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Multi-rotor unmanned aerial vehicle loading device with high loading capacity and multi-rotor unmanned aerial vehicle

A technology of a multi-rotor unmanned aerial vehicle and a loading device, which is applied in the field of unmanned aerial vehicles, can solve the problems of low loading capacity of multi-rotor drones, and achieve the effect of reducing the volume and increasing the loading capacity.

Inactive Publication Date: 2018-03-06
成都鑫晨航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to provide a loading device for a multi-rotor UAV with a large loading capacity and a multi-rotor UAV to solve the problem that the loading capacity of an existing multi-rotor UAV is low

Method used

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  • Multi-rotor unmanned aerial vehicle loading device with high loading capacity and multi-rotor unmanned aerial vehicle
  • Multi-rotor unmanned aerial vehicle loading device with high loading capacity and multi-rotor unmanned aerial vehicle
  • Multi-rotor unmanned aerial vehicle loading device with high loading capacity and multi-rotor unmanned aerial vehicle

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0026] A multi-rotor UAV loading device with a large loading capacity, the loading device includes a storage box, and the storage box includes a first storage component and a second storage component located on the right side of the first storage component , the right side of the first storage component is provided with a right card slot, and a right fence is formed between two adjacent right card slots; the left side of the second storage component is provided with a left card suitable for the right fence slot, and form a left fence that matches the right card slot between two adjacent left card slots, and two connecting bars are also provided, and the lower part of the connecting bar is connected with the first storage component and the second storage component respectively . Through this setting, the multi-rotor UAV can be loaded with items. When the loading capacity is large and the space of the storage box is not enough, one storage box can be split into two storage comp...

Embodiment 2

[0028] A multi-rotor unmanned aerial vehicle, comprising a body, the body is provided with a number of rotary arms, the rotary arms are respectively provided with propellers, the tail of the body is also provided with a cooling device, the cooling device includes a connecting frame, the The connecting frame is connected with the tail of the body, the connecting frame is provided with a radiator, the radiator includes a motor, the motor is connected with the connecting frame, the output shaft of the motor is connected with a worm, and the other end of the worm is connected with a heat sink, The worm is also provided with a T-shaped fixed rod, the lower end of the T-shaped fixed rod is sleeved on the worm, the left end of the T-shaped fixed rod is hinged with a connecting rod one, the other end of the connected rod one is hinged with a connecting rod two, The other end is hinged with connecting rod three, the other end of connecting rod three and the right end of the T-shaped fix...

Embodiment 3

[0030] On the basis of Embodiment 2, the heat sink includes three blades, the blades include a blade slope and a blade plane, and the included angle between the blade slope and the blade plane is 171° to 173°. Through this setting, the heat dissipation effect can be improved and the heat dissipation can be more thorough.

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Abstract

The invention discloses a multi-rotor unmanned aerial vehicle loading device with the high loading capacity and a multi-rotor unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The problem that an existing multi-rotor unmanned aerial vehicle is low in loading capacity is solved. The loading device comprises a storage box, and the storage box comprises a firststorage assembly and a second storage assembly located on the right side of the first storage assembly; right clamping grooves are formed in the right side of the first storage assembly, and a right railing is formed between the two adjacent right clamping grooves; left clamping grooves matched with the right railing are formed in the left side of the second storage assembly, and a left railing matched with the right clamping grooves is formed between the two adjacent left clamping grooves; and two connecting strips are further arranged, and the lower parts of the connecting strips are connected with the first storage assembly and the second storage assembly correspondingly. The multi-rotor unmanned aerial vehicle loading device is suitable for the unmanned aerial vehicles.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a multi-rotor unmanned aerial vehicle loading device with a large loading capacity and a multi-rotor unmanned aerial vehicle. Background technique [0002] UAV is a general term for unmanned aerial vehicles, which are equipped with autopilots, program control devices and other equipment, and can be tracked and positioned by ground stations or pilots. Compared with manned aircraft, it has the advantages of small size, low cost, and convenient use. [0003] There are many types of UAVs, mainly including fixed-wing UAVs, flapping-wing UAVs and multi-rotor UAVs. Due to its simple control, high reliability, vertical take-off and landing without a runway, and the ability to hover in the air after takeoff, multi-rotor UAVs are widely used in various fields compared to fixed-wing UAVs and flapping-wing UAVs. has been widely used. [0004] Existing multi-ro...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64D9/00H05K7/20
CPCH05K7/2039B64C27/08B64D9/00B64U10/10B64U2101/60
Inventor 石存岭
Owner 成都鑫晨航空科技有限公司
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