Standard module for solar array, preparation method of standard module and solar array with standard module

A standard module, solar technology, applied in the field of solar arrays, can solve the problems of complicated design and differences, and achieve the effect of good residual magnetism, uniform tooling, and uniform technical status

Active Publication Date: 2022-04-19
北京博瑞原子空间能源科技有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004]The solar array battery circuit part is usually designed according to the power demand or substrate size, and the traditional CIC battery, bus bar, cable 140, and diode are arranged. The traditional CIC battery It can only be arranged in a rectangle so that the bus bars can be arranged at both ends of the traditional CIC battery for confluence. The design is more cumber

Method used

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  • Standard module for solar array, preparation method of standard module and solar array with standard module
  • Standard module for solar array, preparation method of standard module and solar array with standard module
  • Standard module for solar array, preparation method of standard module and solar array with standard module

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Embodiment Construction

[0076] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals designate the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.

[0077] In the description of the present invention, it should be understood that the orientation descriptions, such as up, down, front, back, left, right, etc. indicated orientations or positional relationships are based on the orientations or positional relationships shown in the drawings, and are only In order to facilitate the description of the present invention and simplify the description, it does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific ...

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Abstract

The invention discloses a standard module for a solar array, a preparation method of the standard module and the solar array with the standard module, and the standard module comprises a CIC battery pack which comprises a plurality of CIC batteries which are electrically connected in sequence, and the CIC battery pack is provided with a first total electrode and a second total electrode; the circuit board is used for being electrically connected with the CIC battery pack, the circuit board is arranged below the CIC battery pack, the size of the cross section of the circuit board corresponds to that of the cross section of the CIC battery pack, a plurality of first bonding pads and a plurality of second bonding pads are arranged on the circuit board, a lap joint area is arranged on the circuit board, and the lap joint area is used for lap joint between two standard modules; the first bus members are arranged in the circuit board and electrically connected with the first total electrode through the first bonding pads, and the first bus members pass through the lap joint area; and the plurality of second bus members are arranged in the circuit board, are electrically connected with the second total electrode through the second bonding pad, and pass through the lap joint area.

Description

technical field [0001] The invention relates to the technical field of the solar array circuit part in the spacecraft power supply subsystem, in particular to a standard module for the solar array, a preparation method thereof and a solar array with the same. Background technique [0002] The spacecraft solar array is composed of circuit parts and mechanical parts. The circuit part includes CIC batteries or CIC battery modules, diodes, cables, and electrical connectors. The mechanical parts include substrates, connecting frames, expansion locking mechanisms, compression release mechanisms, and buffer release mechanisms. , position feedback components, etc. [0003] refer to figure 1 , figure 2 , image 3 and Figure 4 , the basic unit of the existing solar array circuit part is usually a traditional CIC battery, and the traditional CIC battery includes a single solar cell 111, a single glass cover 112, an interconnect 113, and a bypass diode 114, wherein the single glas...

Claims

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Application Information

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IPC IPC(8): H01L31/05H01L31/18
CPCH01L31/0504H01L31/18Y02E10/50
Inventor 胡文涛杨文奕马涤非
Owner 北京博瑞原子空间能源科技有限公司
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