Unmanned aerial vehicle vacuous basis rapid launching device and method based on aviation tow cable and tow target system
A technology for launching devices and unmanned aerial vehicles, which is applied in the directions of launch/drag transmission devices, aircraft parts, transportation and packaging, etc., to achieve the effect of fewer participants, improved air launch efficiency, and simple operation.
Active Publication Date: 2018-03-13
BEIHANG UNIV
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Problems solved by technology
[0005] In view of the above-mentioned problems, the present invention mainly solves the problem of rapid launch of bee colony UAV air-based, and applies the technology of the towed target system to the air-based launch process of the UAV, and proposes a system based on the aerial towed cable towed target Unmanned aerial vehicle air-based rapid launching device and method thereof
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[0028] Such as figure 1 Shown, a kind of unmanned aerial vehicle space-based rapid launching device based on aerial towed target system, this launcher includes mounting bracket (not shown in the figure), aviation winch 5, aerial towed target system and multiple launching Disengagement device 3; wherein, the tow cable tow target system is composed of tow cable 2 and stable tow target 4; the mounting bracket is retractable, and can be received inside the body of the mother machine 1 during the process of transporting the UAV by the mother machine 1 , does not affect the aerodynamic shape of the parent machine 1; when in use, the hatch door of the parent machine 1 is opened, and the mounting bracket can extend out of the parent machine 1 to perform the air-based launching mission of the unmanned aerial vehicle; the aviation winch 5 is installed and fixed on the installation The lower end of the support realizes the release of the aerial towing cable towing target system by the av...
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Abstract
The invention discloses an unmanned aerial vehicle vacuous basis rapid launching device and method based on an aviation tow cable and tow target system. The unmanned aerial vehicle vacuous basis rapidlaunching device comprises a retractable mounting support, the aviation tow cable and tow target system and a launching detaching device. The launching detaching device is of a lug sheet structure ina remote control explosive bolted connection mode. By means of the aviation tow cable and tow target technology, a buzzer unmanned aerial vehicle is connected to a tow cable through the launching device, and launching of the unmanned aerial vehicle is achieved along with releasing of the tow cable. The space utilization efficiency of the structure of the launching device is high, simultaneous launching of a certain amount of unmanned aerial vehicles can be achieved, and the time consumed in the launching process of an unmanned aerial vehicle colony is shortened. A certain height difference exists between every two adjacent small-sized unmanned aerial vehicles in the launching process, and the damage risks of the unmanned aerial vehicles and a mother vehicle are reduced.
Description
technical field [0001] The invention discloses an air-based rapid launch device and method for an unmanned aerial vehicle based on an aerial towed target system, and belongs to the field of unmanned aerial vehicle launch in aviation vehicle technology. Background technique [0002] Since the 1930s, people have longed to realize the air-based launch of aircraft. This launch method transports the sub-aircraft to the mission area through a mother aircraft with a large range and load, which can greatly increase the cruising radius of the sub-aircraft and get rid of It eliminates the ground airport restrictions and increases the flexibility of sub-aircraft take-off and landing. However, limited by technology, risk and cost, aircraft space-based launch technology has not been well developed. [0003] In recent years, with the development of UAV technology and the recent proposal of swarm UAV tactics, the space-based launch technology of small UAVs has attracted more and more atte...
Claims
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Login to View More IPC IPC(8): B64D5/00B64F1/04
CPCB64D5/00B64F1/04
Inventor 马铁林别大卫张晓鸥张秦岭
Owner BEIHANG UNIV