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A foldable drone

A technology of drones and fuselages, which is applied to fuselages, unmanned aircraft, rotorcraft, etc., can solve the problems of inconvenient carrying of drones, lack of wing folding mechanism, and failure to meet the needs of use, so as to achieve improvement The effect of battery life, avoiding device damage, and reducing occupied space

Active Publication Date: 2022-05-13
NANJING ANYUAN TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The fuselage of existing drones cannot be folded when in use, so they cannot adapt to different flight situations. At the same time, they lack the necessary wing folding mechanism. When the space is limited, the ideal flight effect cannot be achieved by folding the wings, and the use requirements cannot be met.

Method used

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  • A foldable drone
  • A foldable drone
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Embodiment Construction

[0021] The technical solution of this patent will be further described in detail below in conjunction with specific embodiments.

[0022] Embodiments of the present patent are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals designate the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary and are only used for explaining the patent, and should not be construed as limiting the patent.

[0023] In the description of this patent, it is to be understood that the terms "center", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", The orientation or positional relationship indicated by "top", "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing this patent and simplifying the des...

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Abstract

The invention relates to the technical field of unmanned aerial vehicles, in particular to a foldable fuselage unmanned aerial vehicle. It includes a folding frame and a folding box arranged above the folding frame, a wing folding mechanism is installed inside the folding frame, and the wing folding mechanism includes a sliding plate slidably installed inside the folding frame, and the sliding Racks are installed symmetrically on both sides of the plate, and the two racks mesh with the first gear that is rotatably installed on the inner bottom surface of the folding frame. The present invention is provided with a folding box, so that the drone body can be operated when necessary. The volume adjustment is convenient to adapt to different flight conditions. By setting the wing folding mechanism, it is convenient to carry the drone during use, reducing the space occupied by the drone, and can be used when encountering a relatively narrow space. The ideal flight effect is achieved by briefly folding the wings, and at the same time, the four wings are folded at the same time, which improves the folding efficiency and greatly reduces the power consumption of the drone.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with a foldable fuselage. Background technique [0002] UAV is an unmanned aircraft. There is no cockpit on the UAV but it is equipped with autopilot, program control device and other equipment. The personnel on the ground, on the ship, or at the remote control station of the main aircraft use radar and other equipment to track, locate, remotely control and telemeter and digitally transmit it. The drone inspection method has the advantages of high efficiency, fast, reliable, low cost, and not affected by the region. [0003] The fuselage of existing drones cannot be folded when in use, so they cannot adapt to different flight situations. At the same time, they lack the necessary wing folding mechanism. When the space is limited, the ideal flight effect cannot be achieved by folding the wings, and the use requirements cannot be met. ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/08B64C1/30B64D47/00B64D47/08
CPCB64C27/08B64C1/30B64D47/00B64D47/08B64U2101/30B64U10/10
Inventor 王三明王聪明马颖金龙朱伟伟顾珊珊
Owner NANJING ANYUAN TECH CO LTD