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A handheld miniature UAV transmitter

An unmanned aerial vehicle, hand-held technology, applied in the field of launchers, can solve the problem of high manual launch error rate, and achieve the effects of high launch success rate, small restrictions and simple operation

Active Publication Date: 2020-12-11
浙江翔龙航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Technical issues: At present, the miniature fixed-wing UAVs are all hand-throwable, and operators need to be trained on the operation. No one who launches a larger miniature fixed-wing UAV has certain requirements for the site, and at the same time, the error rate of manual launch is relatively high.

Method used

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  • A handheld miniature UAV transmitter
  • A handheld miniature UAV transmitter
  • A handheld miniature UAV transmitter

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Embodiment Construction

[0020] Combine below Figure 1-Figure 5 The present invention is described in detail, and for convenience of description, the orientations mentioned below are now stipulated as follows: figure 1 The up, down, left, right, front and back directions of the projection relationship itself are the same.

[0021] The present invention relates to a hand-held miniature unmanned aerial vehicle launcher, which is mainly used in the launching work of miniature fixed-wing unmanned aerial vehicles. The present invention will be further described below in conjunction with the accompanying drawings of the present invention:

[0022] A kind of hand-held miniature unmanned aerial vehicle launcher described in the present invention comprises box body 11, and described box body 11 is provided with power cavity 15, and described box body 11 is provided with the slide that is positioned at the upper right side of described power cavity 15 chamber 76, the left side of the sliding chamber 76 commun...

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Abstract

The invention discloses a handheld miniature unmanned aerial vehicle launcher. The launcher comprises a box body, a power cavity is formed in the box body, a sliding cavity located above the right ofthe power cavity is arranged in the box body, a power device is arranged in the power cavity, a piston device for realizing a one-way ventilation function is arranged in the power device, a carrying device is slidably connected to the inner wall of the lower side of the sliding cavity, a mechanical claw is arranged at each of the interior of the carrying device and the right end of the piston device, a triggering device is arranged below the power device, and a lithium battery which is positioned on the right side of the triggering device is fixedly connected in the power cavity. An existing miniature fixed-wing unmanned aerial vehicle is in a hand-throwing type, operators need to receive operation training, the launching of a large miniature fixed-wing unmanned aerial vehicle has a certain requirement on the site, and meanwhile, the artificial launching error rate is high.

Description

technical field [0001] The invention relates to the technical field of transmitters, in particular to a handheld miniature unmanned aerial vehicle transmitter. Background technique [0002] At present, the miniature fixed-wing UAVs are all hand-throwable. The launch of micro-UAVs requires a long period of professional training for operators. A run-up distance is required, and there are certain requirements for the launch site. Since manual launch requires a certain amount of experience accumulation, the launch error rate is relatively high. A device that can solve the above-mentioned problems is explained by the present invention. Contents of the invention [0003] Technical issues: At present, the miniature fixed-wing UAVs are all hand-throwable, and operators need to be trained for their operations. No one who launches a larger miniature fixed-wing UAV has certain requirements for the venue, and at the same time, the error rate of manual launch is high. [0004] In orde...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F1/04B64F1/06
CPCB64F1/04B64F1/06
Inventor 胡德荣
Owner 浙江翔龙航空科技有限公司
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