Wing connected unmanned plane

A technology of unmanned aerial vehicles and connected wings, which is applied in the direction of rotorcraft, unmanned aerial vehicles, motor vehicles, etc., can solve the problems of limited development, no runway, high energy consumption of vertical take-off and landing, etc., and solve the problem of short power flight time Effect

Inactive Publication Date: 2017-02-08
BEIJING FALCON UAV TECH CO LTD
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The vertical take-off and landing (VTOL) UAV, which has just emerged in the UAV market, technically solves the problem of fixed-wing UAVs completing take-off and landing without a runway and in some complex environments, but due to the high energy consumption of vertical take-off and landing large, which also limits its development

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  • Wing connected unmanned plane
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Embodiment Construction

[0022] The technical solutions of the present invention will be further described in detail below in conjunction with specific embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, and are not intended to limit the present invention.

[0023] In describing the present invention, it should be understood that the terms "center", "longitudinal", "transverse", "upper", "lower", "front", "rear", "left", "right", " The orientations or positional relationships indicated by "vertical", "horizontal", "top", "bottom", "inner" and "outer" are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and Simplified descriptions, rather than indicating or implying that the device or element referred to must have a particular way, be constructed and operate in a particular orientation, and thus should not be construed as limiting...

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Abstract

The invention provides a wing connected unmanned plane. The front part of a plane body is provided with a fixed wing power group and a front wing, wherein the middle part of the plane body is hollow; an airplane control system and a power supply are put inside the plane body; the airplane control system is connected with the power supply through an electric wire; the back part of the plane body is provided with a back wing and a vertical fin; solar battery packs are uniformly distributed on the front wing and the back wing, and are connected with the power supply; the front wing and the back wing are connected through a lateral vertical wing; a machine frame is fixed on the airplane body positioned between the front wing and the back wing; a rotor wing power group is arranged on the machine frame. The wing connected unmanned plane has the advantages that the two leading functions of the solar energy and vertical taking-off and landing are combined; a fixed wing airplane with the connected wing layout is selected to be used as a main body; a solar panel is laid on the connected wing; the structure improvement is performed on the basis of the connected wing airplane; the installation of four rotor wings is completed; finally, the wing connected unmanned plane uses the solar energy as the auxiliary power; the problem of short electric flight time of the vertical taking-off and landing electric unmanned plane can be well solved.

Description

technical field [0001] The invention belongs to the technical field of industrial-grade unmanned aerial vehicles, in particular to a winged unmanned aerial vehicle. Background technique [0002] In recent years, the UAV industry has shown a rapid development trend from consumer UAVs to industrial UAVs. Among them, electric UAVs with the advantages of environmental protection and low noise, low flight time has become a technical shortcoming that is difficult to break through . The vertical take-off and landing (VTOL) UAV, which has just emerged in the UAV market, technically solves the problem of fixed-wing UAVs completing take-off and landing without a runway and in some complex environments. Large size also limits its development. [0003] In this context, a set of vertical take-off and landing UAVs with long electric endurance is imminent. Contents of the invention [0004] In order to solve the above problems, the present invention provides a winged unmanned aerial v...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/22B64D27/24B64C3/20B64C5/06
CPCB64C3/20B64C5/06B64C27/22B64D27/24B64U10/00B64U50/19Y02T50/60
Inventor 刘德山李刚伍可炳黄茂徐新奎
Owner BEIJING FALCON UAV TECH CO LTD
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