CN209814269U - transport drone - Google Patents

Abstract

The utility model discloses a transport unmanned aerial vehicle, which comprises a fuselage and a rotor module. The rotor module drives the fuselage to fly. The rotor module includes: a wing and a propeller arranged in the wing; wherein, the fuselage includes: an annular The pipe frame and the engine room coaxially arranged above the ring pipe frame, the engine room and the ring pipe frame are connected by a plurality of spokes, the spokes are set to be hollow and the two ends are connected to the engine room and the ring pipe frame; A transport box is provided. The top of the transport box can fit into the annular area enclosed by the annular pipe frame and is detachably connected to the annular pipe frame. The transport box is provided with a cover. The transport UAV can carry out portable transportation of light and small-volume goods through the flight of the UAV.

Description

transport drone

technical field

The utility model relates to a transportation tool, in particular to a transportation unmanned aerial vehicle.

Background technique

For some areas with poor traffic conditions, such as mountain roads, potholes and highlands, it is very inconvenient to transport some light and small-sized items, especially during the construction process, construction personnel need to go back and forth between the material warehouse and the construction site In between, it is very inconvenient. In addition, when working at high altitudes, it is even more inconvenient to run back and forth. Under such circumstances, there is an urgent need for a transport drone for transporting some light and small-volume items, so as to improve work efficiency and reduce labor load.

Utility model content

The purpose of the utility model is to provide a transport unmanned aerial vehicle, which can carry out portable transportation of light and small-sized goods through the flight of the unmanned aerial vehicle.

In order to achieve the above object, the utility model provides a transport unmanned aerial vehicle, including a fuselage and a rotor module, the fuselage is driven to fly by the rotor module, and the rotor module includes: a wing and a The propeller inside; wherein, the fuselage includes: an annular pipe frame and a nacelle coaxially arranged above the annular pipe frame, the nacelle and the annular pipe frame are connected by a plurality of spokes, and the spokes are arranged It is hollow and its two ends are connected to the engine room and the annular pipe frame respectively; a transport box is arranged coaxially below the fuselage, and the top of the transport box can fitly extend into the surrounding area of the annular pipe frame and is detachably connected to the annular pipe frame, and the transport box is provided with a cover.

Preferably, the top side of the transport box is provided with a plurality of L-shaped fasteners, the inner side of the L-shaped fasteners is provided with raised blocks, and the outer side of the annular pipe frame is provided with Matching blocks.

Preferably, the outer side of the transport box is provided with a plurality of stoppers along its circumferential direction.

Preferably, a positioning ring is provided on the inner upper part of the transport box, and the cover body is detachably mounted on the positioning ring.

Preferably, the cover body includes: a cover plate and a pressing mechanism, the pressing mechanism is installed under the cover plate, a plurality of screw holes are provided on the positioning ring, and screws matching the screw holes penetrate The cover plate is screwed into the screw hole to fix the cover plate.

Preferably, the pressing mechanism includes: a pressing plate and an elastic mechanism, and the elastic mechanism is connected between the pressing plate and the cover plate.

Preferably, the elastic mechanism includes: a telescopic rod and a spring sleeved on the telescopic rod.

Preferably, the telescopic rod is a multi-section telescopic rod.

According to the above technical solution, in the utility model, the rotor module drives the fuselage to fly, and the rotor module includes: a wing and a propeller arranged in the wing; wherein, the fuselage includes: an annular pipe frame and the engine room coaxially arranged above the annular pipe frame, the engine room and the annular pipe frame are connected by a plurality of spokes, the spokes are set to be hollow and their two ends communicate with the engine room and the annular pipe frame respectively In the pipe frame; a transport box is coaxially arranged below the fuselage, and the top of the transport box can fit into the annular area enclosed by the annular pipe frame, and is detachably connected to the On the ring-shaped pipe frame, the transport box is provided with a cover. When in use, put items within the weighing range into the transport box, start the rotor module, and drive the fuselage to fly through the rotor module, thereby driving the transport box to be transported to a designated location.

Other features and advantages of the present utility model will be described in detail in the following specific embodiments.

Description of drawings

The accompanying drawings are used to provide a further understanding of the utility model, and constitute a part of the description, together with the following specific embodiments, are used to explain the utility model, but do not constitute a limitation to the utility model. In the attached picture:

Fig. 1 is a schematic structural view of a preferred embodiment of the transport unmanned aerial vehicle in the utility model;

Fig. 2 is a schematic diagram of the connection structure between the transport box and the annular pipe frame in the utility model.

Explanation of reference signs

1 engine room 2 ring pipe rack

3 Transport case 4 Wings

5 spokes 6 covers

7 Press plate 8 Locating ring

9 screw holes 10 telescopic rod

11 Spring 12 Stop

13L type fastener 14 blocks

15 raised blocks

Detailed ways

The specific embodiment of the utility model will be described in detail below in conjunction with the accompanying drawings. It should be understood that the specific embodiments described here are only used to illustrate and explain the utility model, and are not intended to limit the utility model.

In the present utility model, unless otherwise specified, the orientation words included in the term such as "up, down, left, right, front, back, inside and outside" only represent the orientation of the term in the normal use state, or are understood by those skilled in the art colloquially and should not be construed as a limitation of the term.

Referring to the transport UAV shown in Figures 1-2, it includes a fuselage and a rotor module 4, and the rotor module 4 drives the fuselage to fly. The rotor module 4 includes: wings and a wherein, the fuselage includes: an annular pipe frame 2 and a nacelle 1 coaxially arranged above the annular pipe frame 2, and the nacelle 1 and the annular pipe frame 2 are connected by a plurality of spokes 5 , the spokes 5 are set to be hollow and both ends are respectively connected to the cabin 1 and the annular pipe frame 2; a transport box 3 is arranged coaxially below the fuselage, and the top of the transport box 3 can fit protrudes into the annular area surrounded by the annular pipe rack 2, and is detachably connected to the annular pipe rack 2, and the transport box 3 is provided with a cover.

Through the implementation of the above technical solution, the rotor module 4 drives the fuselage to fly, and the rotor module 4 includes: a wing and a propeller arranged in the wing; wherein, the fuselage includes: an annular pipe frame 2 and the engine room 1 coaxially arranged above the annular pipe frame 2, the engine room 1 and the annular pipe frame 2 are connected by a plurality of spokes 5, and the spokes 5 are set to be hollow and communicate with the two ends respectively. Inside the engine room 1 and the annular pipe frame 2; a transport box 3 is arranged coaxially below the fuselage, and the top of the transport box 3 can fit into the ring formed by the annular pipe frame 2. area, and is detachably connected to the ring pipe frame 2, and the transport box 3 is provided with a cover. When in use, put items within the weighing range into the transport box 3, start the rotor module 4, and drive the fuselage to fly through the rotor module 4, thereby driving the transport box 3 to be transported to a designated position. The nacelle 1 is provided with electrical components for controlling the operation of the rotor module 4. The connecting wires between the electrical components and the rotor module 4 run through the spokes 5 and the hollow part of the annular pipe frame 2. The working principle of the rotor module 4 is the prior art I won’t go into details here. In addition, in order to facilitate the visual flight of the transport UAV, a collection camera can be arranged at the front end of the ring pipe frame 2, and it can be connected with the receiving device through a wireless signal to know the flight position of the transport UAV in real time. .

In this real-time manner, in order to further realize the detachable connection between the transport box 3 and the annular pipe frame 2 . Preferably, the top side of the transport box 3 is provided with a plurality of L-shaped fasteners 13, the inner side of the L-shaped fasteners 13 is provided with a raised block 15, and the outer side of the annular pipe frame 2 is provided with The block 14 that matches the raised block 15. By rotating the L-shaped fastener 13 hinged on the transport box 3 downwards, the raised block 15 is engaged under the stopper 14 to buckle and fix the transport box 3 on the annular pipe frame 2 .

In this real-time mode, in order to prevent the L-shaped fastener 13 from loosening from the annular pipe rack 2 due to the excessive upward movement of the transport box 3, which will affect the transportation of the goods, preferably, the outer side of the transport box 3 is provided with A plurality of stoppers 12 .

In this real-time manner, in order to further facilitate the detachable fixing of the cover, preferably, a positioning ring 8 is provided on the inner upper part of the transport box 3 , and the cover is detachably mounted on the positioning ring 8 .

In this real-time mode, on the one hand, in order to facilitate the disassembly of the cover body, and on the other hand, prevent the goods in the transport box 3 from shaking too much during transportation, preferably, the cover body includes: a cover plate 6 and a pressing mechanism, and the pressing The mechanism is installed under the cover plate 6, and the positioning ring 8 is provided with a plurality of screw holes 9, and the screws matching the screw holes 9 pass through the cover plate 6 and are screwed to the screw holes 9 Inside to fix the cover plate 6. After the cover plate 6 is fixed on the positioning ring 8, the pressing mechanism contacts and simultaneously compresses the goods in the transport box 3, thereby reducing the excessive shaking of the goods during transportation.

In this real-time mode, in order to further improve the compression effect of the compression mechanism and reduce the damage of the compression mechanism to the cargo, preferably, the compression mechanism includes: a pressure plate 7 and an elastic mechanism, and the elastic mechanism is connected to the Between the pressure plate 7 and the cover plate 6.

In this real-time mode, in order to load as many goods as possible and compress the goods, and improve the flexibility of goods loading, preferably, the elastic mechanism includes: a telescopic rod 10 and a spring sleeved on the telescopic rod 10 11. The setting of the telescopic rod 10 can prevent the spring 11 from bending and play a position-limiting role.

In this real-time manner, in order to further load as many goods as possible and compress the goods, and improve the flexibility of goods loading, preferably, the telescopic rod 10 is a multi-section telescopic rod.

The preferred embodiment of the utility model has been described in detail above in conjunction with the accompanying drawings, but the utility model is not limited to the specific details of the above-mentioned embodiment, and within the scope of the technical concept of the utility model, the technical solution of the utility model can be carried out in many ways. These simple modifications all belong to the protection scope of the present utility model.

In addition, it should be noted that the specific technical features described in the above specific embodiments can be combined in any suitable way if there is no contradiction. The combination method will not be explained separately.

In addition, any combination of various implementations of the present invention can also be made, as long as they do not violate the idea of the present invention, they should also be regarded as the disclosed content of the present invention.

Claims (8)

1. The utility model provides a transportation unmanned aerial vehicle, includes fuselage and rotor module (4), through rotor module (4) drive the fuselage flight, its characterized in that, rotor module (4) include: the aircraft comprises a wing and a propeller arranged in the wing; wherein,

the fuselage includes: the aircraft comprises an annular pipeline frame (2) and an engine room (1) coaxially arranged above the annular pipeline frame (2), wherein the engine room (1) is connected with the annular pipeline frame (2) through a plurality of spokes (5), the spokes (5) are hollow, and two ends of the spokes are respectively communicated with the engine room (1) and the annular pipeline frame (2);

the coaxial transport case (3) that is provided with in below of fuselage, the top of transport case (3) can agree with ground to stretch into the annular region that the closed formation of annular pipeline frame (2) encloses to detachably connect in on the annular pipeline frame (2), be provided with the lid on transport case (3).

2. Transport unmanned aerial vehicle of claim 1, characterized in that the top side of transport case (3) is provided with a plurality of L type fasteners (13), the inboard of L type fastener (13) is provided with protruding piece (15), the outside of looped pipeline frame (2) is provided with dog (14) with protruding piece (15) matches.

3. Transport drone according to claim 2, characterised in that the outside of the transport box (3) is provided with a plurality of stops (12) along its circumferential direction.

4. Transport drone according to claim 1, characterised in that the inner upper part of the transport box (3) is provided with a positioning ring (8), the cover being removably mounted on the positioning ring (8).

5. A transport drone as claimed in claim 4, characterised in that the cover comprises: the cover plate comprises a cover plate (6) and a pressing mechanism, wherein the pressing mechanism is installed below the cover plate (6), a plurality of screw holes (9) are formed in a positioning ring (8), and screws matched with the screw holes (9) penetrate through the cover plate (6) and are in threaded connection with the screw holes (9) so as to fix the cover plate (6).

6. The transport drone of claim 5, wherein the hold down mechanism includes: the pressing plate (7) and the elastic mechanism are connected between the pressing plate (7) and the cover plate (6).

7. A transport drone according to claim 6, characterised in that the elastic mechanism comprises: the telescopic rod (10) and a spring (11) sleeved on the telescopic rod (10).

8. Transport drone according to claim 7, characterised in that the telescopic pole (10) is a multi-section telescopic pole.