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

A device and method for energy conversion of space debris based on laser propulsion

A space debris and energy conversion technology, which is applied to thrust reversers, plasma, machines/engines, etc., can solve the problems of ineffective utilization of space debris materials, and achieve the effect of high conversion and utilization efficiency, simple structure, and effective removal

Active Publication Date: 2018-11-30
CHINA ACAD OF LAUNCH VEHICLE TECH
View PDF6 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a space debris energy conversion device and method based on laser propulsion to solve the problem that the space debris material in the traditional space maintenance method cannot be effectively used

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
  • A device and method for energy conversion of space debris based on laser propulsion
  • A device and method for energy conversion of space debris based on laser propulsion
  • A device and method for energy conversion of space debris based on laser propulsion

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0039] Such as figure 1 As shown, the space debris energy conversion device based on laser propulsion provided in this embodiment includes a device body and an optical collimation mechanism 1, an optical beam splitting mechanism 2, an optical working fluid coupling mechanism 3 and A working fluid supply mechanism 4, wherein the optical beam splitting mechanism 2 is arranged at the bottom of the optical collimation mechanism 1, and the working medium coupling mechanism 3 is correspondingly arranged in a beam output direction of the optical beam splitting mechanism 2, so The optical working medium coupling mechanism 3 is connected to the working medium supply mechanism 4 .

[0040] In use, the optical collimation mechanism is used to collimate the incident laser beam, and transmit the collimated laser beam to the optical beam splitting mechanism. The optical beam splitting mechanism is used to split the collimated laser beam into split laser beams in a specified direction, and ...

Embodiment 2

[0042] Such as figure 2 As shown, the space debris energy conversion device based on laser propulsion provided in this embodiment includes a device body and an optical collimation mechanism 1, an optical beam splitting mechanism 2, and four optical working fluid coupling mechanisms 3 respectively arranged on the device body and four working fluid supply mechanisms 4, wherein the optical beam splitting mechanism 2 is arranged at the bottom of the optical collimation mechanism 1, and each of the optical working fluid coupling mechanisms 3 is respectively arranged in front of the optical beam splitting mechanism 2, In the rear, left, and right four beam output directions, each of the optical working medium coupling mechanisms 3 is connected to each of the working medium supply mechanisms 4 in a one-to-one correspondence.

[0043] In use, the optical collimation mechanism is used to collimate the incident laser beam, and transmit the collimated laser beam to the optical beam spli...

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 relates to the technical field of space debris utilization, in particular to a space debris energy transformation device and method based on laser propelling. The device comprises a device body, an optical aligning mechanism, an optical beam splitting mechanism, optical working medium coupling mechanism and working medium supplying mechanisms, wherein the optical beam splitting mechanism is arranged on the bottom of the optical aligning mechanism, and the optical working medium coupling mechanisms are correspondingly connected with the working medium supplying mechanisms in a one-to-one manner. According to the space debris energy transformation device and method based on laser propelling, space debris serves as a solid working medium for laser propelling, by means of interaction of laser and the collected space debris, space debris ablation and gasification are caused, the space debris is ionized to form plasmas, plasma deflagration waves compress the surface of the space debris to produce thrust, so that reuse of the space debris is achieved. The space debris energy transformation device has the beneficial effects that the structure is simple, the energy transformation utilization rate is high, and secondary pollution cannot be caused for the space environment. The space debris energy transformation and method based on laser propelling can be directly applied to in-orbit control over spacecrafts.

Description

technical field [0001] The invention relates to the technical field of space debris utilization. Background technique [0002] As a harmful existence, space debris has restricted and harmed space activities for a long time, and the increasing number of space debris has seriously affected space security. The traditional way of space maintenance is to remove space debris from orbit, which can protect the operating environment of space vehicles, but it also causes direct waste of these space debris materials. Therefore, to explore a way to effectively use space debris to serve space vehicles The new approach has great application value. Contents of the invention [0003] (1) Technical problems to be solved [0004] The purpose of the present invention is to provide a space debris energy conversion device and method based on laser propulsion to solve the problem that space debris materials in traditional space maintenance methods cannot be effectively utilized. [0005] (2)...

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 Patents(China)
IPC IPC(8): F03H1/00
CPCF03H1/00
Inventor 范国臣陈巍黄虎张耀磊易娟李月乙冉冉吕殿君温聚英李成祥赵大海刘岱
Owner CHINA ACAD OF LAUNCH VEHICLE TECH
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

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com