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Power bus apparatus for improving power mass ratio of power supply controller

A technology of power controller and power confluence, applied in the direction of output power conversion device, electrical components, etc., can solve the problems of wire harness height influence, printed board intertwined, debugging and disassembly difficulties, etc., to simplify the assembly process and reduce the connection Conductors, the effect of achieving reliability

Active Publication Date: 2018-08-28
SHANGHAI INST OF SPACE POWER SOURCES
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In this case, it is often necessary to use large-diameter multi-strand wires to switch between circuit boards, so it will inevitably cause printed boards to be involved with each other, the height of the wire harness will affect the module assembly, and the power-to-quality ratio of the power confluence structure is low. Due to the comprehensive influence of installation, derating, wire path, etc., the controller has problems such as long assembly time, many human operation problems, difficult debugging and disassembly, and poor consistency of multiple single machines.

Method used

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  • Power bus apparatus for improving power mass ratio of power supply controller
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  • Power bus apparatus for improving power mass ratio of power supply controller

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Embodiment Construction

[0015] In order to make the above objects, features and advantages of the present invention more comprehensible, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0016] Such as figure 1 As shown, a power confluence device for a power supply controller for a spacecraft provided by an embodiment of the present invention includes a first power conversion circuit board 11, a second power conversion circuit board 12, a fastening assembly 3, an input power positive interface 4, an output power Positive interface 5, power negative interface 6 and stub welding assembly 7.

[0017] Such as figure 2 As shown, another spacecraft power supply controller power confluence device provided by the embodiment of the present invention includes a first power conversion circuit board 11, a copper component 2, a fastening component 3, an input power positive interface 4, and an output power positive interface...

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Abstract

Disclosed is a power bus apparatus for improving power mass ratio of a power supply controller. The power bus apparatus is characterized in that the apparatus comprises at least one power conversion circuit board, at least one input power positive interface (4), at least one output power positive interface (5), at least one power negative interface (6), a fastening assembly (3) and a power transmission assembly, wherein the at least one power conversion circuit board is mounted on one power supply controller; the at least one input power positive interface (4), at least one output power positive interface (5), and at least one power negative interface (6) are mounted on the first power conversion circuit board (11) through the fastening assembly (3); and the power transmission assembly isfixed with the input power positive interface (4) and / or the output power positive interface (5) and / or the power negative interface (6), and mounted on the power conversion circuit board.

Description

technical field [0001] The invention relates to a power converging device for a power supply controller, in particular to a power converging device suitable for improving the power-to-mass ratio of a power supply controller for spacecraft. Background technique [0002] Improving the power density of power supply controllers is the development trend of space power supply technology today. Compared with previous spacecraft, current power supply controllers have higher requirements in terms of volume, weight, and mechanical properties. Therefore, in the design process of the spacecraft power controller, the power transmission situation should be fully considered, and various power transfer media should be used comprehensively to realize the more effective, convenient and safe input, transfer and output of the power controller power. [0003] At present, the power transmission of the spacecraft power controller is mainly realized through circuit board wiring and cooperating with...

Claims

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Application Information

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IPC IPC(8): H02M1/00
CPCH02M1/00
Inventor 瞿诗霞蔡晓东徐泽锋张俊亭郑磊宋楠丁一宁刘瑜安广帅
Owner SHANGHAI INST OF SPACE POWER SOURCES
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