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A ground track launching device for a soft-wing unmanned aerial vehicle and a method for launching and taking off of a soft-wing unmanned aerial vehicle

A technology for orbital launch and unmanned aerial vehicles, applied in the field of unmanned aerial vehicles, it can solve problems such as needs and inability to adapt to rapid launch, and achieve the effect of improving efficiency and speed

Active Publication Date: 2018-05-04
XIANGYANG HONGWEI AIRCRAFT
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] Aiming at the above defects or improvement needs of the prior art, the present invention provides a ground track launching device for a soft-wing unmanned aerial vehicle, which can realize automatic and reliable launch and take-off of the soft-wing unmanned aerial vehicle through an optimized structure improvement, thereby Solve the defects that the current launch device needs to be towed by a tractor and cannot adapt to the needs of rapid launch of multiple drones

Method used

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  • A ground track launching device for a soft-wing unmanned aerial vehicle and a method for launching and taking off of a soft-wing unmanned aerial vehicle
  • A ground track launching device for a soft-wing unmanned aerial vehicle and a method for launching and taking off of a soft-wing unmanned aerial vehicle
  • A ground track launching device for a soft-wing unmanned aerial vehicle and a method for launching and taking off of a soft-wing unmanned aerial vehicle

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Embodiment Construction

[0033] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below may be combined with each other as long as they do not constitute a conflict with each other.

[0034] A soft-wing unmanned aerial vehicle ground track launching device related to the embodiment of the present invention is used to realize the launch and take-off of the soft-wing unmanned aerial vehicle 1. The launching device includes a ground track 2, an acceleration system 3, and preferably also includes an automatic steering device. 4.

[0035] The soft-wing unmanned aerial vehicle 1 d...

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Abstract

The invention discloses a flexible wing unmanned aerial vehicle ground rail launcher which comprises a ground rail and an accelerating system. The ground rail comprises a launching rail. A groove is formed in the launching rail in the launching and takeoff direction. The launching rail comprises a locking rail located at a front launching and takeoff section and a sliding rail located at a rear launching and takeoff section. A limiting groove is further formed in the bottom of the groove of the locking rail. The accelerating system comprises a transmission belt and a locking releasing mechanism arranged on the transmission belt. When the transmission belt is driven, the transmission belt can drive an unmanned aerial vehicle to slide and accelerate on the locking rail, and when the unmanned aerial vehicle slides to the tail end of the locking rail and enters the sliding rail, the locking releasing mechanism can be separated from a vehicle body, and therefore the unmanned aerial vehicle continuously slides on the sliding rail and takes off after reaching the takeoff speed. By the adoption of the flexible wing unmanned aerial vehicle ground rail launcher, the flexible wing unmanned aerial vehicle can be automatically launched and take off, and therefore the defects that an existing launcher needs to be dragged by a tractor and cannot meet the requirement for launching multiple unmanned aerial vehicles quickly are overcome.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a ground track launching device for a soft-wing unmanned aerial vehicle and a method for launching and taking off of a soft-wing unmanned aerial vehicle. Background technique [0002] The soft-wing UAV is a kind of suspended aircraft with a parafoil as the wing. Its launch method mainly depends on the way of towing by the ground vehicle to launch and take off. The ground vehicle accelerates to the take-off speed of the soft-wing UAV, and then releases it. Then the soft-wing UAV leaves the vehicle and takes off. [0003] When launching and taking off by being towed by a ground vehicle, first fix the soft-wing UAV to the towing vehicle, then hang the parafoil, and the traction and towing vehicle accelerates to 50Km / h~60Km / h. The towing vehicle is separated, the soft-wing UAV is lifted into the air, and then accelerates to climb to complete take-off. [0004] This launch an...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F1/04
CPCB64F1/04
Inventor 薛富利郭海军韩晋阳盛光喜陈保申于腾徐杰
Owner XIANGYANG HONGWEI AIRCRAFT
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