiting rod is slidably connected between the first mounting ring and the second mounting ring.

[0009] Preferably, the protection assembly includes an air inlet groove which is formed in the outer surface of the mounting rack. A partition plate is fixedly connected inside the mounting rack. A plurality of partition plates are evenly distributed inside the mounting rack. Air inlet holes are formed in the outer surface of the partition plate. A filter screen is installed inside the air inlet groove. A shock absorption mechanism is slidably connected to the lower end of the partition plate.

[0010] Preferably, the shock absorption mechanism includes a shock absorption plate which is slidably connected to the lower surface of the partition plate. A spring is fixedly connected to the lower surface of the shock absorption plate. The shock absorption plate is fixedly connected to the inner surface of the mounting rack through the spring.

[0011] Preferably, the collection assembly includes a gravity ball which is fixedly connected to one end of the thin string. A control ring and a clamping ring are slidably connected to the outer surface of the thin string. The control ring is located between the gravity ball and the clamping ring. A clamping arm is rotatably connected inside the clamping ring. A control rod is fixedly connected between the control ring and the clamping arm.

[0012] Preferably, a landing gear is installed at the lower end of the UAV body. The landing gear surrounds the mounting rack. A second carrying plate is fixedly connected inside the landing gear.

[0013] Preferably, an extension plate is fixedly connected to the outer surface of the landing gear. A buffer assembly is fixedly connected to the lower end of the landing gear.

[0014] Preferably, the buffer assembly includes a landing board 1, the landing board 1 is fixedly connected to the lower end of the landing gear, the lower surface of the landing board 1 is fixedly connected to an airbag, and the landing board 1 is fixedly connected to a landing board 2 through the airbag.

[0015] The present invention provides an electronic communication drone for complex environment monitoring. It has the following beneficial effects:

[0016] 1. The adjustment component in the present invention can adjust the main antenna angle and the emergency antenna height according to the communication environment. By extending or shortening the electric telescopic rod, cooperating with the rotating ring and the connecting rod, the main antenna angle is changed to enhance signal reception; when the main antenna fails, the emergency antenna is raised to increase the contact range with the base station, thereby ensuring communication and improving the reliability of the drone in complex communication environments.

[0017] 2. The present invention utilizes telescopic components to enable the UAV to adapt to different space environments. In a narrow space, the telescopic components are activated to retract the wings, reduce the lateral size, avoid collision, and facilitate take-off; in an open area, the reverse operation is performed to unfold the wings, increase lift, improve flight stability and controllability, and enhance the environmental adaptability of the UAV.

[0018] 3. The present invention effectively protects the monitoring equipment with the help of protective components and shock-absorbing mechanisms. The air is filtered by the air inlet slots and filters, the partition plate buffers the wind pressure, and the spring of the shock-absorbing mechanism absorbs vibration, which reduces interference with the equipment and ensures stable operation of the monitoring equipment during flight, improves the accuracy of data monitoring, and ensures the smooth progress of complex environment monitoring tasks. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 is a three-dimensional diagram of the drone of the present invention;

[0020] Figure 2 A bottom view of the device of the present invention;

[0021] Figure 3 is a schematic diagram of the regulating component in the present invention;

[0022] Figure 4 An internal diagram for adjustment in the present invention;

[0023] Figure 5 is a schematic diagram of the mounting frame in the present invention;

[0024] Figure 6 is a schematic diagram of a protection component in the present invention;

[0025] Figure 7 is a schematic diagram of a telescopic assembly in the present invention;

[0026] Figure 8 It is a schematic diagram of the acquisition component in the present invention.

[0027] Among them, 1. UAV body; 2. Fixing plate; 3. Rotating seat; 4. Main antenna; 5. Rotating ring 1; 6. Adjustment component; 7. Wind-resistant component; 8. Wing arm 1; 9. Telescopic component; 10. Carrying plate 1; 11. Mounting rack; 12. Protection component; 13. Carrying plate 2; 14. Motor 1; 15. Wire collection wheel; 16. Thin rope; 17. Collection component; 601. Electric telescopic rod; 602. Rotating ring 2; 603. Connecting rod; 604. Emergency antenna; 701. Wind-resistant net; 702. Ventilation hole; 901. Mounting ring 1; 902. Motor 2; 9 03, threaded rod; 904, mounting ring 2; 905, wing arm 2; 906, wing; 907, limit rod; 1201, air inlet slot; 1202, partition plate; 1203, air inlet hole; 1204, filter; 20, shock-absorbing mechanism; 201, shock-absorbing plate; 202, spring; 1701, gravity ball; 1702, control ring; 1703, clamping ring; 1704, clamping arm; 1705, control rod; 18, landing gear; 1801, expansion plate; 19, buffer assembly; 1901, landing board 1; 1902, airbag; 1903, landing board 2. DETAILED DESCRIPTION

[0028] The following will be combined with the drawings in the specification of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. 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 creative work are within the scope of protection of the present invention.

[0029] Please see attached Figure 1 -Attached Figure 8 The embodiment of the present invention provides an electronic communication drone for complex environment monitoring, including a drone body 1, a fixing plate 2 is fixedly connected to the upper surface of the drone body 1, a rotating seat 3 is fixedly connected to the upper surface of the fixing plate 2, a main antenna 4 is rotatably connected inside the plurality of rotating seats 3, a rotating ring 5 is fixedly connected to the upper end of the outer surface of the main antenna 4, an adjustment component 6 is fixedly connected to the center of the fixing plate 2, a wind-resistant component 7 is arranged outside the main antenna 4, a wing arm 8 is fixedly connected to the outer side of the drone body 1, and the outer surface of the wing arm 8 is arranged A telescopic component 9 is provided, a carrying plate 10 is installed inside the UAV body 1, and the outer surface of the carrying plate 10 is slidably connected to the mounting frame 11, and a protection component 12 is arranged inside the mounting frame 11, and a carrying plate 2 13 is installed inside the UAV body 1, and the carrying plate 2 13 is located below the mounting frame 11, and a motor 14 is installed inside the carrying plate 2 13, and the output end of the motor 14 is fixedly connected to a collection wheel 15, and the inside of the collection wheel 15 is fixedly connected to a thin rope 16, and the collection wheel 15 is fixedly connected to a collection component 17 through the thin rope 16.

[0030] Please refer to the attached Figure 3 and the attached Figure 4 , the adjusting assembly 6 includes an electric telescopic rod 601. The electric telescopic rod 601 is fixedly connected to the center of the upper surface of the fixed plate 2. A second rotating ring 602 is fixedly connected to the outer surface of the output end of the electric telescopic rod 601. A connecting rod 603 is rotatably connected between the first rotating ring 5 and the second rotating ring 602. An emergency antenna 604 is fixedly connected to the top of the output end of the electric telescopic rod 601.

[0031] Please refer to the attached Figure 3 , the wind resistance assembly 7 includes a wind resistance net 701. The wind resistance net 701 is fixedly connected to the edge of the upper surface of the fixed plate 2. The wind resistance net 701 surrounds the main antenna 4 and the emergency antenna 604. Ventilation holes 702 are formed on the outer surface of the wind resistance net 701, and the outer surface of the wind resistance net 701 is streamlined.

[0032] In this embodiment, during the flight of the drone, in order to ensure the stability of electronic communication, it is necessary to adjust the angle and height of the antenna according to different environmental and mission requirements. When it is necessary to adjust the angle of the main antenna 4, the electric telescopic rod 601 starts to work. If the electric telescopic rod 601 extends, its output end moves upward, driving the second rotating ring 602 to move upward. Since the first rotating ring 5 and the second rotating ring 602 are rotatably connected by the connecting rod 603, the upward movement of the second rotating ring 602 will push the first rotating ring 5 through the connecting rod 603, causing the main antenna 4 to rotate around the rotating seat 3, and the angle of the main antenna 4 gradually increases. On the contrary, when the electric telescopic rod 601 contracts, the second rotating ring 602 moves downward, pulling the first rotating ring 5 through the connecting rod 603, and the main antenna 4 rotates in the reverse direction around the rotating seat 3, and the angle decreases; at the same time, the emergency antenna 604 is fixed to the top of the output end of the electric telescopic rod 601. As the electric telescopic rod 601 expands and contracts, the height of the emergency antenna 604 will also change. When the main antenna 4 fails or the communication signal is severely interfered, raising the emergency antenna 604 can increase its contact range with external communication base stations, attempt to establish a new communication connection, provide additional protection for the communication of the drone, and enhance the emergency communication ability of the drone in case of emergencies; when the drone is flying, it will inevitably be affected by wind. The wind resistance net 701 surrounds the main antenna 4 and the emergency antenna 604, playing an important protective role. When the wind blows towards the drone, due to the streamlined outer surface of the wind resistance net 701, the wind can flow smoothly along the surface of the wind resistance net 701, reducing the direct impact of the wind on the antenna; at the same time, the ventilation holes 702 formed on the surface of the wind resistance net 701 also play a key role. Part of the wind will pass through the wind resistance net 701 through the ventilation holes 702, further reducing the wind force acting on the surface of the antenna. In this way, the wind interference on the main antenna 4 and the emergency antenna 604 during flight is greatly reduced, ensuring the stability of the antenna.

[0033] Please refer to the attached Figure 7 , the telescopic component 9 includes a first mounting ring 901, the first mounting ring 901 is fixedly connected to the outer surface of the first wing arm 8, a second motor 902 is installed inside the first mounting ring 901, the output end of the second motor 902 is fixedly connected to a threaded rod 903, the first mounting ring 901 is rotationally connected to a second mounting ring 904 through the threaded rod 903, a second wing arm 905 is fixedly connected inside the second mounting ring 904, a wing 906 is installed at one end of the second wing arm 905, and a limiting rod 907 is slidably connected between the first mounting ring 901 and the second mounting ring 904.

[0034] In this embodiment, if the environment where the drone is located is relatively narrow, in order to prevent the wing 906 from colliding and being damaged in a narrow space, the operator can control the second motor 902 to start. The output shaft of the second motor 902 drives the fixedly connected threaded rod 903 to start rotating. Since the first mounting ring 901 and the second mounting ring 904 are rotationally connected through the threaded rod 903, and the position of the first mounting ring 901 fixed on the first wing arm 8 is relatively fixed, as the threaded rod 903 rotates, the second mounting ring 904 will move along the axial direction of the threaded rod 903. At this time, the limiting rod 907 plays a key guiding and limiting role. It ensures that the second mounting ring 904 can only slide along the straight line direction between it and the first mounting ring 901, preventing the second mounting ring 904 from rotating with the threaded rod 903, making the entire telescopic process stable and orderly. When the second mounting ring 904 moves, it drives the fixedly connected second wing arm 905 to contract towards the direction close to the first wing arm 8, thereby shortening the distance between the wing 906 and the drone body 1, reducing the overall lateral dimension of the drone, and facilitating its smooth takeoff in a narrow space; when the drone flies to an open area, in order to obtain better flight performance and stability, the operator controls the second motor 902 to rotate in the reverse direction again, the threaded rod 903 rotates in the reverse direction accordingly, pushing the second mounting ring 904 to move away from the first wing arm 8 along the limiting rod 907, the second wing arm 905 is pushed out, the distance between the wing 906 and the drone body 1 increases, and the deployed wing can provide greater lift, making the drone fly more stably, and at the same time enhancing the controllability and maneuverability of the drone.

[0035] Please refer to the attached Figure 6 , the protection component 12 includes an air inlet groove 1201, the air inlet groove 1201 is opened on the outer surface of the mounting rack 11, a partition plate 1202 is fixedly connected inside the mounting rack 11, a plurality of partition plates 1202 are evenly distributed inside the mounting rack 11, air inlet holes 1203 are opened on the outer surface of the partition plate 1202, a filter screen 1204 is installed inside the air inlet groove 1201, and a shock absorption mechanism 20 is slidably connected to the lower end of the partition plate 1202.

[0036] In this embodiment, the filter screen 1204 in the air inlet groove 1201 preliminarily filters the outside air and reduces the wind pressure at the same time. The multiple partition plates 1202 inside divide the internal space into multiple small spaces. At the same time, a buffer space is formed to reduce the impact of the reduced wind force on the internal equipment.

[0037] Please refer to the appendix Figure 6 , the shock absorption mechanism 20 includes a shock absorption plate 201. The shock absorption plate 201 is slidably connected to the lower surface of the partition plate 1202. A spring 202 is fixedly connected to the lower surface of the shock absorption plate 201. The shock absorption plate 201 is fixedly connected to the inner surface of the mounting rack 11 through the spring 202.

[0038] In this embodiment, the spring 202 is used to absorb external vibrations and reduce the interference to the monitoring equipment above the shock absorption plate 201.

[0039] Please refer to the appendix Figure 8 , the acquisition component 17 includes a gravity ball 1701. The gravity ball 1701 is fixedly connected to one end of a thin rope 16. A control ring 1702 and a clamping ring 1703 are slidably connected to the outer surface of the thin rope 16. The control ring 1702 is located between the gravity ball 1701 and the clamping ring 1703. A clamping arm 1704 is rotatably connected inside the clamping ring 1703. A control rod 1705 is fixedly connected between the control ring 1702 and the clamping arm 1704.

[0040] In this embodiment, when the drone needs to perform data acquisition, the motor one 14 inside the mounting plate two 13 starts, drives the wire reel 15 to rotate. The wire reel 15 rotates and releases the thin rope 16. The acquisition component 17 moves downward under the action of gravity. At this time, the gravity ball 1701 is affected by gravity and drives the entire acquisition component 17 to descend. At the same time, the clamping arm 1704 is in an open state under its own gravity to contact the target acquisition object. When the clamping arm 1704 contacts the target acquisition object, the motor one 14 starts in the reverse direction to recover the thin rope 16. As the thin rope 16 is continuously recovered, the gravity ball 1701 moves upward. Since the control ring 1702 is connected to the gravity ball 1701 and can slide on the thin rope 16, the upward movement of the gravity ball 1701 drives the control ring 1702 to rise synchronously. During the rising process of the control ring 1702, the clamping arm 1704 is pushed to rotate around the rotation point of the clamping ring 1703 through the fixedly connected control rod 1705, so that the clamping arm 1704 gradually closes, thereby tightly grasping the target acquisition object, realizing the initial opening of the clamping arm 1704 by using gravity, without the need for an additional power device, simplifying the structure and reducing the energy consumption.

[0041] Please refer to the appendix Figure 2 , the landing gear 18 is installed at the lower end of the drone body 1. The landing gear 18 surrounds the mounting rack 11. The mounting plate two 13 is fixedly connected inside the landing gear 18.

[0042] In this embodiment, the landing gear 18 surrounds the monitoring equipment inside the UAV, providing an external protective armor and more modification space.

[0043] Please refer to the appendix Figure 2 , an extension plate 1801 is fixedly connected to the outer surface of the landing gear 18, and a buffer assembly 19 is fixedly connected to the lower end of the landing gear 18.

[0044] In this embodiment, the establishment of the extension plate 1801 facilitates the installation of other monitoring equipment on the UAV, improving the practicability of the UAV.

[0045] Please refer to the appendix Figure 2 , the buffer assembly 19 includes a first landing plate 1901, the first landing plate 1901 is fixedly connected to the lower end of the landing gear 18, an airbag 1902 is fixedly connected to the lower surface of the first landing plate 1901, and a second landing plate 1903 is fixedly connected to the first landing plate 1901 through the airbag 1902.

[0046] In this embodiment, the airbag 1902 between the first landing plate 1901 and the second landing plate 1903 can absorb the impact force during landing and protect the equipment inside the UAV.

[0047] Working principle: When in use, first ensure that all components of the drone are properly connected and in good working condition. Before takeoff, if the communication environment is expected to be complex, the adjustment component 6 can be activated according to the needs. The electric telescopic rod 601 extends or retracts, driving the emergency antenna 604 to rise and fall. At the same time, through the cooperation of the first rotating ring 5, the second rotating ring 602 and the connecting rod 603, the angle of the main antenna 4 is adjusted to enhance the communication signal reception ability; the wind-resistant net 701 of the wind-resistant component 7 outside the antenna can reduce the influence of wind on the antenna during flight, and the ventilation holes 702 and the streamlined outer surface can not only reduce wind resistance but also protect the antenna; during flight, if it is necessary to pass through a narrow space, the telescopic component is activated, and the motor two 902 drives the threaded rod 903 to rotate, so that the second mounting ring 904, the wing arm two 905 and the wing 906 contract or expand to adjust the overall size of the drone; at the same time, the data monitoring process is accompanied during flight. The monitoring device is located in the mounting rack 11, and the internal protection component 12 can protect the monitoring device. The air inlet groove 1201, the filter screen 1204, the partition plate 1202 and the shock absorption mechanism 20 work together to filter the air, reduce interference to the device and buffer vibrations. When data collection is required, the motor one 14 is started to drive the wire reel 15 to rotate, and the collection component 17 is lowered through the thin rope 16. Under the action of gravity, the clamping arms 1704 are opened. After the clamping arms 1704 touch the material, the motor one 14 starts to retract the thin rope 16. The gravity ball 1701 at one end of the thin rope 16 causes the control ring 1702 to rise. Under the action of the control rod 1705, the clamping arms 1704 are closed to achieve the grasping or detection of the target object; if the drone needs to land, the airbag 1902 of the buffer component 19 can effectively reduce the landing impact force and protect the drone and internal devices.

[0048] Although the embodiments of the present invention have been shown and described, for those of ordinary skill in the art, it can be understood that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An electronic communication drone for complex environment monitoring, characterized in that: The invention comprises an unmanned aerial vehicle body (1), wherein a fixing plate (2) is fixedly connected to the upper surface of the unmanned aerial vehicle body (1), a rotating seat (3) is fixedly connected to the upper surface of the fixing plate (2), a main antenna (4) is rotatably connected to the inside of a plurality of the rotating seats (3), a rotating ring (5) is fixedly connected to the upper end of the outer surface of the main antenna (4), an adjustment component (6) is fixedly connected to the center of the fixing plate (2), a wind-resistant component (7) is arranged outside the main antenna (4), a wing arm (8) is fixedly connected to the outer side of the unmanned aerial vehicle body (1), a telescopic component (9) is arranged on the outer surface of the wing arm (8), and the unmanned aerial vehicle body (1) A carrying plate (10) is installed inside the unmanned aerial vehicle (1), the outer surface of the carrying plate (10) is slidably connected to a mounting frame (11), a protection component (12) is arranged inside the mounting frame (11), a carrying plate (13) is installed inside the unmanned aerial vehicle (1), the carrying plate (13) is located below the mounting frame (11), a motor (14) is installed inside the carrying plate (13), the output end of the motor (14) is fixedly connected to a wire collection wheel (15), the inside of the wire collection wheel (15) is fixedly connected to a thin rope (16), and the wire collection wheel (15) is fixedly connected to a collection component (17) via the thin rope (16).

2. The electronic communication drone for complex environment monitoring according to claim 1, characterized in that: The adjustment component (6) comprises an electric telescopic rod (601), the electric telescopic rod (601) is fixedly connected to the center of the upper surface of the fixed plate (2), the outer surface of the output end of the electric telescopic rod (601) is fixedly connected to a rotating ring 2 (602), a connecting rod (603) is rotatably connected between the rotating ring 1 (5) and the rotating ring 2 (602), and an emergency antenna (604) is fixedly connected to the top of the output end of the electric telescopic rod (601).

3. The electronic communication drone for complex environment monitoring according to claim 2, characterized in that: The wind-resistant component (7) comprises a wind-resistant net (701), wherein the wind-resistant net (701) is fixedly connected to the edge of the upper surface of the fixing plate (2), and the wind-resistant net (701) surrounds the main antenna (4) and the emergency antenna (604). The outer surface of the wind-resistant net (701) is provided with ventilation holes (702), and the outer surface of the wind-resistant net (701) is streamlined.

4. The electronic communication drone for complex environment monitoring according to claim 1, characterized in that: The telescopic assembly (9) comprises a mounting ring (901) which is fixedly connected to the outer surface of the wing arm (8); a motor (902) is installed inside the mounting ring (901); a threaded rod (903) is fixedly connected to the output end of the motor (902); the mounting ring (901) is rotatably connected to the mounting ring (904) via the threaded rod (903); a wing arm (905) is fixedly connected inside the mounting ring (904); a wing (906) is installed at one end of the wing arm (905); and a limit rod (907) is slidably connected between the mounting ring (901) and the mounting ring (904).

5. The electronic communication drone for complex environment monitoring according to claim 1, characterized in that: The protection component (12) comprises an air inlet groove (1201), wherein the air inlet groove (1201) is provided on the outer surface of the mounting frame (11), a partition plate (1202) is fixedly connected to the inside of the mounting frame (11), a plurality of partition plates (1202) are evenly distributed inside the mounting frame (11), an air inlet hole (1203) is provided on the outer surface of the partition plate (1202), a filter screen (1204) is installed inside the air inlet groove (1201), and a shock absorbing mechanism (20) is slidably connected to the lower end of the partition plate (1202).

6. The electronic communication drone for complex environment monitoring according to claim 5, characterized in that: The shock absorbing mechanism (20) comprises a shock absorbing plate (201), the shock absorbing plate (201) being slidably connected to the lower surface of the partition plate (1202), the lower surface of the shock absorbing plate (201) being fixedly connected to a spring (202), and the shock absorbing plate (201) being fixedly connected to the inner surface of the mounting frame (11) via the spring (202).

7. The electronic communication drone for complex environment monitoring according to claim 1, characterized in that: The collection component (17) comprises a gravity ball (1701), wherein the gravity ball (1701) is fixedly connected to one end of the thin rope (16), and a control ring (1702) and a clamping ring (1703) are slidably connected to the outer surface of the thin rope (16), wherein the control ring (1702) is located between the gravity ball (1701) and the clamping ring (1703), and a clamping arm (1704) is rotatably connected inside the clamping ring (1703), and a control rod (1705) is fixedly connected between the control ring (1702) and the clamping arm (1704).

8. The electronic communication drone for complex environment monitoring according to claim 1, characterized in that: A landing gear (18) is installed at the lower end of the drone body (1), the landing gear (18) surrounds the mounting frame (11), and the second mounting plate (13) is fixedly connected to the inside of the landing gear (18).

9. The electronic communication drone for complex environment monitoring according to claim 8, characterized in that: The outer surface of the landing gear (18) is fixedly connected to the expansion plate (1801), and the lower end of the landing gear (18) is fixedly connected to the buffer assembly (19).

10. The electronic communication drone for complex environment monitoring according to claim 9, characterized in that: The buffer assembly (19) comprises a landing board 1 (1901), wherein the landing board 1 (1901) is fixedly connected to the lower end of the landing gear (18), an air bag (1902) is fixedly connected to the lower surface of the landing board 1 (1901), and the landing board 1 (1901) is fixedly connected to a landing board 2 (1903) via the air bag (1902).

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