Separable four-propeller double-wing unmanned aerial vehicle

An unmanned aerial vehicle, a separate technology, applied in the field of unmanned aerial vehicles, can solve the problems of unexplained application conditions and the inability of the aircraft to achieve separation, and achieve the effects of high hit rate, low cost and strong flexibility

Active Publication Date: 2017-01-04
SHANGHAI JIAO TONG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the aircraft cannot be separated, a

Method used

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  • Separable four-propeller double-wing unmanned aerial vehicle
  • Separable four-propeller double-wing unmanned aerial vehicle
  • Separable four-propeller double-wing unmanned aerial vehicle

Examples

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Embodiment Construction

[0033] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0034] Such as figure 1 As shown, the present embodiment provides a detachable four-blade biplane drone, including: a four-blade biplane drone composed of a double-blade monoplane drone 1 and a double-blade monoplane drone 2, and a net-catching crane. Cabin 9, net-catching umbrella cabin 8; wherein: net-catching pod 9 is two, that is, the first net-catching pod and the second net-catching pod, and the first net-catching pod and the second net-catching pod pass through the first net-catching pod an...

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Abstract

The invention provides a separable four-propeller double-wing unmanned aerial vehicle. The separable four-propeller double-wing unmanned aerial vehicle comprises a first double-propeller single-wing unmanned aerial vehicle, a second double-propeller single-wing unmanned aerial vehicle, a first arrestment net parachute cabin, a second arrestment net parachute cabin, a first arrestment net pod and a second arrestment net pod, wherein the first double-propeller single-wing unmanned aerial vehicle is connected with the first arrestment net parachute cabin through a first connection mechanism, and the first arrestment net pod is in rigid connection with the first arrestment net parachute cabin; the second double-propeller single-wing unmanned aerial vehicle is connected with the second arrestment net parachute cabin through a second connection mechanism, and the second arrestment net pod is in rigid connection with the second arrestment net parachute cabin; and the first arrestment net pod is connected with the second arrestment net pod through a third connection mechanism. According to the separable four-propeller double-wing unmanned aerial vehicle, arrestment is conducted through cooperation of the two double-propeller single-wing unmanned aerial vehicles, the flexibility is high, secondary arrestment can be carried out, and the recoverability is achieved; and the cost is low, and the separable four-propeller double-wing unmanned aerial vehicle is applied to arrestment of aerial low, slow and small targets.

Description

technical field [0001] The present invention relates to the technical field of unmanned aerial vehicles, in particular to a detachable four-bladed biplane unmanned aerial vehicle. Background technique [0002] With the continuous maturity of remote sensing technology, navigation technology and electronic technology, the production cost of small drones is gradually reduced, and there are more and more types of them, and their application range is more and more extensive. Small drones have brought convenience to the development of industrial and agricultural production and other fields, but they have also brought hidden dangers to public safety. Relevant departments have set up no-fly zones for small unmanned aerial vehicles and gradually introduced relevant management measures. However, there are always incidents such as aircraft loss of control or unidentified aircraft intrusion, and small unmanned aerial vehicles need to be captured or intercepted. [0003] The flight spee...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C27/26B64C37/02
CPCB64C27/08B64C27/26B64C37/02B64U10/25B64U10/10B64U2101/00
Inventor 王红雨鹿存跃赵珣刘伶章宝民王迎春尹午荣
Owner SHANGHAI JIAO TONG UNIV
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