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Empennage type unmanned aerial vehicle launching and recovering device

A technology of drones and tail fins, applied in the field of drones, can solve the problems of long sliding distance and cumbersome recovery methods, and achieve the effect of reducing the height of the bow, restraining the bow from being too high, and ensuring the safety of navigation

Pending Publication Date: 2021-01-15
708TH RES INST OF CSSC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to solve the technical problems that the unmanned aerial vehicle needs to take off to take off the long running distance and the recovery method is cumbersome.

Method used

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  • Empennage type unmanned aerial vehicle launching and recovering device
  • Empennage type unmanned aerial vehicle launching and recovering device
  • Empennage type unmanned aerial vehicle launching and recovering device

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Embodiment Construction

[0026] In order to make the present invention more obvious and understandable, the preferred embodiments are described in detail as follows in conjunction with the accompanying drawings:

[0027] Such as Figure 1-6 As shown, the present invention provides a tail-wing type launch and recovery UAV device, including a left vertical installation surface 1, a right vertical installation surface 2, a launch recovery track 6, a sliding block, a traction rope, a traction motor, and a recovery chain , unmanned aerial vehicle 15 and unmanned aerial vehicle tail hook 20; The upper end face of the left vertical installation elevation 1 and the right vertical installation elevation 2 that is provided with in parallel is respectively provided with launch recovery track 6; Launch recovery track 6 is provided with There is a sliding block; the sliding block is connected with the traction motor by a traction rope; a recovery chain is provided between the sliding blocks on the launch recovery ...

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Abstract

The invention relates to an empennage type unmanned aerial vehicle launching and recovering device and belongs to the technical field of unmanned aerial vehicles. The device comprises a left verticalinstallation face, a right vertical installation face, launching recovery rails, a sliding block, a traction rope, a traction motor, a recovery chain, an unmanned aerial vehicle and an unmanned aerialvehicle tail hook. The launching recovery rails are arranged on the upper end surfaces of a left vertical installation surface and a right vertical installation surface which are arranged in the device in parallel; a sliding block is arranged on each launching recovery rail; the sliding blocks are connected with the traction motor through traction ropes; the recovery chain is arranged between thesliding blocks on the launching recovery rails on the two sides; and the unmanned aerial vehicle tail hook is arranged below the unmanned aerial vehicle. Main equipment of the device is small in occupied size and can be arranged and installed in a narrow space; extra torque can be provided, the rising height of high-speed sailing of the ship is effectively reduced, and sailing safety is improved.

Description

technical field [0001] The invention relates to a tail-type launching and recovering unmanned aerial vehicle device, which belongs to the technical field of unmanned aerial vehicles. Background technique [0002] Small fixed-wing UAVs are widely used. They can not only realize aerial reconnaissance, find suspicious targets, but also have functions such as terrain survey and topographic map drawing. With the promotion of platforms and the demand for use in different scenarios, vehicle-mounted and ship-borne drones have emerged as the times require. However, how to launch and recover drones in narrow spaces has become the primary problem to be solved. [0003] At present, the assisted take-off of small fixed-wing UAVs mainly includes rubber band ejection, hydraulic ejection, liquid-gas mixed ejection, and rocket boosting. The rubber band ejection has a simple structure and is mainly aimed at model aircraft or demonstration small and miniature fixed-wing UAVs. The rubber band ...

Claims

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Application Information

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IPC IPC(8): B64F1/06B64F1/02B64C25/68
CPCB64C25/68B64F1/025B64F1/06
Inventor 赵启兵黄斌陶益徐道铭陆佳骏马凯何巍
Owner 708TH RES INST OF CSSC
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