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Ejection-type unmanned aerial vehicle launching device

A technology of a launching device and an unmanned aerial vehicle, which is applied in the field of unmanned aerial vehicle launching, can solve the problems of high use cost, high price, and difficulty in reaching the launching site of an unlocking mechanism, and achieves the effect of simple structure and reduced use cost.

Inactive Publication Date: 2018-06-29
成都草寓住房租赁有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For the way of hand-throwing take-off, it is difficult to guarantee the normal attitude of the UAV when it takes off, and it is very easy to fail
The ejection methods are all vehicle-mounted or fixed, which is not convenient to carry and travel on the complex, and it is difficult to reach the most favorable launch location. There are great restrictions on the performance of the UAV. The mechanism has high reliability, low cost of use, simple operation, and can be recycled
In the past, the vehicle-mounted launch used the electric squib mechanism to unlock, but the unlocking mechanism has a high cost of use. The electric squib is a pyrotechnic product, which is expensive. There are strict requirements for the purchase and transportation of the electric squib; It is a permanent product, it needs to be replaced once it is launched, and it cannot be recycled

Method used

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  • Ejection-type unmanned aerial vehicle launching device

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Embodiment Construction

[0012] In order to have a clearer understanding of the technical features, purposes and effects of the present invention, the specific implementation manners of the present invention will now be described with reference to the accompanying drawings.

[0013] like figure 1 As shown, a catapult-type unmanned aerial vehicle launching device includes a base 1, a launching platform 2, a locking mechanism and a controller. The top of the base 1 is provided with a spring perpendicular to it, and the spring is in a compressed state. The top of the spring is provided with a launching platform 2, and the locking mechanism includes a first lock body 3, a second lock body 4, a lifting power device 5, a rotating disk 6 and a motor, and the rotating disk 6 is fixedly installed on the base 1 , the lifting power device 5 is fixedly installed on the top surface of the rotating disk 6, and the bottom surface of the rotating disk 6 is connected to the shaft of the motor. The first lock body 3 an...

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PUM

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Abstract

The invention discloses an ejection-type unmanned aerial vehicle launching device. The device includes a base, a launching pad, a locking mechanism and a control device; the top of the base is provided with a spring perpendicular to the base, the top end of the spring is provided with the launching pad, the locking mechanism includes a first lock body, a second lock body, a lifting power plant andan electromagnetic control device, the lifting power plant is fixedly installed on the base, the first lock body is connected with the driving shaft of the lifting power plant, the bottom surface ofthe launching pad is provided with a square groove, a blind hole is formed in the side surface of the square groove, one end of the second lock body is hinged onto the launching pad, a spring reset part is placed in the blind hole, one end of the spring reset part is connected with the second lock body, one close ends of the first lock body and the second lock body are fixedly provided with a first lock block and a second lock block respectively, and the first lock body is provided with an electromagnetic control mechanism. The device has the advantages of simple structure and low use costs.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a catapult-type unmanned aerial vehicle launching device. Background technique [0002] At present, there are two main ways to take off small UAVs: hand-throwing and ejection. For the way of hand-throwing take-off, it is difficult to guarantee the normal attitude of the UAV when it takes off, and it is very easy to fail. The ejection methods are all vehicle-mounted or fixed, which is not convenient to carry and travel on the complex, and it is difficult to reach the most favorable launch location. There are great restrictions on the performance of the UAV. The mechanism has high reliability, low use cost, simple operation and can be recycled. In the past, the vehicle-mounted launch used the electric squib mechanism to unlock, but the unlocking mechanism has a high cost of use. The electric squib is a pyrotechnic product, which is expensive. There are strict req...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/06
CPCB64F1/06B64U70/70
Inventor 徐凡富叶薄迪刘国伟徐明新
Owner 成都草寓住房租赁有限公司
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