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Rotor unmanned aerial vehicle

A technology of unmanned rotor and shock-absorbing plate, which is applied in the field of drones, can solve the problems of large heat generation, large volume, and large vibration, and achieve good aerodynamic shape, good shock isolation performance, and load balance.

Pending Publication Date: 2018-07-31
中科灵动航空科技成都有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the oil-electric hybrid rotor UAV uses an internal combustion engine to drive a generator to generate electricity for the rotor UAV. The entire power generation device is inevitably larger and heavier than the power supply system of a pure electric rotor UAV. , high heat generation, large vibration, etc.

Method used

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Embodiment Construction

[0022] The present invention will be further described below in conjunction with the accompanying drawings and specific preferred embodiments, but the protection scope of the present invention is not limited thereby.

[0023] Such as figure 1 As shown, the rotor drone of the present embodiment includes an equipment platform 1 and a power generating device 2; the equipment platform 1 includes an upper plate 101 and a lower plate 102 arranged in sequence from top to bottom; between the upper plate 101 and the lower plate 102, the The connection column 106 is connected; the upper plate 101 is provided with an opening in the center; the power generating device 2 is placed inside the opening. In this embodiment, the power generation device 2 uses an internal combustion engine to drive a generator to generate electricity; the internal combustion engine adopts a single-cylinder internal combustion engine; the internal combustion engine and the generator are coupled through a clutch. ...

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Abstract

The invention discloses a rotor unmanned aerial vehicle. The rotor unmanned aerial vehicle comprises an equipment platform and a power generation device; the equipment platform comprises an upper plate and a lower plate which are arranged in sequence from the top to bottom; the upper plate is connected with the lower plate through a connecting column; an opening is formed in the center of the upper plate; and the power generation device is placed in the opening. The rotor unmanned aerial vehicle has the advantages that larger loading capacity of the rotor unmanned aerial vehicle can be guaranteed, and meanwhile, the load balance of the rotor unmanned aerial vehicle can also be guaranteed, good vibration reducing performance and heat radiation performance of the rotor unmanned aerial vehicle can be guaranteed, and so on.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a rotary-wing unmanned aerial vehicle. Background technique [0002] Due to the advantages of large load capacity and long battery life, the oil-electric hybrid rotor UAV has gradually become an important development direction of industrial-grade rotor UAVs. However, when the oil-electric hybrid rotor UAV performs flight tasks, it not only You need to mount the fuel tank, and you also need to mount the mission module. However, the oil-electric hybrid rotor UAV uses an internal combustion engine to drive a generator to generate electricity for the rotor UAV. The entire power generation device is inevitably larger and heavier than the power supply system of a pure electric rotor UAV. , high heat generation, large vibration and so on. Therefore, for the rotary-wing unmanned aerial vehicle using hybrid electric power, it is necessary to carry out a reasonable overa...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D27/24B64D27/26B64D47/00B64D37/04B64D27/40
CPCB64D27/24B64D37/04B64D47/00B64D27/40
Inventor 张代智叶祖峰陈福江杨超
Owner 中科灵动航空科技成都有限公司
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