Method for measuring mass center of large-wing aircraft
The invention relates to a method for measuring the mass center of a large-wing aircraft, and the method comprises the steps: placing a to-be-measured aircraft on mass and mass center measurement equipment, and reading the mass of the to-be-measured aircraft; defining an aircraft coordinate system a...
Gespeichert in:
Hauptverfasser: | , , , , , , , , , , , , , |
---|---|
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 | WU YUXIANG CHEN LONG LIU YAFEN DU WENTAO PENG ZHIXIANG JU XINXING XU JIAN ZHOU XUAN LIU SHAOYONG KATSUNAGA MIN GAO XIANG LI MINGZHANG WAN XIANGXIANG CAO HONGYOU |
description | The invention relates to a method for measuring the mass center of a large-wing aircraft, and the method comprises the steps: placing a to-be-measured aircraft on mass and mass center measurement equipment, and reading the mass of the to-be-measured aircraft; defining an aircraft coordinate system as a left-hand system three-dimensional coordinate system, taking the head of the aircraft as an original point, and taking the inverse course of the aircraft as an x axis; solving the moment of the y axis through an unbalanced moment method to obtain an axial centroid xc; solving the moment of the x axis through an unbalanced moment method to obtain an axial centroid yc; respectively rotating the aircraft to be measured anticlockwise and clockwise around the x axis, and obtaining corresponding centroids xc1 and xc2 according to the method of the previous two steps; centroids yc1 and yc2; and calculating the radial centroid zc of the flight to be measured. The problem that the mass center cannot be measured due to t |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN116046261A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN116046261A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN116046261A3</originalsourceid><addsrcrecordid>eNrjZDD3TS3JyE9RSMsvUshNTSwuLcrMS1fITSwuVkhOzStJLVLIT1PISSxKT9UtB8kkZhYlFyWmlfAwsKYl5hSn8kJpbgZFN9cQZw_d1IL8-NTigkSg7tSSeGc_Q0MzAxMzIzNDR2Ni1AAAuH0tqg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Method for measuring mass center of large-wing aircraft</title><source>esp@cenet</source><creator>WU YUXIANG ; CHEN LONG ; LIU YAFEN ; DU WENTAO ; PENG ZHIXIANG ; JU XINXING ; XU JIAN ; ZHOU XUAN ; LIU SHAOYONG ; KATSUNAGA MIN ; GAO XIANG ; LI MINGZHANG ; WAN XIANGXIANG ; CAO HONGYOU</creator><creatorcontrib>WU YUXIANG ; CHEN LONG ; LIU YAFEN ; DU WENTAO ; PENG ZHIXIANG ; JU XINXING ; XU JIAN ; ZHOU XUAN ; LIU SHAOYONG ; KATSUNAGA MIN ; GAO XIANG ; LI MINGZHANG ; WAN XIANGXIANG ; CAO HONGYOU</creatorcontrib><description>The invention relates to a method for measuring the mass center of a large-wing aircraft, and the method comprises the steps: placing a to-be-measured aircraft on mass and mass center measurement equipment, and reading the mass of the to-be-measured aircraft; defining an aircraft coordinate system as a left-hand system three-dimensional coordinate system, taking the head of the aircraft as an original point, and taking the inverse course of the aircraft as an x axis; solving the moment of the y axis through an unbalanced moment method to obtain an axial centroid xc; solving the moment of the x axis through an unbalanced moment method to obtain an axial centroid yc; respectively rotating the aircraft to be measured anticlockwise and clockwise around the x axis, and obtaining corresponding centroids xc1 and xc2 according to the method of the previous two steps; centroids yc1 and yc2; and calculating the radial centroid zc of the flight to be measured. The problem that the mass center cannot be measured due to t</description><language>chi ; eng</language><subject>MEASURING ; PHYSICS ; TESTING ; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES ; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</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&date=20230502&DB=EPODOC&CC=CN&NR=116046261A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230502&DB=EPODOC&CC=CN&NR=116046261A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WU YUXIANG</creatorcontrib><creatorcontrib>CHEN LONG</creatorcontrib><creatorcontrib>LIU YAFEN</creatorcontrib><creatorcontrib>DU WENTAO</creatorcontrib><creatorcontrib>PENG ZHIXIANG</creatorcontrib><creatorcontrib>JU XINXING</creatorcontrib><creatorcontrib>XU JIAN</creatorcontrib><creatorcontrib>ZHOU XUAN</creatorcontrib><creatorcontrib>LIU SHAOYONG</creatorcontrib><creatorcontrib>KATSUNAGA MIN</creatorcontrib><creatorcontrib>GAO XIANG</creatorcontrib><creatorcontrib>LI MINGZHANG</creatorcontrib><creatorcontrib>WAN XIANGXIANG</creatorcontrib><creatorcontrib>CAO HONGYOU</creatorcontrib><title>Method for measuring mass center of large-wing aircraft</title><description>The invention relates to a method for measuring the mass center of a large-wing aircraft, and the method comprises the steps: placing a to-be-measured aircraft on mass and mass center measurement equipment, and reading the mass of the to-be-measured aircraft; defining an aircraft coordinate system as a left-hand system three-dimensional coordinate system, taking the head of the aircraft as an original point, and taking the inverse course of the aircraft as an x axis; solving the moment of the y axis through an unbalanced moment method to obtain an axial centroid xc; solving the moment of the x axis through an unbalanced moment method to obtain an axial centroid yc; respectively rotating the aircraft to be measured anticlockwise and clockwise around the x axis, and obtaining corresponding centroids xc1 and xc2 according to the method of the previous two steps; centroids yc1 and yc2; and calculating the radial centroid zc of the flight to be measured. The problem that the mass center cannot be measured due to t</description><subject>MEASURING</subject><subject>PHYSICS</subject><subject>TESTING</subject><subject>TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES</subject><subject>TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDD3TS3JyE9RSMsvUshNTSwuLcrMS1fITSwuVkhOzStJLVLIT1PISSxKT9UtB8kkZhYlFyWmlfAwsKYl5hSn8kJpbgZFN9cQZw_d1IL8-NTigkSg7tSSeGc_Q0MzAxMzIzNDR2Ni1AAAuH0tqg</recordid><startdate>20230502</startdate><enddate>20230502</enddate><creator>WU YUXIANG</creator><creator>CHEN LONG</creator><creator>LIU YAFEN</creator><creator>DU WENTAO</creator><creator>PENG ZHIXIANG</creator><creator>JU XINXING</creator><creator>XU JIAN</creator><creator>ZHOU XUAN</creator><creator>LIU SHAOYONG</creator><creator>KATSUNAGA MIN</creator><creator>GAO XIANG</creator><creator>LI MINGZHANG</creator><creator>WAN XIANGXIANG</creator><creator>CAO HONGYOU</creator><scope>EVB</scope></search><sort><creationdate>20230502</creationdate><title>Method for measuring mass center of large-wing aircraft</title><author>WU YUXIANG ; CHEN LONG ; LIU YAFEN ; DU WENTAO ; PENG ZHIXIANG ; JU XINXING ; XU JIAN ; ZHOU XUAN ; LIU SHAOYONG ; KATSUNAGA MIN ; GAO XIANG ; LI MINGZHANG ; WAN XIANGXIANG ; CAO HONGYOU</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN116046261A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</creationdate><topic>MEASURING</topic><topic>PHYSICS</topic><topic>TESTING</topic><topic>TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES</topic><topic>TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</topic><toplevel>online_resources</toplevel><creatorcontrib>WU YUXIANG</creatorcontrib><creatorcontrib>CHEN LONG</creatorcontrib><creatorcontrib>LIU YAFEN</creatorcontrib><creatorcontrib>DU WENTAO</creatorcontrib><creatorcontrib>PENG ZHIXIANG</creatorcontrib><creatorcontrib>JU XINXING</creatorcontrib><creatorcontrib>XU JIAN</creatorcontrib><creatorcontrib>ZHOU XUAN</creatorcontrib><creatorcontrib>LIU SHAOYONG</creatorcontrib><creatorcontrib>KATSUNAGA MIN</creatorcontrib><creatorcontrib>GAO XIANG</creatorcontrib><creatorcontrib>LI MINGZHANG</creatorcontrib><creatorcontrib>WAN XIANGXIANG</creatorcontrib><creatorcontrib>CAO HONGYOU</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WU YUXIANG</au><au>CHEN LONG</au><au>LIU YAFEN</au><au>DU WENTAO</au><au>PENG ZHIXIANG</au><au>JU XINXING</au><au>XU JIAN</au><au>ZHOU XUAN</au><au>LIU SHAOYONG</au><au>KATSUNAGA MIN</au><au>GAO XIANG</au><au>LI MINGZHANG</au><au>WAN XIANGXIANG</au><au>CAO HONGYOU</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Method for measuring mass center of large-wing aircraft</title><date>2023-05-02</date><risdate>2023</risdate><abstract>The invention relates to a method for measuring the mass center of a large-wing aircraft, and the method comprises the steps: placing a to-be-measured aircraft on mass and mass center measurement equipment, and reading the mass of the to-be-measured aircraft; defining an aircraft coordinate system as a left-hand system three-dimensional coordinate system, taking the head of the aircraft as an original point, and taking the inverse course of the aircraft as an x axis; solving the moment of the y axis through an unbalanced moment method to obtain an axial centroid xc; solving the moment of the x axis through an unbalanced moment method to obtain an axial centroid yc; respectively rotating the aircraft to be measured anticlockwise and clockwise around the x axis, and obtaining corresponding centroids xc1 and xc2 according to the method of the previous two steps; centroids yc1 and yc2; and calculating the radial centroid zc of the flight to be measured. The problem that the mass center cannot be measured due to t</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | chi ; eng |
recordid | cdi_epo_espacenet_CN116046261A |
source | esp@cenet |
subjects | MEASURING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR |
title | Method for measuring mass center of large-wing aircraft |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-28T05%3A48%3A37IST&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=WU%20YUXIANG&rft.date=2023-05-02&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN116046261A%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 |