Underwater-air dual-purpose unmanned aerial vehicle

A drone and dual-use technology, applied in the field of drones, can solve problems such as limited operating space and inability to operate

Inactive Publication Date: 2017-11-07
吴佳锋
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, these operations are only carried out in the air and cannot be carried out underwater, thereby limiting its operation space, which is the deficiency of the existing technology

Method used

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  • Underwater-air dual-purpose unmanned aerial vehicle
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  • Underwater-air dual-purpose unmanned aerial vehicle

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Embodiment Construction

[0026] In order to clearly illustrate the technical characteristics of this solution, the following will describe this solution through specific implementation modes and in conjunction with the accompanying drawings.

[0027] A water-air dual-purpose unmanned aerial vehicle, as shown in the figure, it includes an unmanned aerial vehicle main body 6 and a remote control module, and the two sides of the unmanned aerial vehicle main body 6 are respectively provided with a wing assembly, and the wing assembly Including the wing 4, the bottom surface of the wing 4 is fixedly connected with a miniature vane pump 33, and the outer end of the wing 4 is fixedly connected with a side wing cover 1, and the side wing cover 1 is a rotary structure with openings at both ends, and the side wing cover 1 is provided with a wing propeller 3 driven by a wing motor 2. The bottom surface of the inner end of the wing 4 is hinged to the main body 6 of the drone. The hinge point is used as a fulcrum f...

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Abstract

The invention provides an underwater-air dual-purpose unmanned aerial vehicle. The underwater-air dual-purpose unmanned aerial vehicle comprises an unmanned aerial vehicle main body; wings are correspondingly arranged on the two sides of the unmanned aerial vehicle main body; miniature vane pumps are fixedly connected with the bottom faces of the wings, and the bottom faces of the inner side ends of the wings are hinged to the unmanned aerial vehicle main body; connecting rods I are fixedly connected with one ends of the side faces of the inner side ends of the wings, and bearings are fixedly connected with the other ends of the side faces of the inner side ends of the wings; guiding-limiting shafts are installed in the bearings, and tracks matched with the guiding-limiting shafts are installed on the unmanned aerial vehicle main body in a supported mode; a support assembly is fixedly connected with the unmanned aerial vehicle main body, an electromotor is installed on the support assembly, an eccentric wheel is driven to rotate by the electromotor, and a pushing rod is driven to move back and forth by the eccentric wheel through a connecting rod II, so that power is provided for folding or unfolding of the wings; tail wing plates arranged in a V-shaped mode are fixedly connected with the tail of the unmanned aerial vehicle main body, and rotating motors are symmetrically installed at the opposite ends of V-shaped inner cavities of the tail wing plates; and tail wing hoods can be driven to rotate by the two rotating motors around the centers of motor shafts so as to provide auxiliary power for flight of the unmanned aerial vehicle. The underwater-air dual-purpose unmanned aerial vehicle can be operated in the air and underwater.

Description

technical field [0001] The invention relates to an unmanned aerial vehicle, in particular to a water-air dual-purpose unmanned aerial vehicle. Background technique [0002] With the development of science and technology, unmanned aerial vehicles (UAVs for short) are more and more widely used. It can be used in aerial photography, agriculture, forestry and plant protection, express delivery, disaster relief, observation of wild animals, monitoring of infectious diseases, surveying and mapping, and news reports. , power inspection, film and television shooting and other fields. But these operations just carry out in the air, can't carry out operation underwater, thereby limited its operation space, Here it is the weak point that existing technology exists. Contents of the invention [0003] The technical problem to be solved by the present invention is to provide a water-air dual-purpose unmanned aerial vehicle for the deficiencies in the prior art. The unmanned aerial vehi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/30B64C27/08B60F5/02
CPCB64C1/30B64C27/08B60F5/02B64U10/10B64U2101/00
Inventor 吴佳锋
Owner 吴佳锋
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