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Spatial low-rail high-voltage power supply system supporting on-rail maintenance

A high-voltage power supply and space technology, applied in parallel operation of DC power supply, space vehicle power supply system, current collector, etc., can solve problems such as complex system composition and large power demand of the space station power supply system

Pending Publication Date: 2021-07-06
SHANGHAI INST OF SPACE POWER SOURCES
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Compared with the previous spacecraft power system, the space station power

Method used

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  • Spatial low-rail high-voltage power supply system supporting on-rail maintenance
  • Spatial low-rail high-voltage power supply system supporting on-rail maintenance
  • Spatial low-rail high-voltage power supply system supporting on-rail maintenance

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Embodiment Construction

[0028] In order to better understand the above technical solutions, the technical solutions of the present application will be described in detail below through the accompanying drawings and specific examples. It should be understood that the embodiments of the present application and the specific features in the examples are detailed descriptions of the technical solutions of the present application, and It is not a limitation to the technical solutions of the present application, and the embodiments of the present application and the technical features in the embodiments can be combined without conflict.

[0029] A space low-rail high-voltage power supply system supporting on-orbit maintenance provided by the embodiment of the present application will be further described in detail below in conjunction with the accompanying drawings. The specific implementation methods may include (such as figure 1 shown):

[0030] In the solution provided by the embodiment of the present ap...

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Abstract

The invention discloses a space low-rail high-voltage power supply system supporting on-rail maintenance, and belongs to the technical field of space power supplies. The system comprises two independent power channels, the two power channels have the same function composition, and energy is provided for a spacecraft load through energy grid connection; each power channel takes the solar cell wing as a starting point and the bus filter as an end point to form an independent 100V power supply bus; each power channel comprises a solar cell wing, a driving mechanism, a shunt regulator, a bus filter, a comprehensive driving controller, a charging and discharging regulator, a lithium ion storage battery pack and a power manager; and the solar cell wing, the shunt regulator, the bus filter, the comprehensive driving controller, the charging and discharging regulator, the lithium ion storage battery pack and the power manager are minimum replaceable units (ORU). Under the condition that related products of the power supply system break down, astronauts carry out on-orbit maintenance operation, and the service life of the power supply system is prolonged.

Description

technical field [0001] The invention relates to a space low-rail high-voltage power supply system supporting on-orbit maintenance, and belongs to the technical field of space power supplies. Background technique [0002] In the early space projects, the mission time of the aerospace system was short, the power was small, the system was relatively simple, and it was constrained by human activities outside the earth. The usual practice was to use high-reliability (zero) components or a large number of redundant designs and on-orbit backup to achieve high availability and high safety of the spacecraft. With the development of the third phase of my country's manned spaceflight, my country will build a long-term manned space station. The space station is different from any previous in-orbit aircraft in our country. It is a manned aircraft with long life, high reliability, high voltage and high power, and the system is more complicated. In order to achieve its 15-year long-life ...

Claims

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Application Information

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IPC IPC(8): B64G1/42B64G1/44H02J1/10H02J7/35
CPCB64G1/428B64G1/443H02J1/10H02J7/35
Inventor 冷学敏马季军乔卫新王田周妍葛茂艳
Owner SHANGHAI INST OF SPACE POWER SOURCES
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