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Multi-rotor electric cruise UAV (Unmanned Aerial Vehicle)

A technology of drones and multi-rotors, applied in the field of drones, can solve the problems of inconvenient operation of drones, and achieve the effect of solving the problem of not being able to lift smoothly, ensuring simplicity, and ensuring stability

Inactive Publication Date: 2018-11-23
扬州飞虎航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] Aiming at the deficiencies of the prior art, the present invention provides a multi-rotor electric cruising drone, which solves the problem that the drone is not easy to operate

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  • Multi-rotor electric cruise UAV (Unmanned Aerial Vehicle)
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  • Multi-rotor electric cruise UAV (Unmanned Aerial Vehicle)

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Embodiment Construction

[0021] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0022] see Figure 1-3 , the present invention provides a technical solution: a multi-rotor electric cruising drone, including a drone body 13, the upper surface of the drone body 13 is fixedly connected with a battery 20, which is convenient for the long-term battery life of the drone, without The bottom surface of the human-machine body 13 is fixedly connected with two symmetrical load-bearing rods 12, and the bottom surface of each load-bearing rod 12 is fi...

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Abstract

The invention discloses a multi-rotor electric cruise UAV (Unmanned Aerial Vehicle). The multi-rotor electric cruise UAV comprises a UAV body, wherein a cavity is arranged at the inner part of the UAVbody; two symmetric first bearings are fixedly embedded on the inner side wall of the cavity; the inner bottom wall of the cavity is fixedly connected with a forward and reverse rotation motor; an output end of the forward and reverse rotation motor is fixedly connected with a first gear; a rotating shaft is arranged at the inner part of the cavity; the outer surface of the rotating shaft is fixedly connected with an annular gear rack in fit with the first gear. According to the multi-rotor electric cruise UAV disclosed by the invention, the multi-rotor electric cruise UAV is convenient to move forwards and backwards, the simplicity during operation of the multi-rotor electric cruise UAV is ensured, and the problem that a UAV is complicated in operation is solved; the multi-rotor electriccruise UAV has the advantage that the operation is convenient; a stable ascending and descending effect of the multi-rotor electric cruise UAV is achieved, the whole stability of the multi-rotor electric cruise UAV is ensured, the problem that the UAV cannot ascend and descend stably is solved, and the multi-rotor electric cruise UAV has the advantage that the whole multi-rotor electric cruise UAV is stable.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a multi-rotor electric cruise unmanned aerial vehicle. Background technique [0002] Unmanned aircraft, referred to as "unmanned aerial vehicle", or "UAV" in English, is an unmanned aircraft that is controlled by radio remote control equipment and its own program control device, or is completely or intermittently operated autonomously by an on-board computer. [0003] UAVs have become indispensable in modern society. Both military and civilian use are a great boost to people. Therefore, UAVs have brought a lot of convenience to our lives. However, the current UAVs are complicated to operate and have various structures. It is not easy to use, so we propose a multi-rotor electric cruise drone. Contents of the invention [0004] (1) Solved technical problems [0005] Aiming at the deficiencies of the prior art, the present invention provides a multi-rotor electr...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C27/12B64D35/00B64C25/58
CPCB64C27/08B64C25/58B64C27/12B64D35/00
Inventor 陈伟
Owner 扬州飞虎航空科技有限公司
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