Solar electric helicopter

A solar energy and helicopter technology, applied in the transmission device to drive multiple propellers, the type of power plant, climate sustainability, etc., can solve the problems of single energy source, uncompensable energy loss, unsuitable for aircraft use, etc., to alleviate energy saving The effect of reducing emission and improving air force

Inactive Publication Date: 2012-07-25
SOUTH CHINA NORMAL UNIVERSITY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, in the field of aviation, the energy used is single, and most of them use petroleum fuel extracts (aviation gasoline, aviation kerosene or aviation diesel oil, etc.) as the main fuel, and use internal combustion engines as the main propulsion device
However, due to the pollution of smoke, noise, oil and water in traditional internal combustion engines, it is not conducive to the requirements of energy saving and environmental protection
The development of solar technology has been quite mature so far, and the use of solar technology has become an inevitable trend. However, due to the limitation of meteorological conditions, solar technology cannot be used normally at night and in rainy weather. Therefore, it is necessary to use other sources of energy for effective supplementation.
Other forms of energy supply, such as wind energy, are not suitable for use on aircraft due to reasons such as energy loss cannot be compensated

Method used

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Embodiment

[0021] The structure diagram of the present invention is as figure 1 As shown, the helicopter using solar energy and battery in the present invention includes an organism 1, a frame 2, a solar panel 3, and a battery pack 4, wherein the frame 2 is fixed on the body 1, and the solar panel 3 for absorbing solar energy is placed on the battery pack 4, the battery pack 4 is installed on the body 1 and / or the frame 2, the propeller 10 is fixed on the frame 2, and the passenger compartment 7 is hinged on the body 1 through the rotating shaft 5 for controlling the movement of the propeller 10 and the passenger compartment 7. The controller 8 that rotates is placed in the passenger compartment 7, and the landing bracket 9 that keeps the fuselage stable when the helicopter is landing is connected with the frame 2. In this embodiment, the solar panel 3 and the battery pack 4 are installed on the machine body 1 .

[0022] The passenger compartment 7 is fixed on the connecting shaft 6 , t...

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PUM

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Abstract

The invention relates to a helicopter using solar energy and storage batteries, which comprises a body, a frame, a solar panel and a storage battery set. The frame is fixed on the body. The solar panel is disposed on the upper surface of the storage battery set which is mounted on the body and/or the frame. A propeller is fixed on the frame. A cab is hinged to the body through rotary shafts. A controller for controlling rotation of the propeller and the cab is disposed in the cab. A landing support for stabilizing the helicopter in landing is connected with the frame. The helicopter is powered by electric energy only, using the solar panel to generate power supplied to electric equipment in the helicopter in real time can meet the double requirements of environmental friendliness and energy conservation and greatly improved flying capacity, and the helicopter is low in manufacturing process requirements, simple and accurate in operation, convenient in management, low in maintenance, environment-friendly, energy-saving, high in flying capacity, long in airborne period, high in reliability, high in energy conservation rate, widely applicable to civil fields of practical flying training, aerial surveillance.

Description

technical field [0001] The invention relates to an electric helicopter, in particular to an electric helicopter with a solar panel and a battery pack, and belongs to the transformation technology of the electric helicopter using solar energy. Background technique [0002] At present, in the field of aviation, the energy used is single, and most of them use petroleum fuel extracts (aviation gasoline, aviation kerosene or aviation diesel oil, etc.) as the main fuel, and use internal combustion engines as the main propulsion device. However, due to the pollution of smoke, noise, oil and water in traditional internal combustion engines, it is not conducive to the requirements of energy saving and environmental protection. The development of solar technology has been quite mature so far, and the use of solar technology has become an inevitable trend. However, due to the limitation of meteorological conditions, solar technology cannot be used normally at night and in rainy weather...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D27/24B64D35/04
CPCY02T50/62Y02T50/60
Inventor 张郁靖
Owner SOUTH CHINA NORMAL UNIVERSITY
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