Integrated solar cell and slot antenna device

A solar cell and slot antenna technology, applied in the field of satellite communication, can solve the problems of reducing the weight of satellites, increasing the light-receiving area of ​​solar cells, reducing the volume of satellites, etc., to achieve the effect of increasing the light-receiving area, reducing weight, and improving load capacity

Active Publication Date: 2019-10-25
XIDIAN UNIV
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Problems solved by technology

[0008] In order to achieve the above object, the present invention provides an integrated device for solar cells and slot antennas, which solves the problem of competition between solar cells and antenna systems for space resources on the limited surface area of ​​micro-nano satellites, and reduces the volume and weight of satellites. Increase the light-receiving area of ​​the solar cell

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  • Integrated solar cell and slot antenna device
  • Integrated solar cell and slot antenna device
  • Integrated solar cell and slot antenna device

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Embodiment Construction

[0027] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0028] In the process of researching the fusion technology of solar cells and antennas, the inventors found that microstrip slot antennas and solar cells have similar planar layered structure characteristics. figure 1 The structure diagram of the microstrip slot antenna shown includes: a slot antenna 1 , a metal floor 3 , a dielectric substrate 4 and a microstrip line 5 . The main structure of the microstrip slot antenna is a laminated structure of a metal flo...

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Abstract

The invention discloses a solar cell and slot antenna integration device, which comprises a slot antenna, a solar cell, a metal floor, a dielectric substrate and a microstrip line, and is characterized in that the metal floor is located on the dielectric substrate, the slot antenna is arranged on the metal floor, the microstrip line covers the lower part of the dielectric substrate and feeds energy for the slot antenna, the microstrip line and the slot antenna form electromagnetic coupling so as to generate electromagnetic radiation; the solar cell is located on the metal floor and does not cover the slot antenna, and the slot antenna runs through the solar cell and the metal floor; and the metal floor acts as a common horizontal plane of the slot antenna and the solar cell. The solar cell and slot antenna integration device solves a problem that the solar cell and the antenna system mutually compete for space resources at the limited surface of a micro-nano satellite, the volume of the satellite is reduced, the weight of the satellite is reduced, and the light receiving area of the solar cell is increased.

Description

technical field [0001] The invention belongs to the technical field of satellite communication, and relates to a solar cell and slot antenna integration device used on a three-dimensional micro-nano satellite. Background technique [0002] Micro-nano-satellites are currently a research hotspot in the field of aerospace science and space technology. Due to the characteristics of small size, low power consumption, short development cycle and formation networking, micro-nano-satellites can complete many complex space tasks at a relatively low cost. . However, due to volume and mass limitations, the load capacity of micro-nano satellites is limited, and their functions and on-orbit tasks are relatively single. At present, solar cells and antenna systems take up 1 / 4 to 1 / 3 of the weight of micro-nano satellites, and solar cells and antenna systems are designed independently, and the two compete with each other for the extremely limited space resources on the satellite. [0003]...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H01Q1/22H01Q1/48H01Q1/50H02S20/10
CPCH01Q1/22H01Q1/48H01Q1/50H02S20/10Y02E10/50
Inventor 白博文李小平张彦超刘彦明孙超石磊
Owner XIDIAN UNIV
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