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Unmanned aerial vehicle retractable type ski recovery device

A recovery device and machine-retractable technology, applied in the field of unmanned aerial vehicle retractable skid recovery device, can solve the problems of increasing the use cost of unmanned aerial vehicles, affecting the reconnaissance performance of unmanned aerial vehicles, poor performance stability and reliability, etc., to achieve Good landing buffer performance, stable and reliable cost, and the effect of improving service life

Pending Publication Date: 2018-10-19
西安爱生无人机技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The existing UAV recovery device has a complex structure, high cost, poor performance stability and reliability, which seriously affects the reconnaissance performance of the UAV during flight, and has a short service life, which increases the cost of using the UAV.

Method used

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  • Unmanned aerial vehicle retractable type ski recovery device
  • Unmanned aerial vehicle retractable type ski recovery device
  • Unmanned aerial vehicle retractable type ski recovery device

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specific Embodiment approach

[0037] Figure 1 to Figure 13Shows a specific embodiment of the present invention, a retractable skid recovery device for drones, including a body 1, an electromagnetic switch 2, a front shrink cylinder 3, a skid 4, a skid wear-resistant layer 5, and a front slide seat 6. Front connecting bolt 7, front shock absorber 8, suction cup 9, rotating bracket 10, front slider 11, disengagement mechanism 12, front slide base 13, middle fixed base 14, first rotating shaft 15, mounting bracket 16, rear Connecting bolt 17, rear sliding seat 18, rear sliding seat base 19, metal plow 20, rear sliding block 21, rear shock absorber 22 and rear shrinking cylinder 23; the front shrinking cylinder 3 is fixedly installed inside the belly of the body 1 , the top end of the front shock absorber 8 is fixedly installed on the bottom of the front shrink cylinder 3 and the bottom end of the front shock absorber 8 is installed on the front slider 11 through the lifting lug and the front connecting bolt ...

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Abstract

The invention discloses an unmanned aerial vehicle retractable type ski recovery device. The unmanned aerial vehicle retractable type ski recovery device comprises that a front shrinking cylinder is installed inside a belly of a machine body, the top end of a front shock absorber is fixedly installed at the bottom of the front shrinking cylinder and the bottom end of the shock absorber is installed on a front sliding block through a hanging lug and a connecting bolt, the front sliding block is installed in a guide groove of a front sliding seat, and the front sliding seat is installed on a front sliding seat base. An electromagnetic switch is installed on the bottom face of the belly of the machine body, and the electromagnetic switch is located right above a suction cup. A rear shrinkingcylinder is installed in a belly of the machine body, the top end of a rear shock absorber is fixedly installed at the bottom of the rear shirking cylinder and the bottom end of the rear shock absorber is installed on a rear sliding block through a hanging lug and a connecting bolt, and metal ploughs are installed on the outside of two sides of the rear end of a ski. The unmanned aerial vehicle retractable type ski recovery device is simple in structure and realizable in separation, and can obtain good landing buffering performance; a replaceable wear resistant layer is installed on the frontpart of the ski to effectively protect a ski body structure; and the metal ploughs are installed on the rear portion of the ski to play the role of stable guidance and deceleration.

Description

technical field [0001] The invention relates to the technical field of UAV landing, in particular to a UAV retractable skid recovery device. Background technique [0002] In the UAV system, the vast majority of UAVs take off by launching from the launcher, rolling off the take-off vehicle to help the flight, and launching the parent aircraft. There is no need to consider the need for "starting". Compared with the wheel system, the skid system has the following characteristics: (1) The retractable skid device has a simple structure, and the radar echo is very small, and it will not hinder the field of view of the effective reconnaissance load; (2) The skid and recovery The friction of the site can make the aircraft decelerate in a short time and distance until it comes to a complete stop, eliminating the need for auxiliary deceleration devices such as brake systems or other arresting equipment in the wheel recovery device; (3) the skid has no requirements for the recovery si...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/52B64C25/58B64C25/10B64C25/22B64C39/02
CPCB64C25/10B64C25/22B64C25/52B64C25/58B64C39/02
Inventor 曹正阳李大健王宝军吴建军
Owner 西安爱生无人机技术有限公司
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