Comprehensive evaluation method for surface integrity of laser paint removal matrix of aircraft aluminum alloy skin

The invention relates to the technical field of aircraft aluminum alloy skin laser paint removal, in particular to a comprehensive evaluation method for aircraft aluminum alloy skin laser paint removal matrix surface integrity. Comprising the steps of S1, determining a surface integrity evaluation i...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: YANG XIAOQIANG, TAN DEQIANG, YANG WENFENG, LI QING, CHANG XUEDONG, HU YUE, LI SHAOLONG, LYU SHUANGQI
Format: Patent
Sprache:chi ; eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator YANG XIAOQIANG
TAN DEQIANG
YANG WENFENG
LI QING
CHANG XUEDONG
HU YUE
LI SHAOLONG
LYU SHUANGQI
description The invention relates to the technical field of aircraft aluminum alloy skin laser paint removal, in particular to a comprehensive evaluation method for aircraft aluminum alloy skin laser paint removal matrix surface integrity. Comprising the steps of S1, determining a surface integrity evaluation index, S2, constructing a multi-stage comprehensive evaluation system, S3, determining an evaluation grade, S4, determining an index set and an evaluation set, S5, determining a first-stage index weight, S6, determining a second-stage index weight, S7, constructing an evaluation (membership) matrix of a second-stage index, S8, performing first-stage comprehensive evaluation on each index, S9, constructing an evaluation (membership) matrix of the first-stage index, and S10, performing first-stage comprehensive evaluation on each index. S11, a final conclusion is obtained, the final target is evaluated according to the evaluation grade according to the calculation result and the maximum membership degree principle, an
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN116011707A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN116011707A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN116011707A3</originalsourceid><addsrcrecordid>eNqNTUsKwjAQ7caFqHcYDyA0CHYtpeLKlfsy1IkdTDJhkhZ7eyN4AFfv8b7rKrXio9JIIfFMQDO6CTNLAE95lAdYUUiTWhwIOGR6KucFxILDRAoRiwhKXkoTPGbl99dF1kHRZih7nsPkC3GyQHpx2FYriy7R7oeban_p7u31QFF6SrFcBcp9ezPmVBvT1M35-E_mA8RlRTw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Comprehensive evaluation method for surface integrity of laser paint removal matrix of aircraft aluminum alloy skin</title><source>esp@cenet</source><creator>YANG XIAOQIANG ; TAN DEQIANG ; YANG WENFENG ; LI QING ; CHANG XUEDONG ; HU YUE ; LI SHAOLONG ; LYU SHUANGQI</creator><creatorcontrib>YANG XIAOQIANG ; TAN DEQIANG ; YANG WENFENG ; LI QING ; CHANG XUEDONG ; HU YUE ; LI SHAOLONG ; LYU SHUANGQI</creatorcontrib><description>The invention relates to the technical field of aircraft aluminum alloy skin laser paint removal, in particular to a comprehensive evaluation method for aircraft aluminum alloy skin laser paint removal matrix surface integrity. Comprising the steps of S1, determining a surface integrity evaluation index, S2, constructing a multi-stage comprehensive evaluation system, S3, determining an evaluation grade, S4, determining an index set and an evaluation set, S5, determining a first-stage index weight, S6, determining a second-stage index weight, S7, constructing an evaluation (membership) matrix of a second-stage index, S8, performing first-stage comprehensive evaluation on each index, S9, constructing an evaluation (membership) matrix of the first-stage index, and S10, performing first-stage comprehensive evaluation on each index. S11, a final conclusion is obtained, the final target is evaluated according to the evaluation grade according to the calculation result and the maximum membership degree principle, an</description><language>chi ; eng</language><subject>CALCULATING ; CLEANING ; CLEANING IN GENERAL ; COMPUTING ; COUNTING ; DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FORADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORYOR FORECASTING PURPOSES ; ELECTRIC DIGITAL DATA PROCESSING ; PERFORMING OPERATIONS ; PHYSICS ; PREVENTION OF FOULING IN GENERAL ; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE,COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTINGPURPOSES, NOT OTHERWISE PROVIDED FOR ; TRANSPORTING</subject><creationdate>2023</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20230425&amp;DB=EPODOC&amp;CC=CN&amp;NR=116011707A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20230425&amp;DB=EPODOC&amp;CC=CN&amp;NR=116011707A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>YANG XIAOQIANG</creatorcontrib><creatorcontrib>TAN DEQIANG</creatorcontrib><creatorcontrib>YANG WENFENG</creatorcontrib><creatorcontrib>LI QING</creatorcontrib><creatorcontrib>CHANG XUEDONG</creatorcontrib><creatorcontrib>HU YUE</creatorcontrib><creatorcontrib>LI SHAOLONG</creatorcontrib><creatorcontrib>LYU SHUANGQI</creatorcontrib><title>Comprehensive evaluation method for surface integrity of laser paint removal matrix of aircraft aluminum alloy skin</title><description>The invention relates to the technical field of aircraft aluminum alloy skin laser paint removal, in particular to a comprehensive evaluation method for aircraft aluminum alloy skin laser paint removal matrix surface integrity. Comprising the steps of S1, determining a surface integrity evaluation index, S2, constructing a multi-stage comprehensive evaluation system, S3, determining an evaluation grade, S4, determining an index set and an evaluation set, S5, determining a first-stage index weight, S6, determining a second-stage index weight, S7, constructing an evaluation (membership) matrix of a second-stage index, S8, performing first-stage comprehensive evaluation on each index, S9, constructing an evaluation (membership) matrix of the first-stage index, and S10, performing first-stage comprehensive evaluation on each index. S11, a final conclusion is obtained, the final target is evaluated according to the evaluation grade according to the calculation result and the maximum membership degree principle, an</description><subject>CALCULATING</subject><subject>CLEANING</subject><subject>CLEANING IN GENERAL</subject><subject>COMPUTING</subject><subject>COUNTING</subject><subject>DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FORADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORYOR FORECASTING PURPOSES</subject><subject>ELECTRIC DIGITAL DATA PROCESSING</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>PREVENTION OF FOULING IN GENERAL</subject><subject>SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE,COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTINGPURPOSES, NOT OTHERWISE PROVIDED FOR</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNTUsKwjAQ7caFqHcYDyA0CHYtpeLKlfsy1IkdTDJhkhZ7eyN4AFfv8b7rKrXio9JIIfFMQDO6CTNLAE95lAdYUUiTWhwIOGR6KucFxILDRAoRiwhKXkoTPGbl99dF1kHRZih7nsPkC3GyQHpx2FYriy7R7oeban_p7u31QFF6SrFcBcp9ezPmVBvT1M35-E_mA8RlRTw</recordid><startdate>20230425</startdate><enddate>20230425</enddate><creator>YANG XIAOQIANG</creator><creator>TAN DEQIANG</creator><creator>YANG WENFENG</creator><creator>LI QING</creator><creator>CHANG XUEDONG</creator><creator>HU YUE</creator><creator>LI SHAOLONG</creator><creator>LYU SHUANGQI</creator><scope>EVB</scope></search><sort><creationdate>20230425</creationdate><title>Comprehensive evaluation method for surface integrity of laser paint removal matrix of aircraft aluminum alloy skin</title><author>YANG XIAOQIANG ; TAN DEQIANG ; YANG WENFENG ; LI QING ; CHANG XUEDONG ; HU YUE ; LI SHAOLONG ; LYU SHUANGQI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN116011707A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</creationdate><topic>CALCULATING</topic><topic>CLEANING</topic><topic>CLEANING IN GENERAL</topic><topic>COMPUTING</topic><topic>COUNTING</topic><topic>DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FORADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORYOR FORECASTING PURPOSES</topic><topic>ELECTRIC DIGITAL DATA PROCESSING</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>PREVENTION OF FOULING IN GENERAL</topic><topic>SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE,COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTINGPURPOSES, NOT OTHERWISE PROVIDED FOR</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>YANG XIAOQIANG</creatorcontrib><creatorcontrib>TAN DEQIANG</creatorcontrib><creatorcontrib>YANG WENFENG</creatorcontrib><creatorcontrib>LI QING</creatorcontrib><creatorcontrib>CHANG XUEDONG</creatorcontrib><creatorcontrib>HU YUE</creatorcontrib><creatorcontrib>LI SHAOLONG</creatorcontrib><creatorcontrib>LYU SHUANGQI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>YANG XIAOQIANG</au><au>TAN DEQIANG</au><au>YANG WENFENG</au><au>LI QING</au><au>CHANG XUEDONG</au><au>HU YUE</au><au>LI SHAOLONG</au><au>LYU SHUANGQI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Comprehensive evaluation method for surface integrity of laser paint removal matrix of aircraft aluminum alloy skin</title><date>2023-04-25</date><risdate>2023</risdate><abstract>The invention relates to the technical field of aircraft aluminum alloy skin laser paint removal, in particular to a comprehensive evaluation method for aircraft aluminum alloy skin laser paint removal matrix surface integrity. Comprising the steps of S1, determining a surface integrity evaluation index, S2, constructing a multi-stage comprehensive evaluation system, S3, determining an evaluation grade, S4, determining an index set and an evaluation set, S5, determining a first-stage index weight, S6, determining a second-stage index weight, S7, constructing an evaluation (membership) matrix of a second-stage index, S8, performing first-stage comprehensive evaluation on each index, S9, constructing an evaluation (membership) matrix of the first-stage index, and S10, performing first-stage comprehensive evaluation on each index. S11, a final conclusion is obtained, the final target is evaluated according to the evaluation grade according to the calculation result and the maximum membership degree principle, an</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN116011707A
source esp@cenet
subjects CALCULATING
CLEANING
CLEANING IN GENERAL
COMPUTING
COUNTING
DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FORADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORYOR FORECASTING PURPOSES
ELECTRIC DIGITAL DATA PROCESSING
PERFORMING OPERATIONS
PHYSICS
PREVENTION OF FOULING IN GENERAL
SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE,COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTINGPURPOSES, NOT OTHERWISE PROVIDED FOR
TRANSPORTING
title Comprehensive evaluation method for surface integrity of laser paint removal matrix of aircraft aluminum alloy skin
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-17T19%3A11%3A03IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=YANG%20XIAOQIANG&rft.date=2023-04-25&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN116011707A%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true