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Unmanned aerial vehicle throwing device and unmanned aerial vehicle

A technology of unmanned aerial vehicles and driving motors, applied in the field of unmanned aerial vehicles, can solve the problems of fixing and inflexible delivery of rescue supplies

Active Publication Date: 2017-07-18
昆山合朗航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The object of the present invention is to provide a UAV throwing device and a UAV, so as to solve the technical problem of the UAV in the process of delivering materials in the prior art, the fixation and inflexibility of delivery of rescue materials

Method used

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  • Unmanned aerial vehicle throwing device and unmanned aerial vehicle
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  • Unmanned aerial vehicle throwing device and unmanned aerial vehicle

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Embodiment Construction

[0061] The technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Apparently, the described embodiments are some of the embodiments of the present invention, but not all of them. 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.

[0062] In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer" etc. The indicated orientation or positional relationship is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, ...

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Abstract

The invention provides an unmanned aerial vehicle throwing device and an unmanned aerial vehicle. The unmanned aerial vehicle throwing device comprises at least one driving motor, at least one rocker mechanism and at least one locking mechanism, wherein the locking mechanism comprises a locking part which is arranged at a device main body; the rocker mechanism comprises a first rocker rod and a bearing shaft; the output end of the driving motor is moveable connected with the bearing shaft through the first rocker rod and is used for driving the bearing shaft to open or close the locking part through the first rocker rod. According to the technical scheme, the first rocker rod can be driven by the driving motor to rotate, furthermore the bearing shaft is driven to move through the first rocker rod, then the bearing shaft can open or close the locking part, relief goods can be put into or taken out from the locking part when the locking part is opened, and the relief goods can be fixedly connected with a throwing device when the locking part is closed. The structure is simple to operate, fixation and launching of the relief goods can be regulated, and the relief goods can be thrown more flexibly and reliably.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle throwing device and an unmanned aerial vehicle. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. [0003] There is no cockpit on the fuselage of the UAV, but equipment such as autopilot and program control device are installed. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. [0004] The UAV can take off like an ordinary aircraft under radio control or be launched into the air with a booster rocket, or it can be brought into the air by the parent aircraft for flight. When recovering, it can automatically land in the same way as the common aircraft landing pro...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D1/02
CPCB64D1/02B64U2101/00Y02T50/40
Inventor 田瑜江文彦王培乐
Owner 昆山合朗航空科技有限公司
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