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In-series coaxial twin-propeller tailstock-type vertical taking-off and landing unmanned aerial vehicle

A vertical take-off and landing, tailstock-type technology, applied in the field of UAV flight principle, can solve the problems of difficult control of flight principle and high energy consumption, and achieve the effect of improving endurance, low energy consumption and effective rudder efficiency

Inactive Publication Date: 2017-05-31
AVIC GUIZHOU AIRPLANE
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The present invention needs to solve the problems of high energy consumption and difficult flight principle control in the process of vertical take-off and landing

Method used

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  • In-series coaxial twin-propeller tailstock-type vertical taking-off and landing unmanned aerial vehicle
  • In-series coaxial twin-propeller tailstock-type vertical taking-off and landing unmanned aerial vehicle
  • In-series coaxial twin-propeller tailstock-type vertical taking-off and landing unmanned aerial vehicle

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Embodiment Construction

[0010] The specific embodiment of the present invention is described below in conjunction with accompanying drawing:

[0011] Tandem coaxial double propeller tailstock type vertical take-off and landing UAV, including front pulling power system 1, fuselage body 2, tube propeller rear propulsion system 3, cross tailstock 4 and outrigger shock absorption system 5, front pulling The power system 1 is installed on the head of the fuselage main body 2, the propulsion system 3 is installed on the tail of the fuselage main body 2 and merged with the wings of the fuselage main body 2, and the cross tailstock 4 is installed behind the sleeve propeller The rear end of the propulsion system 3, the foot damping system 5 is installed on the four wings of the cross tailstock 4.

[0012] In order to ensure the coaxial and same rotation speed with the front pulling power system 1, the tube-in-propeller rear propulsion system 3 of the tandem coaxial double-blade tailstock vertical take-off and...

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Abstract

The invention relates to flight principle technology of unmanned aerial vehicles. An in-series coaxial twin-propeller tailstock-type vertical taking-off and landing unmanned aerial vehicle includes: a front-pulling power system, a main body, a tube sleeve propeller back-pushing power system, a tail tube, a cross-shaped tailstock, and a support leg damping system. The main body internally includes a battery cabin, a mission payload cabin, and a flight control system cabin; when the aerial vehicle is taken-off, the vehicle is support by the support leg damping system. The front-pulling propeller and the back-pushing tube sleeve propeller rotate to generate taken-off power, and meanwhile, the reversal torsional moments due to the propellers are reduced. Flight control manipulates ailerons and a control surface of the cross-shaped tailstock so that the ailerons and the cross-shaped tailstock generate steerage due to slip flow brought by fold propellers, thereby correcting and controlling the attitude of the aerial vehicle and ensuring flight of the aerial vehicle. During vertical landing, the support leg damping system works. The unmanned aerial vehicle has simple and reliable flight principle, and compared with inclined disc coaxial twin-propeller structure, the unmanned aerial vehicle is simpler in control principle.

Description

technical field [0001] The invention relates to the flight principle technology of an unmanned aerial vehicle, in particular to a tandem coaxial double propeller tailstock type vertical take-off and landing unmanned aerial vehicle. Background technique [0002] In recent years, the domestic drone industry has developed by leaps and bounds, and it is widely used in power line inspection, emergency rescue and disaster relief, forest monitoring, communication relay and other fields. The fixed-wing vertical take-off and landing UAV takes into account the vertical take-off and landing, fixed-point operation of the rotorcraft and the fast response and long endurance of the fixed-wing, and is suitable for performing mountain tasks. Its main development direction is divided into tailstock type and tilt rotor type. The fixed-wing vertical take-off and landing technology developed earlier, but the technology is complicated and the progress is slow, but so far only the V-22 "Osprey" a...

Claims

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Application Information

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IPC IPC(8): B64C29/02
Inventor 李支强韦毅施幕开陈惠惠袁云王雪峰刘健
Owner AVIC GUIZHOU AIRPLANE
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