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Solar-wind hybrid power airplane

A hybrid and solar style technology, which is used in the type of power plant, climate sustainability, aviation transportation and other directions, which can solve the problems of unable to collect sunlight, cannot fly overnight, etc., and achieve the effect of driving comfort and stability.

Inactive Publication Date: 2009-12-23
于江
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Existing solar aircraft use sunlight to irradiate the solar cell receiving plate to charge the solar lithium battery, so once it encounters night or cloudy days, it cannot collect sunlight and cannot fly long distances all night.

Method used

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  • Solar-wind hybrid power airplane

Examples

Experimental program
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Effect test

Embodiment Construction

[0012] Such as figure 1 Shown: The solar-wind hybrid aircraft consists of 1 fuselage 2 wings 3 empennages 4 solar panels 5 solar panels 6 electric propellers 9 rechargeable batteries. Four hidden wind generators 7 are respectively installed on each wing, Wind deflectors 8 are installed up and down the wind generator,

[0013] Working principle: four electric propellers 6 work at the same time when the plane takes off, the solar panel 4 on the wing and the solar panel 5 on the empennage are always in working condition, at this time the windshields 8 on all generators are closed, and the generators 7 It is static state, when reaching flying height, at this moment will according to the wind power and the lift force of aircraft, come symmetrically open the number of windshields 8 on the left and right wings, simultaneously the generators 7 on the left and right wings also follow the windshield 8 Open and start to work. When the wind force and lift force are large, the wind deflec...

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PUM

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Abstract

The invention discloses a solar-wind hybrid power airplane comprising an airframe 1, wings 2, a tail wing 3, solar panels 4 and 5, an electric propeller 6 and rechargeable batteries 9. The solar-wind mixed power airplane is characterized in that the wings 2 with the solar panels 4 are respectively provided with four hidden wind-driven generators 7; wind shields 8 which can be opened at the same time are respectively mounted at the upper part and the lower part of the wind-driven generators 7. The wind-driven generators 7 are influenced by wind power to work when the wind shields 8 are opened; and the wind-driven generators 7 stop working when the wind shields 8 are closed; and the upper wing surface and the lower wing surface of either wing 2 are on the same horizontal plane when the wind shields 8 are closed. The airplane solves the problem that the prior solar airplane can only use solar energy as an energy source and has insufficient energy source storage at night or in cloudy days, thereby utilizing a method of combining wind power and solar energy to provide the airplane with the energy sources so that the airplane can remotely fly run day and night.

Description

technical field [0001] The invention relates to a solar wind hybrid aircraft Background technique [0002] Existing solar aircraft use sunlight to irradiate the solar cell receiving plate to charge the solar lithium battery, so once it encounters night or cloudy days, it cannot collect sunlight and cannot fly long distances all night. Contents of the invention [0003] In order to realize day and night long-distance flight, the present invention uses wind energy, a free resource, to install a hidden wind generator on the wing of the aircraft, and fully utilizes the method of wind energy combined with solar energy to provide energy for the aircraft, which can realize continuous flight day and night, which is both environmentally friendly and environmentally friendly. save energy. [0004] In order to achieve the above object, the present invention adopts the following technical solutions: because the aircraft is affected by wind resistance and upward lift when flying in th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D27/02
CPCY02T50/69Y02T50/50
Inventor 于江
Owner 于江
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