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Lift-adjustable vector propulsion type multi-rotor unmanned plane

A multi-rotor unmanned aerial vehicle and propulsion technology, applied in the field of adjustable lift vector propulsion multi-rotor oil-powered unmanned aerial vehicle, can solve the problems of poor output stability, large engine vibration, flameout, etc., and simplify the process of adjusting flight parameters. , Strengthen the stability and handling, not easy to turn off the effect

Pending Publication Date: 2017-08-25
浙江点辰航空科技有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The invention provides an adjustable lift vector that can be applied to fuel power, the lift force can be adjusted, and the attitude of the drone can be adjusted without tilting the fuselage in the level flight state, and the stability and controllability are good. Propulsive multi-rotor UAV; it solves the poor power output stability of the fuel-powered UAV in the prior art, complicated operation, large engine vibration, easy to cause damage to the sensor, frequent speed adjustment will reduce the life of the engine or even appear Technical problems with flameout

Method used

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  • Lift-adjustable vector propulsion type multi-rotor unmanned plane

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Embodiment

[0026] Such as figure 1 As shown, an adjustable lift vector propulsion type multi-rotor UAV includes a fuselage 10, and a landing gear 11 is fixed below the fuselage 10, and the landing gear protects the safety of the entire fuselage when the UAV lands. . Four fuselage arms 9 are connected to the fuselage, and the fuselage arms 9 are evenly connected to the fuselage 10 . The machine arm 9 is used to support the fuel engine 2 and the propeller 1 on it. On the machine arm, a variable lift adjustment structure 3 is fixed simultaneously. The variable lift regulating structure 3 is a frame structure, the propeller 1 is located at the center of the variable lift regulating structure, and the height of the propeller 1 is higher than the uppermost frame of the variable lift regulating structure 3 . A fuel engine 2 is connected below the propeller 1, and the fuel engine 2 drives the propeller 1 to run at a constant speed, and the lift provided by the variable lift adjustment structu...

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Abstract

The invention relates to a civilian unmanned plane technology. A lift-adjustable vector propulsion type multi-rotor unmanned plane comprises a plane body. A plurality of plane arms are connected to the plane body. A propeller is connected to each plane arm. A variable-lift adjustment structure is arranged on each plane arm. Each variable-lift adjustment structure is composed of a rotatable vane. In the state of level flight, an inclined angle is formed after the vanes rotate. The included angle between the inclination direction and the flight direction is acute angle. The lift-adjustable vector propulsion type multi-rotor unmanned plane is suitable for being powered by gasoline, lift can be adjusted, unmanned plane posture adjustment can be conducted without inclining the plane body in the state of level flight, and stability and operability are good; and the technical problems that in the prior art, an unmanned plane powered by gasoline is poor in power output stability, complicated in operation and high in the engine vibration, and a sensor is prone to being damaged, the service life of an engine is shortened due to frequent speed regulating, and flameout even can even occur are solved.

Description

technical field [0001] The present invention relates to a civil unmanned aerial vehicle technology, in particular to an adjustable lift vector propulsion type multi-rotor oil-powered unmanned aerial vehicle. Background technique [0002] The multi-rotor UAV has simple take-off and landing requirements, low hovering speed, low requirements for the use environment, and is very flexible. As multi-rotor drones enter the civilian field, they are widely used in aerial photography, plant protection, surveying and mapping, emergency rescue and other fields. At this stage, lithium battery-powered multi-rotor drones mainly rely on the electronic speed controller (ESC) as a signal receiver to control the propeller speed, and change the propeller speed requirements according to different signal requirements. At this stage, multi-rotor UAVs mostly use lithium batteries as power. However, the endurance time of multi-rotor UAVs in this situation is a difficult problem to overcome. The tec...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08
CPCB64C27/08B64U10/10B64U30/20
Inventor 何小民黄亚坤葛正好章宇轩
Owner 浙江点辰航空科技有限公司
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