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Single-duct coaxial reversal type double-rotor aircraft based on controllable deflector

A deflector and aircraft technology, applied in the field of unmanned aerial vehicles, can solve the problems of few intelligent capabilities of autonomous cruise, autonomous wind resistance mode transformation, limited number of external devices and installation positions, and low degree of intelligence. The effect of eliminating flight safety threats, increasing inertia, and improving work efficiency

Pending Publication Date: 2019-10-22
南京拓步智能科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although this simplifies the balance control, it limits the number of external equipment and the installation location, and also increases the danger when the drone lands.
From the perspective of intelligence, most of the current aircraft and drones are controlled by human remote control, the degree of intelligence is very low, and few have intelligent capabilities such as autonomous cruise and autonomous wind resistance mode change.

Method used

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  • Single-duct coaxial reversal type double-rotor aircraft based on controllable deflector
  • Single-duct coaxial reversal type double-rotor aircraft based on controllable deflector
  • Single-duct coaxial reversal type double-rotor aircraft based on controllable deflector

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0013] The ring-shaped duct enclosure 1 is made of light materials, surrounded by the dual rotors, fixed on the bracket, and can withstand a certain degree of impact. The air at the lower end of the tip flows upward from the periphery, which improves the working environment of the dual-rotor and increases the efficiency of the dual-rotor. The edge of the air inlet at the upper end of the casing is arc-shaped, which can increase the lift.

[0014] A plurality of pluggable interfaces are preset on the annular duct enclosure 1 for installation of various sensors and electronic equipment. Sensors and electronic equipment signal lines are attached to the casing 1 and the bracket 2, and are laid to reach the control circuit 6 at the center of the aircraft bracket.

[0015] The bracket 2 is cross-shaped, made of carbon fiber tube as the skeleton, and made into a streamlined cut surface to reduce disturbance to the airflow of the dual rotors. Bracket 2 is the skeleton of the whole a...

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Abstract

The invention discloses a single-duct coaxial reversal type double-rotor aircraft based on a controllable deflector. The aircraft is composed of an annular duct enclosure, a support, a coaxial reversal propeller, a fairing, the deflector and an electric and control system. The annular duct enclosure is transparent and internally hollow, and is internally provided with a multi-directional slot formounting a sensor, a steering engine and other electronic equipment. The duct enclosure eliminates the flying safety threat caused by exposure of a traditional structure rotor, and improves the working efficiency of the rotor; a stretchable support is arranged under the duct enclosure, and the support is automatically laid down during landing, so that safe landing is realized; coaxial reversal type double rotors are matched with the fairing and a butterfly-shaped body, vertical lifting of an aircraft body can be realized, and the inertial autorotation of the aircraft body is not required to becounteracted by additional arranging a tail rotor; and the non-vertical movement of the aircraft in the air is realized through the cooperation of the deflectable deflector below the double rotors, the control system controls a motor according to data of the sensor, so that autonomous or artificial flight control on the aircraft is realized

Description

technical field [0001] The invention relates to aircraft design, especially a single-duct vertically liftable unmanned aerial vehicle. Background technique [0002] In recent years, with the development of aerodynamics and the progress of material science, small aircraft, especially unmanned aerial vehicles, have achieved unprecedented development. A traditional small electric helicopter consists of a single rotor and a tail rotor. In addition, coaxial anti-propeller electric helicopters and multi-rotor UAVs are also emerging in large numbers. [0003] However, in terms of mechanical structure, many aircraft, especially UAVs, have the problem of rotor exposure. Although many drones have a protective frame on the outside of the rotor, it is still impossible to completely avoid collisions in flight, and additional air resistance and air interference will be greatly increased during flight, which will easily lead to its own crash and endanger the surrounding area. Other item...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/10B64C27/12B64C27/20B64D29/00B64C19/00
CPCB64C27/10B64C27/12B64C27/20B64D29/00B64C19/00
Inventor 王泽峰王晓
Owner 南京拓步智能科技有限公司