A tail zipline type air-based unmanned aerial vehicle launching device and launching method

A technology for launching devices and unmanned aerial vehicles, which is applied to launch devices, aircraft parts, transportation and packaging, etc., can solve the problems of unprotected UAVs crossing turbulent flow areas, low delivery efficiency, and low launch safety. Achieve the effect of high launch success rate and efficiency, wide application range, and ensure launch 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

[0003] Existing UAV space-based launch methods and devices such as patents CN204507271U, CN207417155U, and CN205998129U etc., mostly adopt the gravity launch method, which does not protect the UAV from passing through the turbulent flow area, and the launch safety is low, which is easy to cause unmanned The machine stalls, and the delivery efficiency is not high

Method used

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  • A tail zipline type air-based unmanned aerial vehicle launching device and launching method
  • A tail zipline type air-based unmanned aerial vehicle launching device and launching method
  • A tail zipline type air-based unmanned aerial vehicle launching device and launching method

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Embodiment Construction

[0034] The following combined with the accompanying drawings back to the invention to make a further introduction, a tail zipline type air-based UAV launch device, comprising a winch 1, zipline 3, positioning pulley 2, attitude control device 4, guiding umbrella 5, the winch 1 is provided inside the mother fuselage, the positioning pulley 3 is set at the edge of the door behind the mother fuselage, the zipline 3 end is fixed on the winch 1, the other end is connected with the guiding umbrella 5 after the positioning pulley 2, the zipline 3 is divided into a sliding area and a disengagement zone, and the boundary between the sliding area and the disengagement zone is the disengagement port , the attitude control device 4 is disposed on the disengagement zone, adjacent to the disengagement port.

[0035] The attitude control apparatus comprises a balanced fuselage 4-3, two elevator hinges 4-4, two rudder hinges 4-5, two elevators 4-1, two rudders 4-2, one end of the two elevator hin...

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Abstract

The invention discloses a tail zipline-type air-based unmanned aerial vehicle launching device and a launching method, including a winch, a zipline, a positioning pulley, an attitude control device, and a guiding parachute. On the edge of the rear cabin door of the fuselage, one end of the slide cable is fixed on the winch, and the other end is connected to the guide parachute after passing through the positioning pulley. The slide cable is divided into a sliding area and a disengagement area. Set on the detachment area, adjacent to the detachment port, the present invention can realize multiple UAVs to launch sequentially through a set of equipment, and the UAVs can directly slide through the turbulent flow area to carry out a safe airflow stabilization area, and the launch is successful The rate and efficiency are high, and batch sequential launch can be realized.

Description

Technical field [0001] The present invention relates to the field of aircraft air-based launch technology, in particular to a tail zipline type air-based UAV launch device and launch method. Background [0002] With the spurt development of UAV technology, UAVs have gradually been widely used in many military and civilian fields. Especially in the military field, "drone swarm tactics" have been highly valued by countries around the world. However, due to the general small weight, low speed and limited combat radius of small and medium-sized UAVs, they cannot perform long-distance combat tasks and cannot effectively play the advantages of swarm operations, which limits the application scope of small and medium-sized UAVs. To this end, people have proposed the "mother and child aircraft" program, that is, the mother aircraft with a large range and a large load will transport the unmanned aerial vehicle to the mission area, and realize the large number and rapid launch of the UAV t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D1/02B64D5/00B64D9/00
Inventor 胡志勇付强贾利勇马泽孟
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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