Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

High-power laser constant current source circuit for space navigation

A high-power laser and power circuit technology, applied in lasers, laser parts, semiconductor lasers, etc., can solve the limitations of weight, volume, operating conditions, the inability to guarantee the implementation of load distribution solutions on orbit, and the inability of satellite platforms to provide resources, etc. problem, to achieve the effect of low loss, reduced switching loss, and simple circuit structure

Pending Publication Date: 2021-10-22
SHANGHAI INST OF SPACE POWER SOURCES
View PDF5 Cites 2 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The total power of the space laser load is 86.4KW, the on-orbit cycle works for 2mins, and the work cycle interval is 3~4h. The existing constant current power supply for aerospace has a power density of no more than 1000W / kg, so the weight of a single power supply for the laser load exceeds 100kg , the satellite platform cannot provide such a huge resource, and cannot guarantee the on-orbit implementation of the load distribution scheme
[0004] At present, most of the high-power constant current source circuits that have been disclosed are long-term stable load output. Due to the limitations of the space environment on the weight, volume, and operating conditions of the load drive power supply, the constant current source circuit for space laser loads needs to be further developed.

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • High-power laser constant current source circuit for space navigation
  • High-power laser constant current source circuit for space navigation
  • High-power laser constant current source circuit for space navigation

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0089] A constant current source circuit for an aerospace high-power laser proposed by the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments. The advantages and features of the present invention will become clearer from the following description. It should be noted that the drawings are in a very simplified form and all use imprecise scales, which are only used to facilitate and clearly assist the purpose of illustrating the embodiments of the present invention. In order to make the objects, features and advantages of the present invention more comprehensible, please refer to the accompanying drawings. It should be noted that the structures, proportions, sizes, etc. shown in the drawings attached to this specification are only used to match the content disclosed in the specification, for those who are familiar with this technology to understand and read, and are not used to limit the implementatio...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention discloses a high-power laser constant-current source circuit for space navigation, which comprises a plurality of Superboost constant-current driving power supply modules, which are connected in parallel and a plurality of high-voltage storage battery packs, the input end of each Superboost constant-current driving power supply module being correspondingly connected to the two ends of one high-voltage storage battery pack in parallel; and a plurality of laser load power supply pump modules, wherein the output end of each Superboost constant current driving power supply module is correspondingly connected with one laser load power supply pump module, and each Superboost constant-current driving power supply module is used for driving the corresponding laser load power supply pump module in a constant-current manner. The driving power supply has the characteristics of high stability, high power, high efficiency and high power density, and meets the performance requirements of the laser load for space navigation on the driving power supply.

Description

technical field [0001] The invention relates to the field of power supply for space laser loads, in particular to a constant current source circuit for a high-power laser used in aerospace. Background technique [0002] With the continuous development of semiconductor laser technology, semiconductor lasers have entered the field of high current from the traditional small current field, and are widely used in laser radar, laser navigation, laser ranging and other fields. Most of the working methods of semiconductor lasers are excited by current injection. The load characteristics of the laser are diode characteristics. By applying forward current, the excited atoms are controlled to generate laser output. Therefore, the performance of the laser constant current drive power directly affects the performance of the laser, and the development of a stable and reliable constant current drive power is very important for the normal operation of the entire laser. [0003] In recent y...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): H02M3/07H02M1/36H02J7/00H01S5/042
CPCH02M3/07H02M1/36H02J7/0063H01S5/042H02J2207/20
Inventor 吴家旺李小春金家瑶徐刚李旭评
Owner SHANGHAI INST OF SPACE POWER SOURCES
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products