High-precision rapid aerodynamic heat identification method

According to the high-precision rapid aerodynamic heat identification method, temperature data needing to be identified is divided into N identification time periods, segmentation identification is carried out according to the time sequence to reduce the solving data size and accelerate iteration, d...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: KANG HONGLIN, LI ZELIANG, ZHOU DAN
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 KANG HONGLIN
LI ZELIANG
ZHOU DAN
description According to the high-precision rapid aerodynamic heat identification method, temperature data needing to be identified is divided into N identification time periods, segmentation identification is carried out according to the time sequence to reduce the solving data size and accelerate iteration, data transmission is fully utilized in solving, calculation time is reduced in a geometric progression mode, and the identification accuracy of the aerodynamic heat is improved. The solution time is close to the time of the total amount/N, and meanwhile, the direction of heat flow variation is determined by comparing the identification temperature with the reference temperature; errors caused by comparison of identification heat flows fixed in all previous'identification time periods' and real heat flows are superposed on a measured temperature according to a certain proportionality coefficient, the measured temperature is corrected, a reference temperature of a current time point is formed, and reference distortion
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN117993175A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN117993175A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN117993175A3</originalsourceid><addsrcrecordid>eNrjZLD2yEzP0C0oSk3OLM7Mz1MoSizITFFITC3KT6nMS8zNTFbISE0sUchMSc0ryUzLTE4sAanKTS3JyE_hYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxzn6GhuaWlsaG5qaOxsSoAQDVsC_a</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>High-precision rapid aerodynamic heat identification method</title><source>esp@cenet</source><creator>KANG HONGLIN ; LI ZELIANG ; ZHOU DAN</creator><creatorcontrib>KANG HONGLIN ; LI ZELIANG ; ZHOU DAN</creatorcontrib><description>According to the high-precision rapid aerodynamic heat identification method, temperature data needing to be identified is divided into N identification time periods, segmentation identification is carried out according to the time sequence to reduce the solving data size and accelerate iteration, data transmission is fully utilized in solving, calculation time is reduced in a geometric progression mode, and the identification accuracy of the aerodynamic heat is improved. The solution time is close to the time of the total amount/N, and meanwhile, the direction of heat flow variation is determined by comparing the identification temperature with the reference temperature; errors caused by comparison of identification heat flows fixed in all previous'identification time periods' and real heat flows are superposed on a measured temperature according to a certain proportionality coefficient, the measured temperature is corrected, a reference temperature of a current time point is formed, and reference distortion</description><language>chi ; eng</language><subject>CALCULATING ; COMPUTING ; COUNTING ; ELECTRIC DIGITAL DATA PROCESSING ; MEASURING ; MEASURING QUANTITY OF HEAT ; MEASURING TEMPERATURE ; PHYSICS ; TESTING ; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR</subject><creationdate>2024</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=20240507&amp;DB=EPODOC&amp;CC=CN&amp;NR=117993175A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20240507&amp;DB=EPODOC&amp;CC=CN&amp;NR=117993175A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KANG HONGLIN</creatorcontrib><creatorcontrib>LI ZELIANG</creatorcontrib><creatorcontrib>ZHOU DAN</creatorcontrib><title>High-precision rapid aerodynamic heat identification method</title><description>According to the high-precision rapid aerodynamic heat identification method, temperature data needing to be identified is divided into N identification time periods, segmentation identification is carried out according to the time sequence to reduce the solving data size and accelerate iteration, data transmission is fully utilized in solving, calculation time is reduced in a geometric progression mode, and the identification accuracy of the aerodynamic heat is improved. The solution time is close to the time of the total amount/N, and meanwhile, the direction of heat flow variation is determined by comparing the identification temperature with the reference temperature; errors caused by comparison of identification heat flows fixed in all previous'identification time periods' and real heat flows are superposed on a measured temperature according to a certain proportionality coefficient, the measured temperature is corrected, a reference temperature of a current time point is formed, and reference distortion</description><subject>CALCULATING</subject><subject>COMPUTING</subject><subject>COUNTING</subject><subject>ELECTRIC DIGITAL DATA PROCESSING</subject><subject>MEASURING</subject><subject>MEASURING QUANTITY OF HEAT</subject><subject>MEASURING TEMPERATURE</subject><subject>PHYSICS</subject><subject>TESTING</subject><subject>THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLD2yEzP0C0oSk3OLM7Mz1MoSizITFFITC3KT6nMS8zNTFbISE0sUchMSc0ryUzLTE4sAanKTS3JyE_hYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxzn6GhuaWlsaG5qaOxsSoAQDVsC_a</recordid><startdate>20240507</startdate><enddate>20240507</enddate><creator>KANG HONGLIN</creator><creator>LI ZELIANG</creator><creator>ZHOU DAN</creator><scope>EVB</scope></search><sort><creationdate>20240507</creationdate><title>High-precision rapid aerodynamic heat identification method</title><author>KANG HONGLIN ; LI ZELIANG ; ZHOU DAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN117993175A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2024</creationdate><topic>CALCULATING</topic><topic>COMPUTING</topic><topic>COUNTING</topic><topic>ELECTRIC DIGITAL DATA PROCESSING</topic><topic>MEASURING</topic><topic>MEASURING QUANTITY OF HEAT</topic><topic>MEASURING TEMPERATURE</topic><topic>PHYSICS</topic><topic>TESTING</topic><topic>THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR</topic><toplevel>online_resources</toplevel><creatorcontrib>KANG HONGLIN</creatorcontrib><creatorcontrib>LI ZELIANG</creatorcontrib><creatorcontrib>ZHOU DAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KANG HONGLIN</au><au>LI ZELIANG</au><au>ZHOU DAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>High-precision rapid aerodynamic heat identification method</title><date>2024-05-07</date><risdate>2024</risdate><abstract>According to the high-precision rapid aerodynamic heat identification method, temperature data needing to be identified is divided into N identification time periods, segmentation identification is carried out according to the time sequence to reduce the solving data size and accelerate iteration, data transmission is fully utilized in solving, calculation time is reduced in a geometric progression mode, and the identification accuracy of the aerodynamic heat is improved. The solution time is close to the time of the total amount/N, and meanwhile, the direction of heat flow variation is determined by comparing the identification temperature with the reference temperature; errors caused by comparison of identification heat flows fixed in all previous'identification time periods' and real heat flows are superposed on a measured temperature according to a certain proportionality coefficient, the measured temperature is corrected, a reference temperature of a current time point is formed, and reference distortion</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN117993175A
source esp@cenet
subjects CALCULATING
COMPUTING
COUNTING
ELECTRIC DIGITAL DATA PROCESSING
MEASURING
MEASURING QUANTITY OF HEAT
MEASURING TEMPERATURE
PHYSICS
TESTING
THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
title High-precision rapid aerodynamic heat identification method
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-23T00%3A16%3A43IST&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=KANG%20HONGLIN&rft.date=2024-05-07&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN117993175A%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