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A tiny foldable wheeled aircraft

An aircraft and folding wheel technology, applied in the field of aviation systems, can solve problems such as the inability to deploy unmanned aerial systems, and achieve the effects of improving battery life, reducing power components, reducing overall weight and structural complexity

Active Publication Date: 2022-01-14
BEIJING INST OF SPECIALIZED MACHINERY
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although these UAVs are simpler than manned combat aircraft in terms of size, weight, and combat system complexity, combat troops and individual soldiers operating at the squad level cannot deploy these UAV systems

Method used

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  • A tiny foldable wheeled aircraft
  • A tiny foldable wheeled aircraft
  • A tiny foldable wheeled aircraft

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Embodiment Construction

[0027] The present invention will be further described below in conjunction with the accompanying drawings.

[0028] A micro-sized foldable wheel-shaped aircraft, that is, a wheel-shaped aircraft with a diameter of no more than 10cm in a folded state. The folded state of the aircraft is cylindrical, which is convenient for rolling on the ground and carried by users. The flight state is in a vector two-rotor mode. It is used for Fly missions. It is characterized in that it includes three major components: a cylindrical fuselage, a vector power group, and a folding locking mechanism. It is divided into two modes: folding and flying, and can realize rolling on the ground and flying in the air.

[0029] The cylindrical fuselage is the main structural component of the wheel-shaped aircraft, which is used to install loads such as flight control modules, power supplies, and miniature image transmission equipment, and has the function of withstanding the impact force on the ground dur...

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Abstract

The invention discloses a miniature foldable wheel-shaped aircraft, which belongs to the technical field of aviation systems. The involved wheel-shaped aircraft is mainly composed of a fuselage, a rotor support frame, a vector power group, a folding locking mechanism and other components. The wheel-shaped aircraft mainly includes two state modes, which are folding mode and flight mode, which can realize the functions of rolling forward on the ground and flying in the air. Among them, in the folding mode, the aircraft is folded into a wheel shape for rolling forward or carried by the user. At the same time, in this mode, multiple aircraft combinations can be realized to facilitate the execution of cooperative combat missions; in flight mode, the aircraft is deployed into a vector two-rotor mode under the drive of the folding locking mechanism for performing flight missions. The aircraft involved in the invention has the advantages of novel structure, portable and foldable, diversified functions, and convenient use by individual soldiers.

Description

Technical field: [0001] The invention belongs to the technical field of aviation systems, in particular to a miniature foldable wheel-shaped aircraft. Background technique: [0002] In the Gulf War in the 1990s, the Kosovo War, and the Afghan War in the early 21st century, a large number of various types of unmanned aerial systems were used to complete battlefield reconnaissance, surveillance, temptation, harassment, target search and positioning, firepower and battle assessment. , anti-radiation, attack and other combat missions, and achieved remarkable results. Unmanned aerial vehicle (UAV) has been paid more and more attention by countries all over the world, and has set off a research boom. These UAVs are mainly positioned in platoon-level combat units, mainly composed of unmanned aerial vehicles, ground control stations, and launchers, and complete combat tasks under the control of the ground control station. Although these UAVs are simpler than manned combat aircraft...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C39/02B64C1/30B60F5/02
CPCB64C39/028B64C1/30B60F5/02B64U10/13B64U50/19B64U30/20
Inventor 贾华宇李兆博巫伟男尹晓旭杨志
Owner BEIJING INST OF SPECIALIZED MACHINERY
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