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A recovery device and recovery method for a tail hard space-based unmanned aerial vehicle

A recovery device and drone technology, which is applied to aircraft parts, transportation and packaging, equipment for loading and unloading, etc., can solve the problem of large restrictions on drone body configuration, no docking safety protection measures, and narrow scope of application To achieve the effect of improving docking efficiency, good airflow stability, and improving safety

Active Publication Date: 2022-04-19
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although these methods can realize the recovery of drones, their disadvantages are obvious, and there are no docking safety protection measures. Among them, the methods mentioned in patents CN106516144A and CN205770184U have low recovery efficiency and are prone to collisions between drones. Patent CN107792381A proposes The recovery method obtained has great restrictions on the body configuration of the UAV, and the scope of application is narrow

Method used

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  • A recovery device and recovery method for a tail hard space-based unmanned aerial vehicle
  • A recovery device and recovery method for a tail hard space-based unmanned aerial vehicle
  • A recovery device and recovery method for a tail hard space-based unmanned aerial vehicle

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Embodiment Construction

[0038] The present invention will be further introduced below in conjunction with the accompanying drawings. A tail hard type space-based unmanned aerial vehicle recovery device according to the present invention includes a base machine 1, a manipulator 7, a retractable hard recovery rod 3, a docking device 6, a chain 5, and a winch 4 and the recovery controller 2, the manipulator 7 is installed on the top panel in the cabin above the position of the rear hatch door of the main machine 1 through a bracket, and one end of the retractable hard type recovery rod 3 is fixed on the belly of the main machine 1 fuselage through a rotating shaft, and can Rotating around the shaft, the other end of the retractable hard recovery rod 3 is connected to the docking device 6, one end of the chain 5 is hinged to the retractable hard recovery rod 3, and the other end is connected to the winch 4 arranged inside the fuselage of the main machine 1. The recovery controller 2 is placed in the main ...

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Abstract

The invention discloses a tail hard air-based unmanned aerial vehicle recovery device, which includes a parent machine, a manipulator, a retractable hard recovery rod, a docking device, a chain, a winch and a recovery controller. On the inner top plate, one end of the retractable hard recovery rod is fixed on the belly of the machine body through a rotating shaft, and can rotate around the rotating shaft. The other end of the retractable hard recovery rod is connected to the docking device. The winch installed inside the fuselage of the mother machine is connected, and the recovery controller is placed in the mother machine cabin, and is connected with the retractable hard recovery rod, the winch and the manipulator through the cable. Recycling, and the UAV can be directly retracted into the mother cabin, and the recovery efficiency is high.

Description

technical field [0001] The invention relates to the technical field of aircraft space-based recovery, in particular to a recovery device and recovery method for a tail hard type space-based unmanned aerial vehicle. Background technique [0002] With the blowout development of drone technology, drones have gradually been widely used in many military and civilian fields. Especially in the military field, "UAV swarm tactics" have been highly valued by countries all over the world, and UAV space-based recovery technology is one of the key difficulties in realizing "UAV swarm operations". At present, my country has very limited technology accumulation in the field of UAV space-based recovery technology, and there is no direct design experience and results for reference. There is a big gap with foreign countries, and relevant research is urgently needed. [0003] Existing space-based accurate recovery methods and devices such as patents CN106516144A, CN205770184U and CN107792381A...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D5/00B64D9/00B64D47/00
Inventor 胡志勇任远春艾俊强王启
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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