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Unmanned aerial vehicle group launching mechanism

A technology of unmanned aerial vehicle and launching mechanism, which is applied in the direction of launch/tow transmission device, etc., can solve the problems of low launch efficiency and speed, large impact damage of UAV, and high launch cost, achieve automatic launch, avoid motion interference, improve The effect of emission efficiency

Active Publication Date: 2021-07-23
CHANGAN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to provide a UAV group sending mechanism to solve the problems of low launch efficiency and speed, complicated operation, large impact damage of UAVs, and high launch cost in the above-mentioned background technology.

Method used

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  • Unmanned aerial vehicle group launching mechanism

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specific Embodiment approach 1

[0050] Specific implementation mode one: please refer to Figure 1-20 , the present invention provides a technical solution: an unmanned aerial vehicle group sending mechanism, comprising:

[0051] The motor 1, as a power source, provides power for the operation of the mechanism, and the motor output shaft 12 of the motor 1 is connected to the reduction system 2;

[0052] The deceleration system 2 is used to decelerate the input power and increase the torque and drive the launch mechanism 3 to work. The deceleration system 2 is connected to the transmission assembly 5 through the first bevel gear 262;

[0053] The launch mechanism 3 is used to launch the unmanned aerial vehicle;

[0054] The delivery mechanism 4 is used to transport the unmanned aerial vehicle into the launch mechanism 3;

[0055] The transmission assembly 5 is used to transmit the power to the conveying mechanism 4;

[0056] The motor 1 , the launching mechanism 3 and the transmission assembly 5 are all in...

specific Embodiment approach 2

[0059] Specific embodiment two: this embodiment is a further limitation of specific embodiment one, such as figure 1 and figure 2 As shown, the motor bottom plate 11 of the motor 1 is screwed and fixed together with the carrier plate 41, the motor output shaft 12 of the motor 1 is connected to the first-stage gear shaft 21 through a coupling 211, and the motor 1 provides the launching mechanism 3 and the conveying mechanism 4 with power.

specific Embodiment approach 3

[0060] Specific implementation mode three: this implementation mode is a further limitation of specific implementation mode one, such as Figure 3-6 As shown, the reduction system 2 includes a first-stage gear shaft 21, a second-stage gear shaft 22, a third-stage gear shaft 23, a direction gear shaft 24, an output gear shaft I 25 and an output gear shaft II 26, and the first-stage gear shaft 21 A shaft coupling 211 is installed at the input end, a pinion is arranged at the output end of the first stage gear shaft 21, a large gear and a pinion are respectively fixed at both ends of the second stage gear shaft 22, and a large gear and a pinion are respectively fixed at both ends of the third stage gear shaft 23. A large gear and a pinion are respectively fixed, the pinion of the first stage gear shaft 21 meshes with the large gear of the second stage gear shaft 22, the small gear of the second stage gear shaft 22 meshes with the large gear of the third stage gear shaft 23 The pi...

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Abstract

The invention discloses an unmanned aerial vehicle group launching mechanism which comprises a motor, a speed reduction system, a launching mechanism, a conveying mechanism and a transmission assembly, wherein the motor serves as a power source and provides power for mechanism operation, and a motor output shaft of the motor is connected with the speed reduction system; the speed reduction system is used for reducing the speed and increasing the torque of the input power and driving the launching mechanism to work, and the speed reduction system is connected with the transmission assembly through a first bevel gear; the launching mechanism is used for launching the unmanned aerial vehicle; the conveying mechanism is used for conveying the unmanned aerial vehicle into the launching mechanism; the transmission assembly is used for transmitting power to the conveying mechanism; and the motor, the launching mechanism and the transmission assembly are all installed on a carrying disc of the conveying mechanism. According to the unmanned aerial vehicle group launching mechanism, a mechanical cluster launching system is adopted, compared with a common single launching technology, high-frequency, rapid and automatic launching of folding wing unmanned aerial vehicles can be achieved, and compared with a common gunpowder actuation type cluster launching technology, the unmanned aerial vehicle group launching mechanism is small in impact on the unmanned aerial vehicles, light in damage and beneficial to recycling of the unmanned aerial vehicles.

Description

technical field [0001] The invention relates to the technical field related to UAV group launch, in particular to a UAV group launch mechanism. Background technique [0002] UAV cluster technology not only has unique advantages such as fast response speed, low cost of use, and flexible deployment of UAVs, but also has significant advantages such as more accurate information collection capabilities, more stable execution capabilities, and stronger fault tolerance. Therefore, UAV swarm operations have developed rapidly, and UAV swarm launch technology is a prerequisite for UAV swarm operations, but the existing UAV launch technology is mainly based on a single launch, and it is difficult to It is difficult to meet the needs of cluster operations. At the same time, some gunpowder-activated cluster launch technologies have great impact and damage to drones, which is not conducive to the recovery and launch of drones. After completing a round of launch missions, gunpowder needs t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/04B64F1/06
CPCB64F1/04B64F1/06
Inventor 庞欢王道成刘敬一石东阳
Owner CHANGAN UNIV
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