Unmanned aerial vehicle loading structure and unmanned aerial vehicle

Abstract

The application discloses a kind of unmanned vehicle loading structure and unmanned vehicle, it is related to unmanned vehicle technical field.The application includes: fixed seat frame, fixed seat frame is constructed with parking slot, equipment box is fixedly connected with parking slot side;Shield, including sliding installation in fixed seat frame and with equipment box opposite interface sliding cover, fixed seat frame is provided with for driving sliding cover sliding push member;Telescopic frame, fixed seat frame is constructed with loading slot in parking slot, telescopic frame includes the connecting seat being connected in fixed seat frame bottom and being located in the both sides of loading slot, the connecting seat is all hinged with bending connecting rod, the other end between bearing disc of bending connecting rod is connected.The application is installed on vehicle sunroof by fixed seat frame, can realize the in-vehicle goods loading operation of unmanned vehicle, need not personnel to carry goods and unmanned vehicle to vehicle outside, improve loading efficiency, increase the range of usable environment of unmanned vehicle.

Description

Technical Field

[0001] This invention relates to the field of unmanned aerial vehicle (UAV) technology, specifically to a UAV mounting structure and a UAV. Background Technology

[0002] With the rapid development of drone technology, its application in logistics, agriculture, surveying and mapping is becoming increasingly widespread. Medium and large drones can be used to load goods and transport them to designated locations. However, existing drones present several inconveniences when transporting goods. For example, when using medium and large drones outdoors, to ensure the safety of surrounding people, the drone and the goods to be transported must first be transported by vehicle to an open area, and then both the drone and the goods must be unloaded from the vehicle before transport can begin. This process is not only inefficient and time-consuming, but also impacts the operating environment.

[0003] Therefore, this invention proposes a drone mounting structure that can be installed on the top of a vehicle without the need for handling, and a drone using the structure. Summary of the Invention

[0004] The purpose of this invention is to provide a drone loading structure and a drone in order to solve the problems mentioned in the background art.

[0005] To achieve the above objectives, the present invention specifically adopts the following technical solution:

[0006] A drone mounting structure and a drone, comprising:

[0007] A fixed frame is provided, on which a stopping slot is constructed, and an equipment box is fixedly connected to one side of the stopping slot;

[0008] The protective cover includes a sliding cover that is slidably mounted on a fixed frame and is in contact with the equipment box, wherein the fixed frame is provided with a pusher for driving the sliding cover to slide.

[0009] The telescopic frame includes a loading slot located in the parking slot on the fixed seat frame. The telescopic frame includes connecting seats connected to the bottom of the fixed seat frame and located on both sides of the loading slot. Each connecting seat is hinged with a bent connecting rod, and the other end of the bent connecting rod is connected to a bearing plate.

[0010] An automatic lifting component is installed at the bottom of the fixed seat frame and is used to drive the carrier plate to move up and down.

[0011] Furthermore, the sliding cover has an opening at one horizontal end and a sliding post is constructed at the bottom corner of the opening end. The fixed seat frame is constructed with a horizontal sliding groove for sliding the sliding cover. An L-shaped sliding groove is constructed inside the horizontal sliding groove for guiding the sliding post to slide. When the sliding cover slides to the far end of the fixed seat frame, the top of the sliding cover is flush with the upper surface of the fixed seat frame.

[0012] Further, one end of the equipment box is configured as a circular arc surface and the other end is configured as a flat surface, and the flat end of the equipment box is configured with a stepped edge slot for plugging with the opening end of the sliding cover.

[0013] Further, the push member includes a first cylinder push rod hingedly connected in the fixed seat frame, and the output end of the first cylinder push rod is movably penetrated through the fixed seat frame and is hingedly mounted at the bottom side of the sealing end of the sliding cover.

[0014] Further, the bending connecting rod includes a long handle rod hingedly connected on the connecting seat, a short handle rod hingedly connected at the other end of the long handle rod, and a sliding frame hingedly connected at the other end of the short handle rod, and the opposite ends of the two sliding frames are horizontally slidably mounted in the bearing disc, and an extension rod is hingedly connected at one side of the long handle rod, and a limiting cross rod is slidably penetrated and mounted between the two extension rods.

[0015] Further, the automatic lifting member includes a second cylinder push rod hingedly mounted at the bottom of the fixed seat frame, and the output end of the second cylinder push rod is movably penetrated through the long handle rod and is hingedly connected at the edge of the bearing disc, and the bottom of the bearing disc is configured with a pulling handle.

[0016] A UAV, suitable for the UAV loading structure described above, comprising:

[0017] A body, four corners of the body are fixedly connected with wing rods, and rotating fan blades are mounted at the end of the wing rods.

[0018] A rope fixing member is mounted in the body and is used for stretching and binding goods, and the rope fixing member includes a mounting frame fixedly connected in the body, a partition plate is configured in the middle of the mounting frame, two winding rods are rotatably mounted in the mounting frame and are located on both sides of the partition plate, and a pull rope movably penetrated through the body is wound on the winding rods.

[0019] A detent member is arranged on the mounting frame and is used for fixing the position of the pull rope.

[0020] Further, spring legs are fixedly connected at the bottom of the wing rods, four column grooves for plugging with the spring legs are configured in the parking slot, and an inclined angle is configured at the edge of the column groove.

[0021] Further, the winding rod includes a rotating rod rotatably mounted in the mounting frame, a winding spring fixedly connected on the mounting frame is sleeved at one end of the rotating rod, a fixed ring is configured in the middle of the rotating rod, the pull rope is annular and one ring end is connected in the fixed ring, and the other ring end of the pull rope is movably penetrated through the bottom of the body.

[0022] Further, the clamping pieces include four U-shaped blocks fixedly connected in the mounting frame, the U-shaped blocks are wrapped on the pull rope, two U-shaped blocks on the same side of the spacing plate are slidably inserted with U-shaped extrusion plates, opposite sides of the two U-shaped extrusion plates are provided with racks penetrating the spacing plate, the spacing plate is rotatably provided with a positioning gear engaged with the two racks, and a driving motor for driving the positioning gear to rotate is fixedly installed on the mounting frame.

[0023] The beneficial effects of the present application are as follows:

[0024] 1、The fixed seat frame is installed on the vehicle sunroof, the unmanned aerial vehicle is parked on the top of the fixed seat frame, and is protected by the protective cover, safety is increased, when loading goods, the telescopic frame can be inserted into the vehicle interior, so that the goods are received, personnel do not need to get off the vehicle, only need to bundle the goods on the bottom of the unmanned aerial vehicle, the unmanned aerial vehicle can separate the goods from the vehicle through the loading slot, goods do not need to be carried, time and labor are saved, and loading efficiency is improved.

[0025] 2、The unmanned aerial vehicle is lifted from the roof of the vehicle, has a certain height, safety of surrounding personnel is ensured, and the environment range that the unmanned aerial vehicle can use is increased.

[0026] 3、The pull rope of the unmanned aerial vehicle is automatically retracted, and is fixed by using the clamping pieces, goods do not need to be manually bundled, only need to be sleeved on the goods, and operation is more convenient. BRIEF DESCRIPTION OF DRAWINGS

[0027] Figure 1 is a perspective view of the present application;

[0028] Figure 2 is a partial sectional view of the perspective view of the present application;

[0029] Figure 3 is a perspective view of another state of the present application;

[0030] Figure 4 is a partial sectional view of the perspective view of the fixed seat frame of the present application;

[0031] Figure 5 is a perspective view of the sliding cover of the present application;

[0032] Figure 6 is a perspective view of the telescopic frame of the present application;

[0033] Figure 7 is a perspective view of the present application Figure 6 half sectional view;

[0034] Figure 8 is a perspective view of the unmanned aerial vehicle of the present application;

[0035] Figure 9 is the rope cable fixing device of the present application Figure 8 is a perspective view of the rope cable fixing device of the present application

[0036] Figure 10 is the rope cable fixing device of the present application

[0037] Figure 11 is the rope cable fixing device of the present application

[0038] Fig. 1 is a fixed seat frame; 101, parking slot; 1011, column slot; 1012, bevel; 102, loading slot; 103, horizontal sliding slot; 104, L-shaped sliding slot; 2, equipment box; 201, step edge slot; 3, protective cover; 301, sliding cover; 3011, sliding column; 302, push member; 3021, air cylinder push rod one; 4, telescopic frame; 401, connecting seat; 402, bent connecting rod; 4021, long handle rod; 4022, short handle rod; 4023, sliding frame; 4024, extension rod; 4025, limiting cross rod; 403, bearing disc; 4031, pull handle; 5, automatic lifting member; 501, air cylinder push rod two; 6, machine body; 601, wing rod; 6011, spring foot; 602, rotating fan blade; 7, rope cable fixing device; 701, mounting frame; 702, spacer plate; 703, winding rod; 7031, rotating rod; 7032, winding spring; 7033, fixing ring; 704, pull rope; 8, clamping member; 801, U-shaped block; 802, U-shaped extruded plate; 803, rack; 804, positioning gear; 805, drive motor. DETAILED DESCRIPTION

[0039] In order to make the purpose, technical scheme and advantages of the embodiments of the present application more clear, the technical scheme in the embodiments of the present application will be described clearly and completely below with reference to the drawings in the embodiments of the present application.

[0040] As shown in Figures 1-7 and Figure 11 , one embodiment of the present application proposes a UAV loading structure, which comprises:

[0041] The fixed seat frame 1 is provided with a parking slot 101, and the equipment box 2 is fixedly connected to one side of the parking slot 101. The fixed seat frame 1 is mainly installed on the sunroof of an existing car or SUV vehicle. If it is a truck, a sunroof needs to be opened above the vehicle compartment, and the fixed seat frame 1 is installed above the sunroof of the vehicle compartment.

[0042] The protective cover 3 comprises a sliding cover 301 slidably mounted on the fixed seat frame 1 and connected with the equipment box 2, the fixed seat frame 1 is provided with a push member 302 for driving the sliding cover 301 to slide, the sliding cover 301 can be connected with the equipment box 2 to form a parking space between the sliding cover 301 and the fixed seat frame 1, which is mainly used for wrapping and protecting the unmanned aerial vehicle to avoid damage to the unmanned aerial vehicle during vehicle operation, thereby increasing safety, and the push member 302 is arranged to automatically open the sliding cover 301 without the need for manual external opening, so that personnel can always be in the vehicle to control the start and stop of the unmanned aerial vehicle, thereby increasing convenience.

[0043] The telescopic frame 4 is provided with a loading slot 102 in the parking groove 101 of the fixed seat frame 1, the telescopic frame 4 comprises a connecting seat 401 connected to the bottom of the fixed seat frame 1 and located on both sides of the loading slot 102, the connecting seat 401 is hingedly connected with a bent connecting rod 402, and the other end of the bent connecting rod 402 is connected with a bearing disc 403. It should be noted that the telescopic frame 4 is connected to the bottom of the fixed seat frame 1 and penetrates through the sunroof of the vehicle, when loading goods is needed, the bent connecting rod 402 is unfolded, at this time the bearing disc 403 is lowered, and personnel can directly place the goods on the bearing disc 403, and then the goods are bundled with the unmanned aerial vehicle, when the goods need to be transported, the sliding cover 301 is opened, and the unmanned aerial vehicle is started, so that the goods can pass through the loading slot 102 and be directly transported.

[0044] The automatic lifting member 5 is installed at the bottom of the fixed seat frame 1 and is used to drive the bearing disc 403 to move up and down, when loading goods is not needed, the bearing disc 403 can be driven to rise by the automatic lifting member 5, at this time the bent connecting rod 402 is folded, and the bearing disc 403 can completely block the loading slot 102 to ensure the airtightness of the vehicle as a whole.

[0045] It should be noted that the device is installed on the top of the vehicle and has a certain height from the ground, which can reduce the influence on the surrounding personnel when the unmanned aerial vehicle starts and stops, increase the application range of the use environment, and the loading structure can be installed on multiple vehicles to serve as a transportation path for the exchange of goods between vehicles, for example, scene one: when a vehicle loaded with the device transports goods, the oil level is insufficient during the journey, at this time, the vehicle loaded with the device can be combined with another vehicle loaded with the device, the unmanned aerial vehicles on the two vehicles take off at the same time, one is loaded with goods and the other is empty, and the two unmanned aerial vehicles exchange and stop on the fixed seat frame 1 after taking off, realizing dynamic transfer transportation without the need for personnel to carry, saving a lot of manpower and time, and improving convenience.

[0046] For example, Figures 2-5As shown, the specific motion trajectory of the sliding cover 301 is disclosed, the sliding cover 301 is open at one end, and the bottom corner of the open end is provided with a sliding column 3011, the fixed seat frame 1 is provided with a horizontal sliding groove 103 for sliding the sliding cover 301, and the horizontal sliding groove 103 is provided with an L-shaped sliding groove 104 for guiding the sliding of the sliding column 3011, when the sliding cover 301 slides to the end side of the fixed seat frame 1, the top of the sliding cover 301 is flush with the upper surface of the fixed seat frame 1, the horizontal sliding groove 103 can limit the sliding of the sliding cover 301, ensure that the sliding cover 301 always moves on the fixed seat frame 1, avoid disengagement, increase safety, and the L-shaped sliding groove 104 is used for sliding guide of the sliding column 3011 on the sliding cover 301, so that the sliding trajectory becomes L-shaped, that is, after sliding to the range above the parking groove 101, it can be inclined downward, until it is flush with the fixed seat frame 1, reduce the occupied space on the top of the vehicle, and at the same time, the opening of the sliding cover 301 is connected with the end of the fixed seat frame 1, reduces the airflow into, reduces air resistance, thereby reducing vehicle fuel consumption.

[0047] As shown in the figure, Figures 1-2 The specific structure of the equipment box 2 is disclosed, one end of the equipment box 2 is provided with a circular arc surface and the other end is provided with a plane, the plane end of the equipment box 2 is provided with a stepped edge groove 201 which is inserted with the opening end of the sliding cover 301, it should be noted that the inside of the equipment box 2 is mainly used for installing electronic control equipment, and the circular arc surface of the equipment box 2 is provided in the direction of the vehicle head, and the plane end is provided in the direction of the vehicle tail, the sliding cover 301 and the equipment box 2 can form a streamline after being connected, reduce air resistance, at the same time, in the process of vehicle driving, the equipment box 2 can be used as a gas flow resistance structure after the sliding cover 301 is opened, block the airflow of the unmanned aerial vehicle to a certain extent, so that the unmanned aerial vehicle can take off more stably from the parking groove 101, and the safety is guaranteed.

[0048] As shown in the figure, Figures 2-5As shown, the specific structure of the pusher 302 of the present application is disclosed, which realizes automatic push sliding cover 301, the pusher 302 includes a cylinder push rod one 3021 hinged at one end in the fixed seat frame 1, the output end of the cylinder push rod one 3021 is movably penetrated through the fixed seat frame 1 and hingedly installed at the bottom side of the sealing end of the sliding cover 301, it should be noted that the air pump structure of the cylinder push rod one 3021 is installed in the equipment box 2, the sliding cover 301 can be automatically pushed in the horizontal sliding groove 103 by the cylinder push rod one 3021, without human intervention, automatic operation, increase the convenience, ensure that the unmanned aerial vehicle can also be realized during the operation of the vehicle Take-off and landing operation, and the cylinder push rod one 3021 is connected to the tail end of the sliding cover 301, the sliding column 3011 is constructed at the front end of the sliding cover 301, the sliding column 3011 limits the front end of the sliding cover 301 in the L-shaped sliding groove 104, cooperates with the cylinder push rod one 3021, can fix the position of the sliding cover 301, further avoid the sliding cover 301 from separating, increase the safety.

[0049] As Figure 6The specific folding structure of the bending connecting rod 402 of the present invention is disclosed. The bending connecting rod 402 includes a long handle rod 4021 hinged to the connecting seat 401, a short handle rod 4022 hinged to the other end of the long handle rod 4021, and a sliding frame 4023 hinged to the other end of the short handle rod 4022. The opposite ends of the two sliding frames 4023 are horizontally slidably installed in the bearing plate 403. An extension rod 4024 is hinged to one side of the long handle rod 4021, and a limiting crossbar 4025 is slidably installed between the two extension rods 4024. It should be noted that the length of the long handle 4021 is greater than the length of the short handle 4022, and the distance that the short handle 4022 plus the slide frame 4023 can slide within the bearing plate 403 is greater than or equal to the length of the long handle 4021. The short handle 4022 includes a pivot hinged to the end of the long handle 4021, with short rods connected to both ends of the pivot. The other ends of the two short rods are hinged to the slide frame 4023 via a shaft. It should also be noted that the bottom edge of the loading slot 102 is constructed with a rectangular ring frame. When the bearing plate 4021... 3. During upward movement, the long handle 4021 gradually approaches the short handle 4022, thus entering the cavity between the two short handles and achieving folding, until the bearing plate 403 aligns with the rectangular ring frame, completing the closure of the bearing slot. At this point, the long handle 4021 and the short handle 4022 remain in a V-shape to facilitate subsequent unfolding. When the automatic lifting component 5 pushes the bearing plate 403 down to its lowest point, the long handle 4021 and the short handle 4022 still maintain an angle to facilitate subsequent... The folding operation is achieved by setting an extension rod 4024 and a limiting crossbar 4025. The limiting crossbar 4025 can slide between the extension rod 4024. The hinge points of the extension rod 4024 on the long handle 4021 are located on the same horizontal plane. The two ends of the limiting crossbar 4025 are equipped with ball stops to prevent detachment. This structure ensures that the flipping angles of the two long handles 4021 are always equal, thereby ensuring that the carrying plate 403 remains horizontal during the lifting process and ensuring safety when loading goods.

[0050] like Figures 6-7 As shown, the specific structure of the automatic lifting component 5 of the present invention is disclosed. The automatic lifting component 5 includes a cylinder push rod 501 hinged to the bottom of the fixed seat frame 1. The output end of the cylinder push rod 501 movably passes through the long handle 4021 and is hinged to the edge of the support plate 403. The bottom of the support plate 403 is provided with a pull handle 4031. It should be noted that the air pump structure of the cylinder push rod 501 is the same as that of the cylinder push rod 3021, which saves costs. The cylinder push rod 501 can push the support plate 403 to move up and down, thereby linking the bending connecting rod 402 to fold and store it, so as to reduce the space occupation of the device when it is not in use. The bending connecting rod 402 is tightly hinged and has a certain self-locking property when no external force is applied. With the cylinder push rod 501, the device can achieve autonomous positioning after folding without power drive, ensuring the safety of the device.

[0051] As Figures 8-10 shown, one embodiment of the present application proposes a UAV, comprising:

[0052] The body 6 is fixedly connected with wing rods 601 at four corners, and the end of the wing rod 601 is provided with a rotating fan blade 602, which comprises a rotating motor fixedly connected to the end of the wing rod 601 and a blade connected to the rotating motor.

[0053] The rope fixing part 7 is installed in the body 6 and used for stretching and binding goods, and comprises a mounting frame 701 fixedly connected in the body 6, a partition plate 702 is arranged in the middle of the mounting frame 701, two winding rods 703 are rotatably arranged in the mounting frame 701 and located on both sides of the partition plate 702, a pull rope 704 is arranged on the winding rod 703 and penetrates through the body 6, and the winding rod 703 can wind and store the pull rope 704, so as to prevent the pull rope 704 from being exposed and affecting the operation of the rotating fan blade 602, and increase the safety.

[0054] The clamping part 8 is arranged on the mounting frame 701 and used for fixing the position of the pull rope 704, and after the pull rope 704 binds the goods, the length of the pull rope 704 can be fixed to ensure the stability of the binding, the UAV itself is provided with a binding structure, and external ropes are not needed to realize the binding of goods, so that the convenience of using the device is increased.

[0055] As Figure 4 and Figure 8 shown, the docking cooperation structure of the UAV and the fixed seat frame 1 is disclosed, the bottom of the wing rod 601 is fixedly connected with a spring leg 6011, the parking groove 101 is provided with four column grooves 1011 for inserting the spring leg 6011, and the edge of the column groove 1011 is provided with an inclined angle 1012. It should be noted that the spring leg 6011 comprises a sleeve rod fixedly connected to the wing rod 601, a support rod is slidingly inserted into the bottom of the sleeve rod, and a supporting spring is sleeved on the support rod and connected between the sleeve rod and the support rod. Such a structure not only can buffer the impact force when the UAV lands to prevent hard collision when the UAV lands and improve safety, but also can realize the positioning and docking operation of the UAV when the UAV is parked on the parking groove 101 of the fixed seat frame 1 by inserting and cooperating the column groove 1011 and the spring leg 6011, and at the same time, the inclined angle 1012 of the column groove 1011 can be in dislocation with the spring leg 6011, so that the spring leg 6011 can be more easily inserted into the column groove 1011, the fault tolerance is increased, and the positioning and docking operation of the UAV is more beneficial.

[0056] As Figure 10The specific structure of the winding rod 703 of the present invention is disclosed. The winding rod 703 includes a rotating rod 7031 rotatably mounted in the mounting frame 701. One end of the rotating rod 7031 is sleeved with a coil spring 7032 fixedly connected to the mounting frame 701. A fixed ring 7033 is constructed in the middle of the rotating rod 7031. The pull rope 704 is annular, with one end of the loop connected to the fixed ring 7033. The other end of the pull rope 704 movably passes through the bottom of the machine body 6. The coil spring 7032 can realize the automatic rotation of the rotating rod 7031. When it is necessary to load items, the pull rope can be pulled. The rope 704 is located at one end below the body 6, causing the loop to continuously expand for attaching items. The loops of the two ropes 704 can be attached to the items simultaneously to improve the stability of the binding. Then, the spring force of the coil spring 7032 causes the rotating rod 7031 to rotate automatically, realizing the automatic tightening function of the rope 704. The position of the rope 704 is then fixed by the locking piece 8 to achieve a stable binding operation. Compared with using ropes to bind items and drones, this structure is more convenient to use, saves manpower and time, and improves the loading efficiency of items.

[0057] like Figures 9-10 The specific structure of the locking component 8 is disclosed, which is used to fix the position of the pull rope 704 and ensure the binding stability. The locking component 8 includes four U-shaped blocks 801 fixedly connected in the mounting frame 701. The U-shaped blocks 801 partially wrap around the pull rope 704. U-shaped compression plates 802 are slidably inserted into two U-shaped blocks 801 on the same side of the partition plate 702. On the opposite sides of the two U-shaped compression plates 802, racks 803 are constructed that movably pass through the partition plate 702. Positioning gears 804 that mesh with the two racks 803 are rotatably installed in the partition plate 702. A device for driving the positioning gears is fixedly installed on the mounting frame 701. The drive motor 805, which rotates 804, can drive the positioning gear 804 to rotate. The positioning gear 804 can simultaneously mesh with two racks 803, causing the two racks 803 to move closer or further apart. When the racks 803 move closer together, the two U-shaped pressing plates 802 move closer together and move inward toward the U-shaped block 801. This allows the pull rope 704 to be clamped by the docking of the U-shaped block 801 and the U-shaped pressing plates 802, thus fixing its position. When the racks 803 move further apart, the pull rope 704 is released. This automated operation is more convenient.

[0058] The foregoing description of the disclosed embodiments enables a person skilled in the art to make or use the application. Modifications of these embodiments will occur to persons of skill in the art, and that the appended claims are intended to cover all such modifications that do not depart from the true spirit and scope of the application. Therefore, the application is not limited to the embodiments shown but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.

Claims

1. A drone loading structure, characterized by, Include: Fixed seat frame (1), the fixed seat frame (1) is constructed with parking slot (101), one side of the parking slot (101) is fixedly connected with equipment box (2); Cover (3), including slidingly installed on the fixed seat frame (1) and opposite to the equipment box (2) sliding cover (301), the fixed seat frame (1) is provided with push member (302) for driving sliding cover (301) sliding; Telescopic frame (4), the fixed seat frame (1) is constructed with loading slot (102) located in the parking slot (101), the telescopic frame (4) includes connecting seat (401) connected to the bottom of the fixed seat frame (1) and located on both sides of the loading slot (102), the connecting seat (401) is hinged with a bending connecting rod (402), one end of the bending connecting rod (402) is connected with a bearing disc (403); Automatic lifting device (5), installed at the bottom of the fixed seat frame (1) and used to drive the bearing disc (403) to move up and down; The open end of the horizontal end of the sliding cover (301) is provided with a sliding column (3011), and the fixed seat frame (1) is provided with a horizontal sliding groove (103) for sliding the sliding cover (301), and the horizontal sliding groove (103) is provided with an L-shaped sliding groove (104) for guiding the sliding of the sliding column (3011), when the sliding cover (301) slides to the end side of the fixed seat frame (1), the top of the sliding cover (301) is flush with the upper surface of the fixed seat frame (1); The bending connecting rod (402) includes a long handle rod (4021) hinged to the connecting seat (401), one end of the long handle rod (4021) is hinged with a short handle rod (4022), one end of the short handle rod (4022) is hinged with a sliding frame (4023), the opposite ends of the two sliding frames (4023) are slidingly installed in the bearing disc (403), one side of the long handle rod (4021) is hinged with an extension rod (4024), the two extension rods (4024) are slidingly installed with a limiting cross rod (4025) between them; The automatic lifting device (5) includes a cylinder push rod two (501) hinged to the bottom of the fixed seat frame (1), the output end of the cylinder push rod two (501) is movably penetrated through the long handle rod (4021) and hinged to the edge of the bearing disc (403), and the bottom of the bearing disc (403) is provided with a pulling handle (4031).

2. The unmanned aerial vehicle loading structure of claim 1, wherein, One end of the equipment box (2) is constructed as a circular arc surface, and the other end is constructed as a plane, the plane end of the equipment box (2) is constructed with a stepped edge groove (201) inserted with the open end of the sliding cover (301).

3. The unmanned aerial vehicle loading structure of claim 1, wherein, The push member (302) includes a cylinder push rod one (3021) hinged at one end in the fixed seat frame (1), the output end of the cylinder push rod one (3021) is movably penetrated through the fixed seat frame (1) and hinged to the bottom side of the closed end of the sliding cover (301).

4. A UAV using the UAV loading structure according to any one of claims 1-3, characterized in that, Include: Machine body (6), the four corners of the machine body (6) are fixedly connected with wing rods (601), and the wing rods (601) are installed with rotating fan blades (602) at the ends; The rope fixing part (7) is installed in the machine body (6) and used for stretching and binding goods, the rope fixing part (7) comprises a mounting frame (701) fixedly connected in the machine body (6), a partition plate (702) is arranged in the middle of the mounting frame (701), two winding rods (703) are rotatably installed in the mounting frame (701) and located on the two sides of the partition plate (702), and a pull rope (704) is arranged on the winding rod (703) and penetrates the machine body (6) movably. The clamping part (8) is arranged on the mounting frame (701) and used for fixing the position of the pull rope (704).

5. The unmanned aerial vehicle of claim 4, wherein, The wing rod (601) is fixedly connected with a spring leg (6011) at the bottom, the parking groove (101) is provided with four column grooves (1011) for inserting the spring leg (6011), and the edge of the column groove (1011) is provided with an inclined angle (1012).

6. The unmanned aerial vehicle of claim 4, wherein, The winding rod (703) comprises a rotating rod (7031) rotatably installed in the mounting frame (701), one end of the rotating rod (7031) is sleeved with a winding spring (7032) fixedly connected to the mounting frame (701), the middle of the rotating rod (7031) is provided with a fixed ring (7033), the pull rope (704) is annular and one ring end is connected to the fixed ring (7033), and the other ring end of the pull rope (704) penetrates the bottom of the machine body (6) movably.

7. The unmanned aerial vehicle of claim 4, wherein, The clamping part (8) comprises four U-shaped blocks (801) fixedly connected in the mounting frame (701), the U-shaped block (801) is semi-wrapped on the pull rope (704), two U-shaped blocks (801) on the same side of the partition plate (702) are slidably provided with U-shaped extrusion plates (802), the opposite sides of the two U-shaped extrusion plates (802) are provided with racks (803) movably penetrating the partition plate (702), the partition plate (702) is rotatably installed with a positioning gear (804) engaged with the two racks (803), and the mounting frame (701) is fixedly installed with a driving motor (805) used for driving the positioning gear (804) to rotate.

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