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High-power-density high-pulse load power supply platform

A technology of high power density and load power supply, which is applied in current collectors, photovoltaic power generation, electric vehicles, etc., can solve the problems of high launch cost, low power density, increased weight and volume, and achieve high power density, high efficiency, and realization of The effect of wireless energy sharing

Inactive Publication Date: 2018-12-07
SHENZHEN AEROSPACE NEW POWER TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The traditional method needs to be realized by continuously increasing the power of the power controller of the satellite platform. The weight and volume increase with the increase of power, the power density is low, and the launch cost is high.

Method used

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  • High-power-density high-pulse load power supply platform
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Examples

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Embodiment Construction

[0018] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0019] The present invention proposes a power supply platform suitable for high power density and high pulse loads, which is based on an integrated power controller bus architecture, such as figure 1 As shown, it includes a bidirectional buck-boost supercapacitor charging and discharging module (CCDR), which provides instantaneous high power for dynamic pulse loads or electric propulsion power (PPU) and other payloads. At the same time, the architecture includes wired grid-connected controllers and wireless The energy transmission module realizes energy interconnection among multiple power controllers / busbars.

[0020] Integrated three ports achieve high power density and high efficiency

[0021] The integrated power controller puts the shunt SR module, battery charge regulator BCR module and battery discharge regulator BDR module in the tra...

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Abstract

The invention provides a high-power-density high-pulse load power supply platform which is based on an integrated power supply controller bus framework. The platform includes an integrated power supply controller, a solar cell array, a storage battery, a bus, an MPPT module, a wired energy transmission module and a wireless energy transmission module, a load and a super-capacitor charging / discharging CDDR module, the integrated power supply controller is realized by adopting a three-port converter, the three-port converter is connected with the solar cell array, a storage battery and a bus, the MPPT module is integrated in the integrated power supply controller; an 'Energy LAN' consisting of multiple solar array-battery DC power supply systems PBPS is connected with the bus via a wired grid-connected controller; the CDDR module is arranged between the online and pulsed load and used for charging and discharging the super capacitor through a bidirectional boosting and voltage reducing module, so that a small average power is input, and the larger peak pulse power is output.

Description

technical field [0001] The invention relates to the technical field of power supply control, in particular to a high power density and high pulse load power supply platform. Background technique [0002] Under complex space conditions and multi-task requirements, in order to meet the normal work of different types of payloads, higher requirements are put forward for satellite power controllers. In particular, repetitive pulse loads require the input of very high energy, ie, pulse or burst energy, for a very short period of time. The traditional method needs to be realized by continuously increasing the power of the power controller of the satellite platform. The weight and volume increase with the increase of power, the power density is low, and the launch cost is high. Contents of the invention [0003] In order to solve the problems in the prior art, the present invention provides a high power density high pulse load power supply platform, and the present invention is s...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02J7/35H02J7/34H02J50/20
CPCH02J7/345H02J7/35H02J50/20Y02E10/56
Inventor 韩悦朱洪雨张艺刘清张博温柳新军
Owner SHENZHEN AEROSPACE NEW POWER TECH
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