Launching and recovery system for small unmanned aerial vehicle

A small unmanned aerial vehicle and recovery system technology, which is applied in the field of launch and recovery systems, can solve problems such as methods that cannot meet the requirements of use, and achieve the effects of facilitating launch, ensuring different statics, and ensuring quality

Active Publication Date: 2018-03-30
四川汉科计算机信息技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

During the recovery process, people need to park the small drone in a static position before it can be recovered. In order to reduce the possibility of target exposure, the drone needs to be recovered at any time, and the static recovery method cannot meet the use requirements

Method used

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  • Launching and recovery system for small unmanned aerial vehicle
  • Launching and recovery system for small unmanned aerial vehicle
  • Launching and recovery system for small unmanned aerial vehicle

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Embodiment Construction

[0026] The present invention will be further described below in conjunction with the accompanying drawings, but the protection scope of the present invention is not limited to the following description.

[0027] Such as figure 1 As shown, the launch and recovery system of the small unmanned aerial vehicle includes a car body 1. A launch chamber is opened at the rear side of the tail of the car body 1 near the roof position, and a launch mechanism 2 is installed in the launch chamber. There is a recovery cavity near the roof position at the top, and a recovery mechanism 3 is installed in the recovery cavity, and a channel connecting the two is provided between the launching cavity and the recovery cavity, and a conveying mechanism 4 is installed in the channel.

[0028] Specifically, the launch mechanism 2 includes an elastic launch device 5, which is arranged on the front wall of the launch chamber, and has a chute and a guide rail 6 on the bottom surface of the launch chamber...

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Abstract

The invention relates to a launching and recovery system for a small unmanned aerial vehicle. The launching and recovery system for the small unmanned aerial vehicle comprises a vehicle body; a launching chamber is formed in the rear side, close to the roof position, of the tail part of the vehicle body; a launching mechanism is mounted in the launching chamber; a recovery chamber is formed in therear part, close to the roof position, of the left side of the vehicle body; a recovery mechanism is mounted in the recovery chamber; a through groove, which is used for enabling the launching chamber to be in communication with the recovery chamber, is formed between the launching chamber and the recovery chamber; and a conveying mechanism is mounted in the through groove. The launching and recovery system for the small unmanned aerial vehicle has the advantages of good concealing performance and high maneuvering characteristic.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a launch and recovery system for small unmanned aerial vehicles. Background technique [0002] Unmanned aircraft, referred to as Unmanned Aerial Vehicle (UAV), has the advantages of flexible maneuverability, quick response, unmanned flight, and low operation requirements. UAVs can realize real-time image transmission and detection of high-risk areas by carrying multiple types of sensors. At present, the demand for drones by the military and police is increasing. For small unmanned aerial vehicles, it is often manually controlled to release, manually operated to fly, and manually operated to recover. In the process of manual release, it is often necessary to release from a stationary place. If it is released in a moving car, it is a dynamic release, but it is difficult to operate. Especially in war or crime fighting, it is very important to release easily. Duri...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/06B64F1/00
CPCB64F1/00B64F1/06
Inventor 曹双华
Owner 四川汉科计算机信息技术有限公司
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