CN219524284U - Hybrid high-load cargo-delivering unmanned aerial vehicle - Google Patents

Abstract

The utility model provides a hybrid high-load delivery unmanned aerial vehicle, which is characterized in that a solar power supply main board is arranged on the upper surface of an unmanned aerial vehicle main body to supply power to the unmanned aerial vehicle through solar power, a power supply side plate is fixedly connected with the outer surface of the solar power supply main board to increase the power supply amount, the inner surface of the hybrid high-load delivery unmanned aerial vehicle main body is electrically connected with a unmanned aerial vehicle power supply battery, the unmanned aerial vehicle can be effectively powered under the high-load operation through the arranged unmanned aerial vehicle power supply battery, the unmanned aerial vehicle power supply battery is charged through a charging plug electrically connected with the left surface of the unmanned aerial vehicle main body, goods are loaded through the delivery assembly, a supporting rod is fixedly connected with the upper surface of the unmanned aerial vehicle main body, the goods to be delivered are placed into a delivery container through the lower surface of the unmanned aerial vehicle main body, and the upper surface of a motor rotating shaft is nested and connected with a delivery unmanned aerial vehicle fan blade to provide rotating power.

Description

Hybrid high-load cargo-delivering unmanned aerial vehicle

Technical Field

The utility model relates to the field of unmanned aerial vehicles, and belongs to a hybrid high-load delivery unmanned aerial vehicle.

Background

The current logistics industry development is rapid, and along with the development of science and technology, unmanned aerial vehicle delivery is going to the gate and will become the trend of science and technology development, but unmanned aerial vehicle's battery storage's electric quantity is limited, leads to unmanned aerial vehicle flight time shorter, has restricted unmanned aerial vehicle application further development. Therefore, a high-load delivery unmanned aerial vehicle with high cruising ability is urgently needed in the market.

Disclosure of Invention

In order to achieve the above purpose, the present utility model provides the following technical solutions:

the utility model provides a high load of hybrid unmanned aerial vehicle that carries goods, includes unmanned aerial vehicle host computer body, its characterized in that, the below of unmanned aerial vehicle host computer body is equipped with supporting component and delivery subassembly, the surface of unmanned aerial vehicle host computer body is equipped with unmanned aerial vehicle power supply unit, the side of unmanned aerial vehicle host computer body is equipped with unmanned aerial vehicle transportation subassembly;

the unmanned aerial vehicle power supply assembly comprises a solar power supply main board, a power supply side board, an unmanned aerial vehicle power supply battery and a battery charging plug, wherein the solar power supply main board and the power supply side board are arranged on the upper surface of the unmanned aerial vehicle main body, the power supply side board surrounds the solar power supply main board, and the unmanned aerial vehicle power supply battery is positioned below the solar power supply main board and the power supply side board; unmanned aerial vehicle power supply battery sets up in the unmanned aerial vehicle main part, solar energy power supply mainboard and power supply curb plate turn into the electric energy with solar energy for unmanned aerial vehicle power supply battery charges, battery charging plug connects the commercial power in order to give unmanned aerial vehicle power supply battery charges.

Further, the below of unmanned aerial vehicle host computer body is equipped with supporting component, supporting component includes H type bracing piece, unmanned aerial vehicle landing gear, landing gear shock attenuation screw thread urceolus, unmanned aerial vehicle horizontal pole and connecting axle, the bottom of H type bracing piece is inlayed and is connected unmanned aerial vehicle landing gear, the surface nested connection of unmanned aerial vehicle landing gear the landing gear shock attenuation screw thread urceolus, the horizontal through connection of H type bracing piece the unmanned aerial vehicle horizontal pole, the surface of unmanned aerial vehicle horizontal pole is provided with the connecting axle, H type bracing piece is equipped with two, and all slope is established unmanned aerial vehicle host computer body below, symmetrical installation, wherein the unmanned aerial vehicle horizontal pole passes through the connecting axle with H type bracing piece is connected.

The delivery assembly is located two between the H-shaped support rods, and the delivery assembly is located above the unmanned aerial vehicle cross rod.

Further, the delivery assembly comprises a support rod, a wireless connector, a singlechip, a delivery container, a box door and a door handle; the utility model discloses a door handle, including the upper surface fixed connection of unmanned aerial vehicle host computer body the bracing piece, the upper surface electric connection of bracing piece wireless connector, wireless connector one end electric connection singlechip, the lower surface of unmanned aerial vehicle host computer body is dismantled and is connected the cargo delivery packing box, the front end of cargo delivery packing box is opened and shut and is connected the chamber door, the front end bolted connection of chamber door the door handle.

Further, unmanned aerial vehicle transportation subassembly comprises six power components, and every power component includes unmanned aerial vehicle flabellum pole, mount pad, servo motor, motor shaft and delivery unmanned aerial vehicle flabellum.

The unmanned aerial vehicle flabellum pole is equipped with the tail end, the tail end is established six in the unmanned aerial vehicle owner body outside, the top fixed connection on unmanned aerial vehicle flabellum pole top the mount pad, the upper surface electric connection of mount pad servo motor, servo motor's upper surface rotates to be connected the motor shaft, the upper surface nested connection of motor shaft the delivery unmanned aerial vehicle flabellum.

The utility model has the beneficial effects that:

according to the unmanned aerial vehicle, the solar power supply main board and the power supply side boards are arranged on the upper surface of the unmanned aerial vehicle main body to supply solar power, and the unmanned aerial vehicle battery is arranged to supply battery power, so that the cruising ability of the unmanned aerial vehicle is greatly improved through the cooperation of the two hybrid power.

The foregoing description is only an overview of the present utility model, and is intended to provide a better understanding of the present utility model, as it is embodied in the following description, with reference to the preferred embodiments of the present utility model and the accompanying drawings.

Drawings

FIG. 1 is a schematic diagram of a structure provided by the present utility model;

FIG. 2 is a schematic diagram of the structure provided by the present utility model;

FIG. 3 is a schematic view of a partial structure provided by the present utility model;

FIG. 4 is a front view of the present utility model;

FIG. 5 is a side view of the present utility model;

fig. 6 is a bottom view of the present utility model.

Reference numerals:

1. an unmanned aerial vehicle main body;

2. a support assembly; 201. an H-shaped supporting rod; 202. unmanned aerial vehicle landing gear; 203. a damping threaded outer cylinder of the floor stand; 204. unmanned aerial vehicle horizontal pole; 205. a connecting shaft;

3. a power supply assembly for the unmanned aerial vehicle; 301. a solar power supply main board; 302. a power supply side plate; 303. a power supply battery of the unmanned aerial vehicle; 304. a battery charging plug;

4. an unmanned aerial vehicle transport assembly; 401. unmanned aerial vehicle fan blade pole; 402. a mounting base; 403. a servo motor; 404. a motor shaft; 405. fan blades of a delivery unmanned aerial vehicle;

5. a delivery assembly; 501. a support rod; 502. a wireless connector; 503. a cargo delivery container; 504. a door; 505. door handle.

Detailed Description

The following describes in further detail the embodiments of the present utility model with reference to the drawings and examples. The following examples are illustrative of the utility model and are not intended to limit the scope of the utility model.

Embodiment 1 please refer to fig. 1-6, a hybrid high load delivery unmanned aerial vehicle, including unmanned aerial vehicle main body 1, its characterized in that, the below of unmanned aerial vehicle main body 1 is equipped with supporting component 2 and delivery subassembly 5, unmanned aerial vehicle main body 1's surface is equipped with unmanned aerial vehicle power supply module 3, unmanned aerial vehicle main body's side is equipped with unmanned aerial vehicle transportation subassembly 4.

The unmanned aerial vehicle power supply assembly comprises a solar power supply main board 301, a power supply side board 302, an unmanned aerial vehicle power supply battery 303 and a battery charging plug 304, wherein the solar power supply main board 301 and the power supply side board 302 are arranged on the upper surface of the unmanned aerial vehicle main body 1, the power supply side board 302 surrounds the solar power supply main board 301, and the unmanned aerial vehicle power supply battery 303 is positioned below the solar power supply main board 301 and the power supply side board 302; unmanned aerial vehicle power supply battery 303 sets up in unmanned aerial vehicle main part 1, solar energy power supply mainboard 301 and power supply curb plate 302 are with solar energy conversion for unmanned aerial vehicle power supply battery 303 charges, battery charging plug 304 connects the commercial power in order to give unmanned aerial vehicle power supply battery 303 charges.

The below of unmanned aerial vehicle owner organism 1 is equipped with supporting component 2, supporting component 2 includes H type bracing piece 201, unmanned aerial vehicle landing gear 202, landing gear shock attenuation screw thread urceolus 203, unmanned aerial vehicle horizontal pole 204, connecting axle 205, the bottom of H type bracing piece 201 is inlayed and is connected unmanned aerial vehicle landing gear 202, the surface nested connection of unmanned aerial vehicle landing gear 202 landing gear shock attenuation screw thread urceolus 203, the horizontal through connection of H type bracing piece 201 unmanned aerial vehicle horizontal pole 204, the surface of unmanned aerial vehicle horizontal pole 204 is provided with connecting axle 205, H type bracing piece 201 is equipped with two, all inclines to establish unmanned aerial vehicle owner organism 1 below, symmetrical installation, wherein unmanned aerial vehicle horizontal pole 204 is passed through connecting axle 205 with H type bracing piece 201 is connected.

The delivery assembly 5 is located between the two H-shaped support bars 201 and above the unmanned aerial vehicle cross bar 204.

The delivery assembly 5 comprises a support rod 501, a wireless connector 502, a single chip microcomputer (not shown), a delivery container 503, a box door 504 and a door handle 505; the upper surface fixed connection of unmanned aerial vehicle host computer body 1 bracing piece 501, the upper surface electric connection of bracing piece 501 wireless connector 502, wireless connector 502 one end electric connection singlechip (not shown), the lower surface dismantlement of unmanned aerial vehicle host computer body 1 is connected cargo container 503, the front end of cargo container 503 is opened and shut and is connected chamber door 504, the front end bolted connection of chamber door 504 door handle 505.

The unmanned aerial vehicle transportation subassembly 4 comprises six power components, and every power component includes unmanned aerial vehicle flabellum 401, mount pad 402, servo motor 403, motor shaft 404, delivery unmanned aerial vehicle flabellum 405.

The unmanned aerial vehicle fan blade pole 401 is equipped with the tail end, the tail end is established six in the unmanned aerial vehicle main part body 1 outside, the top fixed connection on unmanned aerial vehicle fan blade pole 401 top mount pad 402, the upper surface electric connection of mount pad 402 servo motor 403, servo motor 403's upper surface rotates to be connected motor pivot 404, motor pivot 404's upper surface nested connection delivery unmanned aerial vehicle fan blade 405.

Working principle:

the drone power supply battery 303 supplies power to the drone main body 1. Further, the unmanned aerial vehicle power supply battery 303 provides electric energy for the servo motor 403, so that the servo motor 403 drives the delivery unmanned aerial vehicle fan blade 405 to rotate through the motor rotating shaft 404, and then lift force is generated to transport goods.

Before unmanned aerial vehicle takes off, unmanned aerial vehicle power supply battery 303 charges unmanned aerial vehicle power supply battery 303 through battery charging plug 304 connection commercial power supply, and solar power supply mainboard 301 and power supply curb plate 302 are solar cell panel, can utilize photoelectric effect to answer the direct light energy conversion electric energy of becoming, can charge unmanned aerial vehicle power supply battery 303. The goods to be transported are placed in the cargo box 503 and the box door 504 is closed, completing the placement of the goods. At this time, the singlechip is connected with the ground data center through the wireless connector 502, the ground data center sends a take-off signal to the wireless connector, and the singlechip controls the unmanned aerial vehicle transportation assembly 4 to start.

When the unmanned aerial vehicle flies, the voltage of the unmanned aerial vehicle power supply battery 303 can continuously drop, when the singlechip detects that the voltage of the unmanned aerial vehicle power supply battery drops to 36V, the singlechip controls the solar power supply main board 301 to charge the unmanned aerial vehicle power supply battery 303, when the singlechip detects that the voltage of the unmanned aerial vehicle power supply battery 303 is lower than 30V, the singlechip controls the power supply side board 302 to charge the unmanned aerial vehicle power supply battery 303 in cooperation with the solar power supply main board 301, so that the power supply amount is increased.

Landing is performed by the unmanned aerial vehicle landing frame 202 after the goods are delivered, and vibration generated at the time of landing is reduced by the landing frame damper rubber outer cylinder 203.

The technical features of the above-described embodiments may be arbitrarily combined, and all possible combinations of the technical features in the above-described embodiments are not described for brevity of description, however, as long as there is no contradiction between the combinations of the technical features, they should be considered as the scope of the description.

The above examples illustrate only a few embodiments of the utility model, which are described in detail and are not to be construed as limiting the scope of the utility model. It should be noted that it will be apparent to those skilled in the art that several variations and modifications can be made without departing from the spirit of the utility model, which are all within the scope of the utility model. Accordingly, the scope of protection of the present utility model is to be determined by the appended claims.

Claims (4)

1. The utility model provides a high load of hybrid unmanned aerial vehicle that carries goods, includes unmanned aerial vehicle host computer body, its characterized in that, the below of unmanned aerial vehicle host computer body is equipped with supporting component and delivery subassembly, the surface of unmanned aerial vehicle host computer body is equipped with unmanned aerial vehicle power supply unit, the side of unmanned aerial vehicle host computer body is equipped with unmanned aerial vehicle transportation subassembly;

the unmanned aerial vehicle power supply assembly comprises a solar power supply main board, a power supply side board, an unmanned aerial vehicle power supply battery and a battery charging plug, wherein the solar power supply main board and the power supply side board are arranged on the upper surface of the unmanned aerial vehicle main body, the power supply side board surrounds the solar power supply main board, and the unmanned aerial vehicle power supply battery is positioned below the solar power supply main board and the power supply side board; unmanned aerial vehicle power supply battery sets up in the unmanned aerial vehicle host computer is internal, solar energy power supply mainboard and power supply curb plate turn into the electric energy with solar energy for unmanned aerial vehicle power supply battery charges, battery charging plug connects the commercial power in order to give unmanned aerial vehicle power supply battery charges.

2. The hybrid high-load cargo-delivering unmanned aerial vehicle according to claim 1, wherein a supporting component is arranged below the unmanned aerial vehicle main body, the supporting component comprises an H-shaped supporting rod, an unmanned aerial vehicle landing frame, a landing frame shock-absorbing threaded outer cylinder, an unmanned aerial vehicle cross rod and a connecting shaft, the bottom end of the H-shaped supporting rod is embedded and connected with the unmanned aerial vehicle landing frame, the outer surface of the unmanned aerial vehicle landing frame is embedded and connected with the landing frame shock-absorbing threaded outer cylinder, the transverse surface of the H-shaped supporting rod is in penetrating connection with the unmanned aerial vehicle cross rod, the outer surface of the unmanned aerial vehicle cross rod is provided with the connecting shaft, the two H-shaped supporting rods are obliquely arranged below the unmanned aerial vehicle main body and are symmetrically installed, and the unmanned aerial vehicle cross rod is connected with the H-shaped supporting rod through the connecting shaft;

the delivery assembly is located two between the H-shaped support rods, and the delivery assembly is located above the unmanned aerial vehicle cross rod.

3. The hybrid high load delivery drone of claim 2, wherein the delivery assembly includes a support bar, a wireless connector, a single chip, a delivery box, a box door, and a door handle; the utility model discloses a door handle, including the upper surface fixed connection of unmanned aerial vehicle host computer body the bracing piece, the upper surface electric connection of bracing piece wireless connector, wireless connector one end electric connection singlechip, the lower surface of unmanned aerial vehicle host computer body is dismantled and is connected the cargo delivery packing box, the front end of cargo delivery packing box is opened and shut and is connected the chamber door, the front end bolted connection of chamber door the door handle.

4. The hybrid high load delivery unmanned aerial vehicle of claim 1, wherein the unmanned aerial vehicle transport assembly is comprised of six power assemblies, each power assembly comprising an unmanned aerial vehicle fan blade bar, a mount pad, a servo motor, a motor shaft, and a delivery unmanned aerial vehicle fan blade;

the unmanned aerial vehicle flabellum pole is equipped with the tail end, the tail end is established six in the unmanned aerial vehicle owner body outside, the top fixed connection on unmanned aerial vehicle flabellum pole top the mount pad, the upper surface electric connection of mount pad servo motor, servo motor's upper surface rotates to be connected the motor shaft, the upper surface nested connection of motor shaft the delivery unmanned aerial vehicle flabellum.