Torch transmission unmanned aerial vehicle

An unmanned aerial vehicle and torch technology, applied in the field of unmanned aerial vehicles, can solve the problems of affecting the balance of the center of gravity of the whole machine, short battery life, and separation from the downwash flow of the rotor, so as to improve the load-to-weight ratio of the whole machine, improve compatibility, reduce effect of influence

Pending Publication Date: 2021-02-09
SHENYANG INST OF AUTOMATION - CHINESE ACAD OF SCI
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AI Technical Summary

Problems solved by technology

When the torch is passed by UAV, it faces a series of problems such as the short battery life of the UAV, the influence of the rotor downwash airflow on the torch flame, and the torch attitude affecting the center of gravity balance of the whole machine. Therefore, there is an urgent need for a fuselage structure with a high load-to-weight ratio. A kind of torch delivery UAV, in which the torch flame is separated from the downwash airflow of the rotor and the torch attitude does not affect the balance of the center of gravity of the whole machine

Method used

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  • Torch transmission unmanned aerial vehicle
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  • Torch transmission unmanned aerial vehicle

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Embodiment Construction

[0025] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0026] Such as figure 1 As shown, a kind of torch delivery drone provided by the present invention includes a rotor drone 1, a torch tilting mechanism 2, a battery counterweight system 3 and a torch 5, wherein the rotor drone 1 adopts a four-rotor configuration, and the battery The counterweight system 3 is arranged in the rotor UAV 1, the torch tilting mechanism 2 is arranged on the outside of the rotor UAV 1, the torch 5 is installed on the torch tilting mechanism 2, and the torch tilting mechanism 2 is driven to realize tilting. turn action.

[0027] Such as figure 2 As shown, in the embodiment of the present invention, the rotor UAV 1 includes a fuselage 101, a frame 102, a machine arm 103 and four main rotors 105, wherein the outer side of...

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Abstract

The invention relates to the technical field of unmanned aerial vehicles, and in particular relates to a torch transmission unmanned aerial vehicle. The torch transmission unmanned aerial vehicle comprises a rotor wing unmanned aerial vehicle, a torch tilting mechanism, a battery balance weight system and a torch, the rotor wing unmanned aerial vehicle is of a four-rotor-wing structure, the battery balance weight system is arranged in the rotor wing unmanned aerial vehicle, the torch tilting mechanism is arranged on the outer side of the rotor wing unmanned aerial vehicle, the torch is installed on the torch tilting mechanism, and tilting action is achieved through driving of the torch tilting mechanism. The functions that the unmanned aerial vehicle is high in load ratio, rotor wing downwash airflow does not influence torch flames, and torch postures do not influence the gravity center balancing characteristic of the whole vehicle can be achieved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a torch relay unmanned aerial vehicle. Background technique [0002] Large-scale games such as the Olympic Games, Paralympic Games, Winter Olympics, and Winter Paralympics require torch relay activities. At present, torch relay through drones is an important way. When the torch is passed by UAV, it faces a series of problems such as the short battery life of the UAV, the influence of the rotor downwash airflow on the torch flame, and the torch attitude affecting the center of gravity balance of the whole machine. Therefore, there is an urgent need for a fuselage structure with a high load-to-weight ratio. A kind of torch transfer UAV in which the torch flame is separated from the downwash airflow of the rotor and the torch attitude does not affect the balance of the center of gravity of the whole machine. Contents of the invention [0003] In view of the above...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/06B64D47/00B64C27/08B64D27/24
CPCB64C1/06B64D47/00B64C27/08B64D27/24B64U10/10B64U2101/00
Inventor 何玉庆杨丽英李思梁马立新黄朝雄常彦春张远航
Owner SHENYANG INST OF AUTOMATION - CHINESE ACAD OF SCI
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