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drone

A technology of unmanned aerial vehicles and airframes, applied in the field of unmanned aerial vehicles, can solve the problems of high requirements for airport distance conditions, unfavorable hiding of aircraft bases, and low combat efficiency

Active Publication Date: 2022-07-05
AIR FORCE UNIV PLA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, the current drones require a long landing and rolling distance, and have high requirements for the distance from the airport, which is not conducive to the hiding of the aircraft base, and leads to low combat efficiency.

Method used

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Embodiment Construction

[0040] The technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0041] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", " Back, Left, Right, Vertical, Horizontal, Top, Bottom, Inner, Outer, Clockwise, Counterclockwise, Axial , "radial", "circumferential" and other indicated orientations or positional relationships are based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenie...

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Abstract

The invention provides an unmanned aerial vehicle, which relates to the technical field of unmanned aerial vehicles. The UAV includes a double tail support body, a tail wheel, a balance wing, two tail wheel tail supports and two telescopic locking tail wheel vertical supports; one end of the tail wheel tail support is pivotally connected to the double tail support body, and the tail The wheel is arranged at the other end of the tail-wheel tail support; the balance wing is pivoted between the two tail-wheel tail supports, and a gyroscope balance piece is arranged on the balance wing to make the inclination of the balance wing match the dive of the drone. The angles are the same; the tail wheel standing support is fixedly arranged on the double tail support body, and the extension end of the tail wheel standing support is pivotally connected with the tail wheel tail support. The technical effect of reducing the landing roll distance of the drone is achieved.

Description

technical field [0001] The present invention relates to the technical field of unmanned aerial vehicles, and in particular, to unmanned aerial vehicles. Background technique [0002] With the leap in the world's technological level and the change in the form of warfare, the status and frequency of the use of UAVs have exploded. In the foreseeable future, people will gather manpower and funds for the design, manufacture, and flight control of UAVs, and use UAVs extensively and in large numbers in wars. There are three main types of UAVs: fixed-wing UAVs, unmanned helicopters and multi-rotor UAVs. Among the fixed-wing UAVs, the long-endurance and large-capacity models are the top of the national strength and technology. Such drones often focus on the latest scientific research results and top technologies. [0003] However, the current UAV needs a long landing and rolling distance, and has high requirements on the distance from the airport, which is not conducive to the hid...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C25/10B64C25/36
Inventor 严子荟方立波
Owner AIR FORCE UNIV PLA
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