A composite aeroplane with rotor and inflatable airbag with vector thrust

A technology of floating aircraft and inflatable airbags, which is applied in the direction of hybrid aircraft, unmanned aircraft, aircraft, etc., can solve the problems of limited payload capacity, large payload, slow flight speed, etc., and achieve rich and diverse movement modes , Accurate and fast movement adjustment, the effect of reducing energy consumption

Active Publication Date: 2020-11-24
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The aerostat has a history of nearly a century of development, and many types of large aerostats have been derived, which bring the aerostat back from the remote atmospheric flight area and use it near the ground, and the miniaturization has potential application value and has It has the advantages of long time in the air and low requirements for take-off and landing sites, but its flight speed is slow and its maneuverability is also poor
[0003] For the near-Earth space, there are mainly small fixed-wing detection and reconnaissance UAVs, multi-axis rotor UAVs, and small unmanned helicopters. At the same time, the most widely used security systems are mainly fixed-position pan-tilt camera monitoring systems. , these systems have certain application limitations. For example, due to the relatively fast flight speed of fixed-wing UAVs, there are certain requirements for flight heights, and the required flying space is large and the turning radius is large; multi-axis rotor UAVs Due to its structural problems, limited payload capacity and endurance have been criticized by people; compared with the former two, small unmanned helicopters have larger payloads, lower flight speeds, and better space maneuverability than fixed-wing helicopters. At the same time, many oil-powered and electric helicopters on the market have a longer battery life than multi-axis rotor drones. However, their structures are more complicated, their research and development costs are higher, and their operation is more difficult. certain danger

Method used

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  • A composite aeroplane with rotor and inflatable airbag with vector thrust
  • A composite aeroplane with rotor and inflatable airbag with vector thrust
  • A composite aeroplane with rotor and inflatable airbag with vector thrust

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Embodiment Construction

[0023] The present invention will be further described in detail with reference to the accompanying drawings and embodiments.

[0024] The present invention has vector thrust rotor and inflatable airbag composite floating aircraft, which is composed of helium floating body 1 and independent rotor power module 2, two main parts, such as figure 1 , figure 2 shown.

[0025] The floating body 1 is used to provide the main lift force. It is a spherical, ellipsoidal or other symmetrical film-type aerostat airbag. The material includes but is not limited to aluminum film, latex and other lightweight materials; the interior uses helium or other The inert gas that is lighter than air is used for filling, and since the gas density is lower than that of air, it can provide a certain lift; at the same time, helium is used as the inert gas, which can ensure the safety of the aeroplane, and the cost is relatively low.

[0026] The rotor power module 2 is used to provide aircraft attitude...

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Abstract

The invention discloses a composite aeroplane with a rotor and an inflatable air bag with vector thrust, which includes an aerostat and a rotor power module. The rotor in the rotor power module is made of a 8-shaped frame formed by laser and a flexible film to form a blade, which is installed on the largest diameter circular surface of the aerostat at equal intervals in the circumferential direction. It is divided into horizontal and vertical layouts, which can realize vector The propelled rotor module is regularly programmed to output power, which can complete the rapid movement of the aircraft in all directions, including climbing, descending, hovering, and spinning. The top of the aerostat is designed with a flexible thin-film solar cell module, and the bottom is designed with a charging and central control unit. The invention is mainly used in adjacent spaces, enclosed indoor spaces and semi-enclosed spaces. It not only has the advantages of long battery life, large ceiling, stable floating and low flight noise of the aerostat, but also has the advantages of high maneuverability of the multi-rotor UAV. Excellent performance and handling performance.

Description

technical field [0001] The invention belongs to unmanned aerial vehicle technology, new energy technology and Internet of Things technology, and specifically relates to a rotor and an inflatable air bag composite aerostat with vector thrust. Background technique [0002] An aerostat generally refers to an aircraft whose specific gravity is lighter than air and which relies on atmospheric buoyancy to lift into the air. In the fields of electronics and military and civilian use, hot air balloons are generally not included in the range of aerostats. Also, spaceships don't necessarily rely on buoyancy. In addition to military use, large civilian aerostats can also be used for transportation, transportation, entertainment, disaster relief, film and television shooting, scientific experiments and so on. At present, people's research mainly focuses on the research and development and design of large-scale, high-altitude floating vehicles, and there are few applications of using f...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64B1/32B64B1/34B64C27/08
CPCB64B1/32B64B1/34B64C27/08B64B2201/00B64U10/30B64U50/34B64U10/10B64U30/20
Inventor 王少萍张益鑫周之涵王康乐刘宝旭
Owner BEIHANG UNIV
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