A tube-type launching compound-wing unmanned aerial vehicle and a method for realizing lateral rolling operation

A technology of unmanned aerial vehicles and compound wings, which is applied in the direction of unmanned aircraft, rotorcraft, motor vehicles, etc., can solve the problem that the tube-type launched unmanned aerial vehicle cannot hover, achieve good maneuverability, improve stability, Effect of increasing pose transition rate

Active Publication Date: 2021-11-12
XIAN LINGKONG ELECTRONICS TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Aiming at the deficiencies in the prior art, the purpose of the present invention is to provide a tube-type launching compound-wing unmanned aerial vehicle and a method for realizing the rolling operation, so as to solve the technical problem that the tube-type launching unmanned aerial vehicle cannot hover in the prior art

Method used

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  • A tube-type launching compound-wing unmanned aerial vehicle and a method for realizing lateral rolling operation
  • A tube-type launching compound-wing unmanned aerial vehicle and a method for realizing lateral rolling operation
  • A tube-type launching compound-wing unmanned aerial vehicle and a method for realizing lateral rolling operation

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Embodiment

[0037] This embodiment provides a kind of tube-type launch composite wing unmanned aerial vehicle, such as Figure 1 to Figure 6 As shown, it includes a fuselage 1, two side wings 2 and two empennages 3. The bottom of the fuselage 1 is provided with a lower wing storage groove 4, and a rotatable lower wing 5 is installed in the lower wing storage groove 4. A rotatable first propeller 6 is installed on the wing 5; a rotatable second propeller 7 and a third propeller 8 are respectively installed on the two side wings 2;

[0038] A first storage surface 9 for storing the side wings 2 is provided on the fuselage 1 close to the two side wings 2, and a first preset angle is formed between the first storage surfaces 9; There are second storage surfaces 10, and the second storage surfaces 10 form a second preset angle.

[0039] In the above technical solution, by adding a lower wing at the bottom of the fuselage of the UAV, and installing propellers on the side wings, the tubular UAV...

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Abstract

The invention discloses a tube-type launching compound-wing unmanned aerial vehicle and a method for realizing lateral rolling operation, comprising a fuselage, two side wings and two tail fins, the bottom of the fuselage is provided with a lower wing storage slot, and the A rotatable lower wing is installed in the storage tank of the lower wing, and the lower wing is added to the UAV, and the propeller is installed on the side wing, which realizes the fixed-wing mode flying to the target point and then hovering, which improves the suspension. The stability of the cabin solves the technical problem that the tube-type launching UAV cannot hover in the prior art; in addition, the UAV makes the UAV realize Rolling action, so that when the UAV is flying in fixed-wing mode, not only the side wings can generate rolling torque to make the aircraft achieve rolling action, but also the different rotation speeds between the three propellers can also generate rolling torque to make the aircraft achieve Rolling action, increased rate of attitude change and reduced flank loads.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicle flight control, and relates to a tubular launching unmanned aerial vehicle, a folding unmanned aerial vehicle, a fixed-wing unmanned aerial vehicle, and a multi-rotor unmanned aerial vehicle, in particular to a tubular launching compound wing unmanned aerial vehicle and its realization Method for scrolling. Background technique [0002] At present, the development of UAVs on the market is very mature in terms of flight control and power drive; but on the other hand, based on the flight principles of conventional UAVs, it also shows inherent shortcomings in diversified flight tasks: multi-rotor UAVs The structure leads to low flight speed, short battery life, and slow remote response speed of the UAV. The fixed-wing structure leads to the high minimum flight speed of the UAV, which cannot be hovered for reconnaissance, and is easy to be found. The flight method is limited. The take...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/08B64C27/28B64C1/30
CPCB64C27/08B64C27/28B64C1/30B64U70/70B64U70/80B64U10/10
Inventor 贾育松沈洋
Owner XIAN LINGKONG ELECTRONICS TECH CO LTD
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