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Solar aircraft

A technology of solar energy and flying objects, applied in the field of flying objects in the air, can solve the problems of no flying objects, etc., and achieve the effects of convenient operation, obvious use effect and ingenious design

Inactive Publication Date: 2017-09-01
王立新
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

There are no reports of such flying objects

Method used

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Embodiment Construction

[0011] Figure 1-3 The front middle part of the machine compartment 3 shown in the figure is provided with a driver's cabin 15, the rear side of the driver's cabin is provided with a manned and cargo compartment, the upper end of the driver's compartment is provided with a power compartment 5, and a combined power box 23 is arranged in the power compartment. The upper end of the combined power box is connected with a central shaft 8, and the central shaft is installed on the upper end of the combined power box by a bushing. The upper end of the central shaft is provided with a turntable 26, and 8 fin connecting plates 25 are arranged on the circumference of the turntable. The outer end of the board is connected with 8 fin plates with a width of 2 meters and a length of 10 meters. The fin plates are evenly installed and fixed on the turntable by the fin connection plate. plate, the positive solar receiving plate 6, and the negative solar receiving plate 7 are alternately instal...

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Abstract

The invention discloses a solar aircraft. According to the solar aircraft, a cab is arranged in the front middle portion of a cabin; a power bin is arranged at the upper end of the cab; a combined power box is arranged in the power bin; an intermediate shaft is connected at the upper end of the combined power box; a rotating table is arranged at the upper end of the intermediate shaft; eight flying fin connecting plates are arranged on the circumference of the rotating table; eight flying fin plates are connected at the outer ends of the flying fin connecting plates; two sets of positive pole and negative pole solar receiving panels are arranged at the upper ends of the flying fin plates; the positive pole solar receiving panels and the negative pole solar receiving panels are mounted and fixed on the flying fin plates in mutually spaced and alternate modes; a positive pole circulation ring is arranged on one of the positive pole solar flying fin connecting plates; a negative pole circulation ring is arranged on one of the negative pole solar flying fin connecting plates; and positive pole and negative pole carbon brushes are arranged at the upper end of the power bin. At the time of working, the solar receiving panels at the upper ends of blades convey solar energy to an accumulator through the positive pole and negative pole circulation rings, the carbon brushes and connecting wires, a direct current is turned into an alternate current through an inverter to drive the combined power box, and the flying fin plates are driven to rotate to fly.

Description

technical field [0001] The present invention relates to an aerial vehicle, specifically a solar transport aircraft. Background technique [0002] Solar flying object is a kind of transport aircraft powered by absorbing solar energy. It uses the sunlight resources in nature to carry objects into the air to transport materials, or manned for sightseeing, investigation, and travel. There are no reports of such flying objects. Contents of the invention [0003] The object of the present invention is to provide a solar-powered flying object to make full use of natural resources, convert solar energy into electric energy, drive the flying object to fly in the air, and provide convenience for human sightseeing, travel, investigation or transportation of materials. [0004] The scheme of the present invention is composed of a machine cabin, a driving cabin, a manned and loaded cargo cabin, a power cabin, a combined power box and a solar receiving panel. There are manned and carg...

Claims

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Application Information

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IPC IPC(8): B64C27/04B64D27/24H02J7/35
CPCH02J7/35B64C27/04B64D27/24B64D27/353
Inventor 王立新
Owner 王立新
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