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Solar aircraft

A technology for aircraft and solar energy, applied in instruments, current collectors, aircraft parts, etc., can solve the problems of low operating energy efficiency, low speed of aircraft, complex structure, etc., and achieve the effect of reasonable structural design, fast response, and enhanced adjustment function.

Inactive Publication Date: 2019-11-19
西安长峰机电研究所
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

High-altitude balloons, airships, and conventional UAV systems have their own characteristics and advantages, but due to their complex structures and large systems, these aircraft speeds are very low, the energy efficiency of conventional operations is very low, and there are disadvantages such as the aircraft cannot be controlled for a long time

Method used

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  • Solar aircraft

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Embodiment Construction

[0020] The present invention will be further described below in conjunction with the accompanying drawings and embodiments, and the present invention includes but not limited to the following embodiments.

[0021] The invention provides an aircraft that can suspend in the air for a long time and provide power for itself. The main structure of the aircraft includes: an upper semi-elliptical upper plate, a lower semi-elliptical lower plate, two-blade rotors, an annular airbag, and a solar panel , semi-circular camera, sensor, solar system, engine, navigation system, monitoring system, control system and fixed landing gear. The main body of the upper plate and the lower plate are connected, and the battery required for power supply is installed in the cabin, and a rotating motor is fixed vertically in the center, and the motor drives the two-bladed rotor to rotate, providing initial power energy, so that the aircraft can reach the set height. The annular airbag is opened, and the...

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Abstract

The invention provides a solar aircraft which comprises a cabin body, rotor wings, an annular air bag and a solar panel. The rotor wings are mounted at the upper end of the cabin body and are poweredand driven by a battery mounted in the cabin body; the solar panel covers the upper surface of the cabin body to convert solar energy into electric energy to charge the battery; and the air bag surrounds the periphery of the cabin body, the air bag is folded in the cabin body when the aircraft lifts off, and the air bag is opened when the aircraft lifts off to be in position and is filled with gas, and the specific gravity of the gas is smaller than that of air. By means of a technology of combining suspension with solar energy, the solar aircraft is reasonable in structural design, has overlong suspending time and is high in energy utilization ratio.

Description

technical field [0001] The invention relates to a multipurpose aircraft, which is suitable for terrain detection, fire prevention and fire extinguishing and other occasions. Background technique [0002] Aircraft technology that utilizes solar energy and has vertical take-off and landing functions has broad application prospects, such as fixed-point observation in the air, reconnaissance, communication transfer, battlefield monitoring, monitoring and disposal of the environment and disaster conditions, etc. At present, the aircraft with vertical take-off and landing function are mainly helicopters, airships, etc. Solar-powered aircraft are mainly unmanned aerial vehicles with conventional layout, and there are not many aircraft that use the combination of rotor vertical take-off and landing and suspension. High-altitude balloons, airships, and conventional UAV systems have their own characteristics and advantages. However, due to their complex structures and large systems, t...

Claims

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Application Information

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IPC IPC(8): B64D27/24B64D47/08H02J7/35G05D1/10
CPCB64D27/24B64D47/08G05D1/101Y02T50/50Y02T50/60
Inventor 贾江宏王宏涛王海峰
Owner 西安长峰机电研究所
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