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Solar energy system for unmanned plane to use

An energy system and solar energy technology, applied in the field of solar energy energy systems, can solve the problems of high cost and high price of unsuitable investigation, patrolling, maintenance and repair, etc., and achieve the effect of breaking through the bottleneck of system energy technology, prolonging the sailing time, and simple operation

Inactive Publication Date: 2014-06-04
武汉美格科技股份有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For now, traditional UAVs are driven by aviation oil, which has defects such as short voyage time, high price, high maintenance and repair costs, and cannot be applied to fields such as reconnaissance and patrol that require high voyage time.

Method used

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  • Solar energy system for unmanned plane to use
  • Solar energy system for unmanned plane to use

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Embodiment Construction

[0021] In order to enable those skilled in the art to better understand the technical solutions of the present invention, and to make the above-mentioned purpose, features and points of the present invention more obvious and understandable, the following schematic diagrams are combined with the principle figure 1 and structural representation figure 2 The present invention is described in further detail.

[0022] combine figure 1 and figure 2 To illustrate the working principle of the present invention, the flexible and high-efficiency solar module components 2, 3, 4 and 5 absorb solar energy and convert it into electric energy, connect the power management system 6 through the connecting wire and the transfer terminal, and process it through the power management system The electric energy is stored in the energy storage battery pack 7, and the power management system is connected with the UAV operation system and the additional equipment of the fuselage through the data l...

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Abstract

The invention provides a solar energy system for an unmanned plane to use. The solar energy system is composed of a solar cell module, a power source management system, an energy storage battery and a data adapter. The solar cell module is formed by packaging of a flexible high-efficiency thin film solar cell piece and is characterized in that the flexible requirement for surface materials of the plane body streamline design can be met, and output is efficient and stable. The power source management system is composed of a unilateral diode, a solar maximum power tracking system, a voltage stabilization chip and the like and can achieve automatic charging control over the battery under low light. The energy storage battery is a high capacity lithium battery pack. The independent energy system can be integrated on the solar unmanned plane, the endurance of the unmanned plane can be greatly increased, the size of the solar unmanned plane can be reduced, meanwhile, the long-time power guarantee can be provided for other auxiliary functions of the unmanned plane, and the solar unmanned plane can be applied to various application fields.

Description

technical field [0001] The invention-type patent relates to a solar energy system that can be used by drones, specifically designing the design, materials and processing technology research of an energy system. Background technique [0002] After the wars in Iraq and Afghanistan, drones have gradually been recognized by people. Especially after the rapid development of drones and their popularity in various civilian fields, people gradually began to pay attention to the energy consumption and endurance of drones. For now, traditional UAVs are driven by aviation oil, which has the disadvantages of short voyage time, high price, high maintenance and repair costs, and cannot be applied to fields such as investigation and patrol that require high voyage time. [0003] The patent of this invention will solve this problem. The new solar power system and model design will break through the 7g / w efficiency bottleneck of the drone motor, which can improve the aerodynamic performance...

Claims

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Application Information

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IPC IPC(8): H02S10/40H01L31/042H02J7/35B64D27/24
CPCY02E10/50Y02T50/60
Inventor 不公告发明人
Owner 武汉美格科技股份有限公司
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