High-load all-terrain fixed-wing unmanned aerial vehicle
By designing a sliding cargo loading platform and buoyancy support plate, combined with the structure of the wing, propeller, and tail rotor, the problem of limited payload of existing high-payload all-terrain fixed-wing UAVs was solved, enabling the mounting of various sensors and equipment and the transportation of goods, thus improving payload capacity and stability.
Patent Information
- Application Number
- CN202422932574.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-29
- Publication Date
- 2025-11-07
- Estimated Expiration
- 2034-11-29
AI Technical Summary
Existing heavy-duty all-terrain fixed-wing UAVs cannot effectively carry multiple sensors and equipment, and their cargo transport capacity is limited.
The design incorporates a slidable cargo loading platform and buoyancy support plate, combined with the structure of the wings, propeller, and tail rotor, enabling the mounting of various sensors and equipment as well as the transport of goods, thus enhancing the drone's payload capacity.
It has enabled the integration of various sensors and devices, improving the drone's payload capacity and enhancing its stability and operational flexibility on different terrains and water surfaces.
Smart Images
Figure CN223521061U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to fixed wing unmanned aerial vehicle device technical field especially relates to a kind of high load all-terrain fixed wing unmanned aerial vehicle. BACKGROUND
[0002] High load all-terrain fixed wing unmanned aerial vehicle is a kind of unmanned aircraft specially designed for flying in various terrain and environmental conditions.This kind of unmanned aerial vehicle combines the efficiency of fixed-wing aircraft and the flexibility of all-terrain operation, usually has larger load capacity, can carry various sensors and equipment, and transport goods, etc.
[0003] In the prior art, part of high load all-terrain fixed wing unmanned aerial vehicle device, the working principle of high load all-terrain fixed wing unmanned aerial vehicle combines the basic physical principle of fixed-wing aircraft and modern unmanned aerial vehicle technology, the wing has larger wing area, provides higher lift, so that the unmanned aerial vehicle can maintain flight at lower speed, but part of high load all-terrain fixed wing unmanned aerial vehicle device, the device of load, generally by binding goods on the bottom support frame to load, this kind of load effect is poor, cannot carry various sensors and equipment, cannot transport more goods. SUMMARY
[0004] The utility model provides a kind of high load all-terrain fixed wing unmanned aerial vehicle, to improve the problem of part of high load all-terrain fixed wing unmanned aerial vehicle device in prior art, load is limited and cannot carry more goods.
[0005] To achieve the above object, the utility model provides the following technical scheme:
[0006] A kind of high load all-terrain fixed wing unmanned aerial vehicle, including body, the inner wall of the body is equipped with machine cabin, the inner wall side of the machine cabin is fixedly connected with the rotating assembly for opening hatch, the bottom of the two sides of the body is fixedly connected with two support frames, the outer portion of the two support frames is slidably connected with sliding connection plate, the inner wall of the sliding connection plate is threadedly connected with bolt one, the outer portion of the bolt one is threadedly connected with goods placing plate, the bottom of the bolt one is threadedly connected with nut, the bottom of the support frame is fixedly connected with bottom fixed plate, one end of the body is fixedly connected with tail rotor.
[0007] Body is the overall component of unmanned aerial vehicle, its inside is provided with machine cabin, machine cabin is controlled by rotating assembly, for opening and closing hatch, the bottom of body is fixedly connected with support frame, for providing support force, maintaining stability, sliding connection plate slides on support frame, by the suitable position of sliding, goods placing plate is placed on it, by bolt one and nut fixed connection, keep horizontal position, for placing other goods or equipment.Tail rotor generates thrust, so that unmanned aerial vehicle can fly forward.
[0008] As a further description of the above technical solutions:
[0009] The rotating assembly comprises a rotating shaft I, the cabin door is rotatably connected to the outside of the rotating shaft I, and the rotating shaft I is fixedly connected to the inner wall of one side of the cabin.
[0010] The rotating shaft I controls the opening and closing of the cabin door by rotating.
[0011] As a further description of the above technical solutions:
[0012] The inner wall of the bottom fixed plate is threadedly connected with a bolt II, and the outer thread of the bolt II is connected with a buoyancy support plate.
[0013] The bottom fixed plate is connected to the support frame, and the buoyancy support plate and the support frame are connected through the bolt II, so that the unmanned aerial vehicle can stop on the water.
[0014] As a further description of the above technical solutions:
[0015] The inner wall of the buoyancy support plate is rotatably connected with a rotating shaft II, the rotating shaft II is rotatably connected with a rotating shaft, and the rotating shaft II is rotatably connected with a machine wheel.
[0016] The rotating shaft II drives the machine wheel to rotate, so that the unmanned aerial vehicle can move on the plane, and the rotating shaft separates the machine wheel from the inner wall of the buoyancy support plate, thereby reducing the friction.
[0017] As a further description of the above technical solutions:
[0018] One side of the body is fixedly connected with a head control center, two wings are fixedly connected to the body, and the bottom of the two wings is fixedly connected with a propeller.
[0019] The head control center controls the whole unmanned aerial vehicle by receiving instructions, the wings cooperate with the propeller to improve the lift and reduce the resistance, so that the air resistance of the unmanned aerial vehicle is reduced when flying.
[0020] As a further description of the above technical solutions:
[0021] One side of the two wings is fixedly connected with two connecting rods, and the tail wing is fixedly connected to one end of the two connecting rods.
[0022] The connecting rod connects the wing with the tail wing to ensure the stability and direction control of flight.
[0023] As a further description of the above technical solutions:
[0024] One end of the head control center is fixedly connected with a rotator, and the inner wall of the rotator is rotatably connected with a camera I.
[0025] The rotator can control the camera one to rotate, so that the angle of the camera one is increased.
[0026] As a further description of the above technical solutions:
[0027] The bottom of the machine body is fixedly connected with a rotary controller, the bottom of the rotary controller is rotationally connected with a rotating disc, the bottom of the rotating disc is fixedly connected with two receiving plates, and the inner walls of the two receiving plates are rotationally connected with a camera two.
[0028] The rotary controller controls the rotating disc to rotate, so that the receiving plates rotate, and the receiving plates control the camera two to rotate, so that the camera two realizes multiple angle shooting.
[0029] The utility model has the advantages of the following:
[0030] 1、 the cabin door is rotated through the rotating shaft one, the cabin door is opened to open the machine cabin of the machine body, the goods are put in, the cabin door is closed, the goods plate connected through the bolt one on the sliding connecting plate is matched and connected, other goods are placed on the goods plate and bound, a plurality of sensors and equipment are carried, and more goods are transported.
[0031] 2、 the bottom of the wing and the connecting rod is connected with the propeller, the fixed wing unmanned aerial vehicle can vertically take off and land, the tail propeller at the tail is matched, the camera one and the camera two are matched, the operator can observe the front and rear environment, the unmanned aerial vehicle can take off and land from different terrains, the buoyancy support plate is connected on the support frame through the bottom fixed plate and the bolt two, and the unmanned aerial vehicle can stay on the water surface. DRAWINGS
[0032] Figure 1 A perspective view of a high-load all-terrain fixed-wing unmanned aerial vehicle is provided for the utility model;
[0033] Figure 2 A wing structure schematic view of a high-load all-terrain fixed-wing unmanned aerial vehicle is provided for the utility model;
[0034] Figure 3 A buoyancy support plate structure schematic view of a high-load all-terrain fixed-wing unmanned aerial vehicle is provided for the utility model;
[0035] Figure 4 A support frame structure schematic view of a high-load all-terrain fixed-wing unmanned aerial vehicle is provided for the utility model;
[0036] Figure 5 A wheel structure schematic view of a high-load all-terrain fixed-wing unmanned aerial vehicle is provided for the utility model;
[0037] Figure 6The utility model provides a kind of cabin structure schematic diagram of high load all-terrain fixed wing unmanned aerial vehicle proposed by the utility model.
[0038] Figure 7 The utility model provides a kind of rotating controller structure schematic diagram of high load all-terrain fixed wing unmanned aerial vehicle proposed by the utility model.
[0039] Legend:
[0040] 1, body; 2, cabin; 3, rotating shaft one; 4, hatch; 5, support frame; 6, sliding connection plate; 7, put goods board; 8, bolt one; 9, nut; 10, bottom fixed plate; 11, bolt two; 12, buoyancy support plate; 13, rotating shaft two; 14, rotating shaft; 15, wheel; 16, head control center; 17, wing; 18, propeller; 19, connecting rod; 20, tail; 21, tail rotor; 22, rotator; 23, camera one; 24, rotating controller; 25, turntable; 26, receiving plate; 27, camera two. Specific implementation
[0041] The technical scheme in the embodiments of the utility model will be described clearly and completely below in conjunction with the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor belong to the scope of protection of the utility model.
[0042] Referring to Figure 1 , Figure 3 and Figure 6 , the utility model provides an embodiment: a kind of high load all-terrain fixed wing unmanned aerial vehicle, including body 1, it is the main frame structure of unmanned aerial vehicle, connect each part, the inner wall of body 1 is equipped with cabin 2, located inside body 1, usually used to store goods or other equipment, the inner wall of cabin 2 one side is fixedly connected for opening hatch 4 rotating shaft one 3, rotating shaft one 3 connects hatch 4, responsible for its opening and closing, rotating shaft one 3 is rotatably connected with hatch 4, rotating shaft one 3 is rotated to control opening and closing, to prevent goods from falling in flight process, the bottom of the two sides of body 1 is fixedly connected with two support frames 5, for unmanned aerial vehicle, so that it remains stability, the outer sliding connection of two support frames 5 has sliding connection plate 6, sliding on support frame 5, different width put goods board 7 is placed by sliding, bolt one 8 is screw connected in the inner wall of sliding connection plate 6, connect put goods board 7 and sliding connection plate 6, so that different size put goods board 7 keeps horizontal direction fixed.
[0043] Referring to Figure 3 , Figure 4The outer thread of the bolt one 8 is connected with the goods placing plate 7, which is used for placing the goods and equipment of the part, and the bottom of the bolt one 8 is connected with the nut 9, which is used for fixing and connecting the goods placing plate 7 and the sliding connecting plate 6 in cooperation with the bolt one 8, and the bottom of the support frame 5 is fixedly connected with the bottom fixed plate 10, which is used for connecting the buoyancy support plate 12, and one end of the machine body 1 is fixedly connected with the tail propeller 21, which generates thrust through rotation to enable the unmanned aerial vehicle to fly forward
[0044] With reference to Figures 3 to 5 The inner wall of the bottom fixed plate 10 is threadedly connected with the bolt two 11, which connects the bottom fixed plate 10 and the buoyancy support plate 12, the outer thread of the bolt two 11 is connected with the buoyancy support plate 12, which ensures the stability when flying on water or landing on water, the inner wall of the buoyancy support plate 12 is rotatably connected with the rotating shaft two 13, the outer rotating shaft two 13 is rotatably connected with the rotating shaft 14, and the outer rotating shaft two 13 is rotatably connected with the machine wheel 15, the rotating shaft 14 separates the machine wheel 15 and the inner wall of the buoyancy support plate 12, reduces the rotation of the rotating shaft two 13, drives the machine wheel 15 to rotate, reduces the friction between the machine wheel 15 and the inner wall of the buoyancy support plate 12, and the machine wheel 15 can slide the unmanned aerial vehicle on the ground.
[0045] With reference to Figure 1 、 Figure 2 One side of the machine body 1 is fixedly connected with the head control center 16 outside, which controls the whole unmanned aerial vehicle by receiving instructions, and the two wings 17 are fixedly connected with the two wings 17 of the machine body 1, which improves the lifting force and reduces the resistance, reduces the air resistance of the unmanned aerial vehicle when flying, the bottom of the two wings 17 is fixedly connected with the propeller 18, which enables the unmanned aerial vehicle to vertically rise and land, and keeps hovering in the air, one side of the two wings 17 is fixedly connected with the two connecting rods 19, which is used for connecting the wings 17 and the tail 20, ensuring the stability and direction control of flight, and one end of the two connecting rods 19 is fixedly connected with the tail 20, which can effectively guide the flight direction.
[0046] With reference to Figure 1 、 Figure 7 One end of the head control center 16 is fixedly connected with the rotator 22, the inner wall of the rotator 22 is rotatably connected with the camera one 23, the rotator 22 rotates to enable the camera one 23 to take pictures at multiple angles, one end of the machine body 1 is fixedly connected with the rotating controller 24 at the bottom, the bottom of the rotating controller 24 is rotatably connected with the rotating disc 25, the bottom of the rotating disc 25 is fixedly connected with the two receiving plates 26, the inner wall of the two receiving plates 26 is rotatably connected with the camera two 27, the rotating controller 24 is responsible for controlling the rotation of the rotating disc 25, driving the rotation of the receiving plate 26 and the camera two 27, the receiving plate 26 provides support for the camera two 27, and multiple angle shooting is realized.
[0047] Working principle: first, the body 1 as the main frame of the unmanned aerial vehicle, is equipped with cabin 2, for storing goods or equipment. Before flight, the operator inputs instructions through the head control center 16, controls the functions of the unmanned aerial vehicle. The cabin door 4 in the cabin 2 is controlled to open and close through the rotating shaft 1 3, to ensure that the goods and equipment will not fall in flight.
[0048] Before take-off, the operator adjusts the position of the sliding connecting plate 6 on the support frame 5 according to the size of the goods, fixes the appropriate goods placing plate 7 on the sliding connecting plate 6 through the bolt 1, places the goods on the goods placing plate 7, and binds the goods or equipment with the binding belt to prevent the goods or equipment from falling.
[0049] When the unmanned aerial vehicle starts to fly, the bottom propeller 18 makes the unmanned aerial vehicle vertically lift, land and hover. The tail rotor 21 generates thrust to make the unmanned aerial vehicle fly forward, and the shape of the wing 17 is streamlined to reduce the separation of airflow and the formation of vortex, reduce the surface friction resistance and induced drag, cooperate with the wing 17 to reduce air resistance, and the wing 17 is connected with the tail wing 20 through the connecting rod 19 to ensure the stability and direction control of flight.
[0050] During flight, the head control center 16 continuously receives instructions for the unmanned aerial vehicle running process and adjusts the flight state of the unmanned aerial vehicle in real time, the rotator 22 provides power to control the camera 1 23 inside to rotate, so that the camera 1 23 can take pictures at multiple angles and capture images during flight. At the same time, the rotary controller 24 provides power to control the rotating disc 25 to rotate and drive the supporting plate 26 to support the camera 2 27 to rotate, so that the camera 2 can also rotate at multiple angles to realize multi-angle shooting.
[0051] Finally, it should be pointed out that: the above only for the preferred embodiments of the present application, and not for limiting the present application, although the present application has been described in detail with reference to the foregoing embodiments, for those skilled in the art, it can still modify the technical solutions recorded in the foregoing embodiments, or make equivalent replacement for part of the technical features, any modification, equivalent replacement, improvement, etc. made within the spirit and principles of the present application, should be included in the protection scope of the present application.
Claims
1. A high load capacity all-terrain fixed-wing drone comprising a fuselage (1), characterized in that: The inner wall of the machine body (1) is provided with a cabin (2), one side of the inner wall of the cabin (2) is fixedly connected with a rotating assembly for opening the cabin door (4), the bottom of the two sides of the machine body (1) is fixedly connected with two support frames (5), the outer part of the two support frames (5) is slidably connected with a sliding connection plate (6), the inner wall of the sliding connection plate (6) is threadedly connected with a bolt (8), the outer part of the bolt (8) is threadedly connected with a goods placing plate (7), the bottom of the bolt (8) is threadedly connected with a nut (9), the bottom of the support frame (5) is fixedly connected with a bottom fixed plate (10), one end of the machine body (1) is fixedly connected with a tail rotor (21).
2. The high-load-capacity all-terrain fixed-wing UAV of claim 1, wherein: The rotating assembly comprises a rotating shaft (3), the outer part of the rotating shaft (3) is rotatably connected with a cabin door (4), and the outer part of the rotating shaft (3) is fixedly connected to one side of the inner wall of the cabin (2).
3. The high-load-capacity all-terrain fixed-wing UAV of claim 1, wherein: The inner wall of the bottom fixed plate (10) is threadedly connected with a bolt (11), and the outer part of the bolt (11) is threadedly connected with a buoyancy support plate (12).
4. The high-load-capacity all-terrain fixed-wing UAV of claim 3, wherein: The inner wall of the buoyancy support plate (12) is rotatably connected with a rotating shaft (13), the outer part of the rotating shaft (13) is rotatably connected with a rotating shaft (14), and the outer part of the rotating shaft (13) is rotatably connected with a machine wheel (15).
5. The high-load-capacity all-terrain fixed-wing UAV of claim 1, wherein: One side of the machine body (1) is fixedly connected with a head control center (16), the two sides of the machine body (1) are fixedly connected with two wings (17), and the bottom of the two wings (17) is fixedly connected with a propeller (18).
6. The high-load-capacity all-terrain fixed-wing UAV of claim 5, wherein: One side of the two wings (17) is fixedly connected with two connecting rods (19), one end of the two connecting rods (19) is fixedly connected with a tail wing (20).
7. The high-load-capacity all-terrain fixed-wing UAV of claim 5, wherein: One end of the head control center (16) is fixedly connected with a rotator (22), and the inner wall of the rotator (22) is rotatably connected with a camera (23).
8. The high-load-capacity all-terrain fixed-wing UAV of claim 1, wherein: The bottom of the machine body (1) is fixedly connected with a rotation controller (24), the bottom of the rotation controller (24) is rotatably connected with a rotating disc (25), the bottom of the rotating disc (25) is fixedly connected with two receiving plates (26), and the inner wall of the two receiving plates (26) is rotatably connected with a camera (27).