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Self-charging tail-sitting type unmanned aerial vehicle adaptive to launch canister

A self-charging technology for unmanned aerial vehicles, applied in charging stations, power plant types, motor vehicles, etc., can solve the problems of increasing flight radius, short battery life, and prolonging use time, so as to improve battery life and wing area Effects that increase and increase duration

Pending Publication Date: 2022-07-15
BEIJING LINJIN SPACE AIRCRAFT SYST ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to provide a self-charging tail-sitting UAV adapted to the launch tube, combined with tail-sitting take-off and landing technology, folding wing / rudder technology and wireless charging technology, using the common high-voltage transmission lines in cities and fields to UAVs carry out magnetoelectric conversion charging to prolong their use time, increase their flight radius, and solve the problems of complex scene adaptation and efficient cruising flight of UAVs, and short battery life.

Method used

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  • Self-charging tail-sitting type unmanned aerial vehicle adaptive to launch canister
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  • Self-charging tail-sitting type unmanned aerial vehicle adaptive to launch canister

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Embodiment Construction

[0024] In order to make those skilled in the art better understand the solutions of the present invention, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only Embodiments are part of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0025] This embodiment provides a self-charging tail-mounted UAV adapting to the launch tube. The schematic diagram of the composition is shown in Figure 1. The UAV comprises: a head propeller 1, a propeller drive motor 2, a fuselage 4, Wing actuation motor 5, folding wing 6, rechargeable battery, electromagnetic induction power generation device...

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Abstract

The invention provides a self-charging tail-sitting type unmanned aerial vehicle adaptive to a launch canister. The unmanned aerial vehicle comprises a head propeller, a propeller driving motor, folding wings, wing actuating motors, a fuselage, a rechargeable battery and an electromagnetic induction power generation device, the head propeller is positioned at the head end of the fuselage; the folding wings are located on the two sides of the side wall of the fuselage. The propeller driving motor provides driving force for the head propeller; the wing actuating motors provide driving force for unfolding or folding of the folding wings; the rechargeable battery provides electric energy for the propeller driving motor and the wing actuating motor; and the electromagnetic induction power generation device is used for charging the rechargeable battery.

Description

technical field [0001] The invention belongs to the field of unmanned aerial vehicle design, in particular to a self-charging tail-sitting type unmanned aerial vehicle adapted to a launch tube. Background technique [0002] As a new type of aircraft that takes into account vertical rotor take-off and landing and efficient fixed-wing cruise flight, tail-mounted UAV combines the advantages of rotorcraft and fixed-wing aircraft, and has great advantages in complex application scenarios. Many researches have been carried out at home and abroad, such as the T-Wing tail-mounted UAV designed by the University of Sydney, the single-rotor hover-level flight multi-modal UAV designed by the Massachusetts Institute of Technology, and the Novlit-UAV of Northwestern Polytechnical University. 3 drones, etc. Existing small UAVs are basically powered by batteries, but limited by the energy density of batteries, the flight time of UAVs is very limited. When using UAVs for tasks such as recon...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64C29/02B64C3/56B64C9/02B64C11/00B64D27/24B60L53/12
CPCB64C39/02B64C29/02B64C3/56B64C9/02B64C11/00B64D27/24B60L53/12B60L2200/10B64U50/34B64U10/25B64U50/19B64U2101/00
Inventor 赤丰华曹粟李波张孝南吉申莘武猛郭晓明惠向阳高世琦滕锐焦子涵李铮杨浩薛铮刘宇飞梅杰陈鑫赵楠王哲卢志鎏
Owner BEIJING LINJIN SPACE AIRCRAFT SYST ENG INST
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