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Unmanned aerial vehicle

A technology for unmanned aerial vehicles and power components, which is applied in the field of aircraft, can solve the problems of high speed, lower speed and range than fixed-wing aircraft, and high requirements for airport runways, and achieves the effect of reducing wind resistance and energy loss.

Inactive Publication Date: 2019-02-12
SZ DJI TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Rotary-wing aircraft can take off and land vertically at low speed, and do not have high requirements on the airport runway, but their speed and range are not as good as those of fixed-wing aircraft; Aircraft cannot have the best of both worlds

Method used

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  • Unmanned aerial vehicle
  • Unmanned aerial vehicle
  • Unmanned aerial vehicle

Examples

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Embodiment Construction

[0026] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals denote 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 only for explaining the present invention and should not be construed as limiting the present invention.

[0027] In describing the present invention, it should be understood that the terms "center", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", " Orientation indicated by rear, left, right, vertical, horizontal, top, bottom, inside, outside, clockwise, counterclockwise, etc. The positional relationship is based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present invention and simplifying the description, rather than indicating ...

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PUM

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Abstract

An unmanned aerial vehicle (100) includes a fuselage (10), a plurality of rotor power assemblies (20) disposed on the fuselage (10), and fixed wing power assembly (30) detachably mounted on the fuselage (10). When the fixed wing power assembly (30) is mounted on the fuselage (10), the fixed wing power assembly (30) is rotatable relative to the fuselage (10).

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an unmanned aircraft. Background technique [0002] Common ordinary aircraft are divided into two categories: rotary-wing aircraft and fixed-wing aircraft. Rotary-wing aircraft can take off and land at low speeds and have low requirements on airport runways, but their speed and range are not as good as those of fixed-wing aircraft; Aircraft cannot have the advantages of both. Contents of the invention [0003] An embodiment of the present invention provides an unmanned aerial vehicle. [0004] The unmanned aerial vehicle of the embodiment of the present invention comprises: [0005] body; [0006] a plurality of rotor power assemblies disposed on said fuselage; and [0007] A fixed-wing power assembly detachably installed on the fuselage, when the fixed-wing power assembly is installed on the fuselage, the fixed-wing power assembly can rotate relative to the fuselage. ...

Claims

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Application Information

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IPC IPC(8): B64C1/16B64C1/30B64C27/22B64C27/12
CPCB64C1/16B64C27/12B64C27/22B64U30/29B64U10/25B64U50/13B64U30/14B64U10/13B64C27/26B64C1/30B64U10/00B64U30/20B64U70/80
Inventor 周震昊刘翊涵熊荣明
Owner SZ DJI TECH CO LTD