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

Component space radiation effect detection device

A detection device and space radiation technology, applied in the field of space environment detection, can solve problems such as inaccuracy of assessment results, achieve the effects of small size, improved accuracy, and easy installation and debugging

Inactive Publication Date: 2018-06-15
SHANDONG INST OF AEROSPACE ELECTRONICS TECH +1
View PDF6 Cites 3 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Since the space radiation environment is often different at different locations and at different times in space, this method only assesses electronic components under space radiation conditions, but fails to combine the information of the space environment on orbit. Therefore, the assessment results are somewhat inaccurate Spend

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
  • Component space radiation effect detection device
  • Component space radiation effect detection device
  • Component space radiation effect detection device

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0026] The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0027] The invention provides a device for detecting space radiation effects of components, such as figure 1 , figure 2 , image 3 As shown, the detection device includes a radiation environment probe 1 , a component detection module 2 , an amplification module 3 , a control module 4 , a power module 5 and a casing 6 , and the front cover and the rear cover of the casing 6 are fixedly connected by a connecting screw 7 .

[0028] The radiation environment probe 1 is used to obtain space radiation environment data; the radiation environment probe 1 includes a LET probe and a proton probe, and the LET probe includes a low LET probe and a high LET probe. The three probes are respectively installed in independent structures, and each is connected to the corresponding amplifying module 3 through lead-out wires. The amplification module 3 is independent, whic...

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 present invention discloses a component space radiation effect detection device. A radiation environment probe is added to obtain space radiation environment information of a current position whenan electronic component on-orbit test is performed. The component space radiation effect detection device combines real-time measured space radiation environment to perform checking of a measured component so as to improve the accuracy of the assessment of the electronic component space environmental suitability.

Description

technical field [0001] The invention relates to the technical field of space environment detection, in particular to a device combining electronic components and space radiation environment detection. Background technique [0002] The on-orbit verification of domestic electronic components is one of the important tasks of spaceborne experiments. The main purpose of on-orbit verification of electronic components is to assess the radiation resistance of electronic components in the space radiation environment. For example, the space radiation effect experimental unit carried in our satellites assesses the space adaptability of electronic components under the action of space radiation, so as to provide support for the evaluation of future electronic components in orbit. In the design of the experimental device, the detection circuit is mainly designed around the device under test. The detection circuit can detect the voltage, current, and single event upset of the device under...

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): G01T1/24
CPCG01T1/24
Inventor 李璟璟邵思霈任文冠王博胡喜庆郝晓云潘睿元肖婷刘金胜刘泳王月张玉兔王世金
Owner SHANDONG INST OF AEROSPACE ELECTRONICS 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