Rotary table type unmanned aerial vehicle continuous ejection device and control method thereof

A technology of ejection device and unmanned aerial vehicle, which is applied in the direction of launch/drag transmission device, etc., can solve problems such as reducing efficiency and increasing manpower, and achieves the effect of shortening the ejection cycle, increasing the ejection frequency, and facilitating rapid formation.

Pending Publication Date: 2018-11-13
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Most of the existing ejection take-off methods are single launch, that is, each time a UAV is launched, after the ejection frame is reset, the UAV is artificially erected on the ejection frame trailer, and then the second operation is performed, which greatly increases the manpower It also reduces the efficiency

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  • Rotary table type unmanned aerial vehicle continuous ejection device and control method thereof

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Embodiment Construction

[0032] Below in conjunction with accompanying drawing, technical scheme of the present invention is described in further detail:

[0033] This invention may be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art. In the drawings, components are exaggerated for clarity.

[0034] Such as figure 1 As shown, the present invention discloses a turntable type unmanned aerial vehicle continuous ejection device, which includes a parking platform, an electric telescopic rod, an ejection frame and a control module; the parking platform includes a base, a turntable, a turntable, a driving motor, a driving gear and several machine bracket; the turntable is cylindrical, and its lower end surface is connected to the base through bearings, and can rotate freely relat...

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Abstract

The invention discloses a rotary table type unmanned aerial vehicle continuous ejection device and a control method thereof. The ejection device comprises a parking platform, an electric telescopic rod, an ejection frame and a control module. The parking platform comprises a base, a rotating platform, a rotary table, a driving motor, a driving gear and a plurality of unmanned aerial vehicle brackets. The rotating platform is column-shaped, and the lower end surface of the rotating platform is connected with the base through bearings. A ring of racks are circumferentially arranged on the outerwall of the rotating platform. An output shaft of the driving motor is fixedly connected with a rotating shaft of the driving gear. The driving gear meshes with the racks on the outer wall of the rotating platform. The lower end surface of the rotary table is fixedly connected with the upper end surface of the rotating platform. The electric telescopic rod is disposed on the upper end surface of the rotating platform. The control module is electrically connected with the driving motor, the electric telescopic rod and the ejection frame separately. The rotary table type unmanned aerial vehiclecontinuous ejection device and the control method thereof solve the problem that single launching and a launching interval are long in time when deck operations of an unmanned aerial vehicle, improvethe launching rate of the unmanned aerial vehicle, shorten the launching period of the unmanned aerial vehicle, and are beneficial to the rapid formation of combat formation of an unmanned aerial vehicle group.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicle automation, in particular to a turntable type unmanned aerial vehicle continuous ejection device and a control method thereof. Background technique [0002] With the rapid development of modern science and technology, drones have gradually been valued by various countries, and they have played a huge role in both military and civilian fields. With the research on UAVs, people have gradually found that the launch of UAVs has a direct impact on the requirements of the UAV system's battlefield survivability, reusability, regional adaptability, and operational flexibility. One of the most difficult and critical phases of drone operations. [0003] UAV launch refers to the process of enabling the UAV to reach a certain height and speed in a certain place and through a certain method. Mainly divided into taxi takeoff, vertical takeoff, hand-throw takeoff, catapult takeoff, rocket-assisted takeof...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/06
CPCB64F1/06
Inventor 魏小辉张钊李天童聂宏房兴波
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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