Fixed wing type unmanned aerial vehicle with vertical takeoff and landing functions

A technology of vertical take-off and landing and unmanned aerial vehicle, which is applied in the direction of vertical take-off and landing aircraft, rotorcraft, unmanned aerial vehicles, etc., can solve the problems of increased flight weight of parachutes, inconvenient to carry, dangerous for operators, etc.

Pending Publication Date: 2017-09-12
SHENZHEN MICROMULTICOPTER AERO TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Catapult take-off requires a catapult frame, which is not easy to carry; hand-throwing take-off is a certain danger to the operator, and at the same time, the drone cannot be thrown by hand when its own weight is too large; runway taxi take-off and landing in the wi

Method used

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  • Fixed wing type unmanned aerial vehicle with vertical takeoff and landing functions
  • Fixed wing type unmanned aerial vehicle with vertical takeoff and landing functions

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Embodiment Construction

[0014] All features disclosed in this specification, or steps in all methods or processes disclosed, may be combined in any manner, except for mutually exclusive features and / or steps.

[0015] Any feature disclosed in this specification (including any appended claims, abstract and drawings), unless expressly stated otherwise, may be replaced by alternative features which are equivalent or serve a similar purpose. That is, unless expressly stated otherwise, each feature is one example only of a series of equivalent or similar features.

[0016] Such as figure 1 and figure 2 Shown, comprise drone fuselage 6, fuselage 6 both sides are provided with fixed wing 5, and fixed wing 5 is provided with first drive motor and the first helical wing 4 that is installed on the first drive motor, fuselage 6 A first battery and a first driver control assembly are arranged inside for the first driver to operate;

[0017] Both ends of the fuselage 6 are provided with an assembly groove, a ...

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Abstract

The invention discloses a fixed wing type unmanned aerial vehicle with vertical takeoff and landing functions. The fixed wing type unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein fixed wings are arranged at both sides of the unmanned aerial vehicle body; a first driving motor and a first rotary wing are arranged on each fixed wing, each first rotary wing is arranged on the corresponding first driving motor, a first battery and a first driver control assembly are arranged in the unmanned aerial vehicle body, and the first battery is used for driving a first driver to act. The fixed wing type unmanned aerial vehicle has the advantages that in the takeoff phase, the fixed wing type unmanned aerial vehicle is vertical to the horizontal surface through a first bending mechanism and a second bending mechanism, and then vertically takes off and lands; after takeoff, the first bending mechanism and the second bending mechanism are reset, the whole unmanned aerial vehicle is in a straight line shape, and the advancing function is realized through the rotary wings on the two bending mechanisms; under the mutual action of the rotary wings on the fixed wings, the whole power and steering of the unmanned aerial vehicle can be controlled.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a fixed-wing unmanned aerial vehicle capable of vertical take-off and landing. Background technique [0002] UAV is an unmanned aircraft operated by radio remote control equipment and self-contained program control device. There is no cockpit on board, 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 mother plane use radar and other equipment to track, locate, remote control, telemetry and digital transmission. It can take off like an ordinary aircraft under radio remote control or launch into the air with a booster rocket, and can also be taken into the air by the parent aircraft for flight. When recovering, it can automatically land in the same way as the common aircraft landing process, and can also be recovered by remote control with a parachute or a block. ...

Claims

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Application Information

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IPC IPC(8): B64C39/02B64C29/00B64C27/26
CPCB64C27/26B64C29/00B64C39/024B64U50/19B64U2101/00B64U2201/20
Inventor 卢致辉袁琦田伟程黄少龙韦建园
Owner SHENZHEN MICROMULTICOPTER AERO TECH CO LTD
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