Solar aviation obstruction beacon

A technology of aviation obstruction lights and solar energy, applied in the field of aviation obstruction lights, can solve problems such as failure to work normally

Pending Publication Date: 2018-06-01
YINGLI ENERGY CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In view of this, the embodiment of the present invention provides a solar aviation obstruction light to solve the problem in the prior art that the solar energy aviation obstruction light cannot work normally in the case of snow

Method used

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  • Solar aviation obstruction beacon
  • Solar aviation obstruction beacon
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Embodiment Construction

[0024] In the following description, specific details such as specific system structures and technologies are presented for the purpose of illustration rather than limitation, so as to thoroughly understand the embodiments of the present invention. It will be apparent, however, to one skilled in the art that the invention may be practiced in other embodiments without these specific details. In other instances, detailed descriptions of well-known systems, devices, circuits, and methods are omitted so as not to obscure the description of the present invention with unnecessary detail.

[0025] In order to illustrate the technical solutions of the present invention, specific examples are used below to illustrate.

[0026] see figure 1 , providing a schematic diagram of a three-dimensional structure of a solar aviation obstruction light, detailed as follows:

[0027] The solar aviation obstruction light comprises a lamp body base 101, a lamp body 102, a solar panel 103 and a cont...

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Abstract

The invention provides a solar aviation obstruction beacon which is applicable to the technical field of an aviation obstruction beacon. The solar aviation obstruction beacon comprises a lamp body pedestal, a lamp body, a solar panel and a control device; the lamp body is arranged on the lamp body pedestal; the lamp body pedestal is arranged on the control device; the solar panel is arranged at one side of the control device; the solar aviation obstruction beacon also comprises a photosensitive transducer, a temperature sensing transducer and a heating wire; the photosensitive transducer and the temperature sensing transducer are arranged on the lamp body pedestal; the heating wire is arranged inside the lamp body and on the solar panel; the input end of the control device is connected with the photosensitive transducer and the temperature sensing transducer; and the output end of the control device is connected with the heating wire. According to the solar aviation obstruction beaconprovided by the invention, by detecting the temperature and light information outside the lamp body, the heating wire can be controlled to automatically heat the solar panel and a lampshade so as to achieve a snow removing effect and solve the problem that the solar aviation obstruction beacon fails to work normally under a snow accumulation condition.

Description

technical field [0001] The invention belongs to the technical field of aviation obstruction lights, in particular to a solar energy aviation obstruction light. Background technique [0002] According to national standards, high-rise buildings whose tops are 45 meters above the ground need to be equipped with aviation obstruction lights to show the outline of the building and thus serve as a warning to aircraft operators. With the continuous development of technology, solar aviation obstruction lights have appeared, which provides a new technical solution for the power supply mode of aviation obstruction lights. Aviation obstruction lights use solar panels to convert solar energy into electricity to power the body of the obstruction lights. [0003] However, the solar panels of traditional solar aviation obstruction lights and the lampshades of obstruction lights are usually directly exposed to the air, and the solar panels will not work normally when there is snow in winter...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F21S9/03F21V23/04F21V29/90F21V31/00F21W111/04
CPCF21S9/032F21V23/0442F21V23/0464F21V29/90F21V31/005F21W2111/04
Inventor 张建旗张文龙陈志军尚琪
Owner YINGLI ENERGY CHINA
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