Six-component balance for wind tunnel jet flow experiment and application mode thereof

Six-component balance for wind tunnel jet flow experiment and application mode thereof

The invention belongs to the technical field of wind tunnel experiment testing devices, and discloses a six-component balance for a wind tunnel jet flow experiment and an application mode of the six-component balance. The whole six-component balance is of a tubular structure, the front section is a...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: ZHANG LIBO, HE PINGWEI, MA TAO, ZHANG CHANGFENG, PAN HUAYE, LI TENGJI, WANG SHUMIN, ZHANG WEI
Format: Patent
Sprache:chi ; eng
Schlagworte:
MEASURING
PHYSICS
TESTING
TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES
TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
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 ZHANG LIBO
HE PINGWEI
MA TAO
ZHANG CHANGFENG
PAN HUAYE
LI TENGJI
WANG SHUMIN
ZHANG WEI
description The invention belongs to the technical field of wind tunnel experiment testing devices, and discloses a six-component balance for a wind tunnel jet flow experiment and an application mode of the six-component balance. The whole six-component balance is of a tubular structure, the front section is a spray pipe connecting flange fixedly connected with a model engine spray pipe, the middle section is a measuring section, the rear section is a gas supply pipeline connecting flange fixedly connected with a gas supply pipeline, a through hole is formed in the central axis of the six-component balance, and the through hole is the gas supply pipeline for jetting medium gas; the measuring section is provided with a resistance element strain cavity, and a resistance strain beam is arranged in the resistance element strain cavity. The application mode comprises a middle resistance element strain cavity six-component balance and a front resistance element strain cavity six-component balance. The six-component balance ado
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN115077853A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN115077853A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN115077853A3</originalsourceid><addsrcrecordid>eNqNyjEKwkAQRuE0FqLeYTxAwBBCbCUoVjaKbRg3_5KV3ZklWUmOr4IHsHrF-5bZ_erm3GiIKpBED_YsBmR1oMlJR-klAk9PJLJeJ8IcMbjwtfzZHKN3hpNToaAdKPUYoHadLSz7EZtfV9n2dLw15xxRW4yRDQSpbS5FUe3qel-Vh_If8wYw6jnF</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Six-component balance for wind tunnel jet flow experiment and application mode thereof</title><source>esp@cenet</source><creator>ZHANG LIBO ; HE PINGWEI ; MA TAO ; ZHANG CHANGFENG ; PAN HUAYE ; LI TENGJI ; WANG SHUMIN ; ZHANG WEI</creator><creatorcontrib>ZHANG LIBO ; HE PINGWEI ; MA TAO ; ZHANG CHANGFENG ; PAN HUAYE ; LI TENGJI ; WANG SHUMIN ; ZHANG WEI</creatorcontrib><description>The invention belongs to the technical field of wind tunnel experiment testing devices, and discloses a six-component balance for a wind tunnel jet flow experiment and an application mode of the six-component balance. The whole six-component balance is of a tubular structure, the front section is a spray pipe connecting flange fixedly connected with a model engine spray pipe, the middle section is a measuring section, the rear section is a gas supply pipeline connecting flange fixedly connected with a gas supply pipeline, a through hole is formed in the central axis of the six-component balance, and the through hole is the gas supply pipeline for jetting medium gas; the measuring section is provided with a resistance element strain cavity, and a resistance strain beam is arranged in the resistance element strain cavity. The application mode comprises a middle resistance element strain cavity six-component balance and a front resistance element strain cavity six-component balance. The six-component balance ado</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>2022</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=20220920&amp;DB=EPODOC&amp;CC=CN&amp;NR=115077853A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20220920&amp;DB=EPODOC&amp;CC=CN&amp;NR=115077853A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ZHANG LIBO</creatorcontrib><creatorcontrib>HE PINGWEI</creatorcontrib><creatorcontrib>MA TAO</creatorcontrib><creatorcontrib>ZHANG CHANGFENG</creatorcontrib><creatorcontrib>PAN HUAYE</creatorcontrib><creatorcontrib>LI TENGJI</creatorcontrib><creatorcontrib>WANG SHUMIN</creatorcontrib><creatorcontrib>ZHANG WEI</creatorcontrib><title>Six-component balance for wind tunnel jet flow experiment and application mode thereof</title><description>The invention belongs to the technical field of wind tunnel experiment testing devices, and discloses a six-component balance for a wind tunnel jet flow experiment and an application mode of the six-component balance. The whole six-component balance is of a tubular structure, the front section is a spray pipe connecting flange fixedly connected with a model engine spray pipe, the middle section is a measuring section, the rear section is a gas supply pipeline connecting flange fixedly connected with a gas supply pipeline, a through hole is formed in the central axis of the six-component balance, and the through hole is the gas supply pipeline for jetting medium gas; the measuring section is provided with a resistance element strain cavity, and a resistance strain beam is arranged in the resistance element strain cavity. The application mode comprises a middle resistance element strain cavity six-component balance and a front resistance element strain cavity six-component balance. The six-component balance ado</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>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyjEKwkAQRuE0FqLeYTxAwBBCbCUoVjaKbRg3_5KV3ZklWUmOr4IHsHrF-5bZ_erm3GiIKpBED_YsBmR1oMlJR-klAk9PJLJeJ8IcMbjwtfzZHKN3hpNToaAdKPUYoHadLSz7EZtfV9n2dLw15xxRW4yRDQSpbS5FUe3qel-Vh_If8wYw6jnF</recordid><startdate>20220920</startdate><enddate>20220920</enddate><creator>ZHANG LIBO</creator><creator>HE PINGWEI</creator><creator>MA TAO</creator><creator>ZHANG CHANGFENG</creator><creator>PAN HUAYE</creator><creator>LI TENGJI</creator><creator>WANG SHUMIN</creator><creator>ZHANG WEI</creator><scope>EVB</scope></search><sort><creationdate>20220920</creationdate><title>Six-component balance for wind tunnel jet flow experiment and application mode thereof</title><author>ZHANG LIBO ; HE PINGWEI ; MA TAO ; ZHANG CHANGFENG ; PAN HUAYE ; LI TENGJI ; WANG SHUMIN ; ZHANG WEI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN115077853A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</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>ZHANG LIBO</creatorcontrib><creatorcontrib>HE PINGWEI</creatorcontrib><creatorcontrib>MA TAO</creatorcontrib><creatorcontrib>ZHANG CHANGFENG</creatorcontrib><creatorcontrib>PAN HUAYE</creatorcontrib><creatorcontrib>LI TENGJI</creatorcontrib><creatorcontrib>WANG SHUMIN</creatorcontrib><creatorcontrib>ZHANG WEI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ZHANG LIBO</au><au>HE PINGWEI</au><au>MA TAO</au><au>ZHANG CHANGFENG</au><au>PAN HUAYE</au><au>LI TENGJI</au><au>WANG SHUMIN</au><au>ZHANG WEI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Six-component balance for wind tunnel jet flow experiment and application mode thereof</title><date>2022-09-20</date><risdate>2022</risdate><abstract>The invention belongs to the technical field of wind tunnel experiment testing devices, and discloses a six-component balance for a wind tunnel jet flow experiment and an application mode of the six-component balance. The whole six-component balance is of a tubular structure, the front section is a spray pipe connecting flange fixedly connected with a model engine spray pipe, the middle section is a measuring section, the rear section is a gas supply pipeline connecting flange fixedly connected with a gas supply pipeline, a through hole is formed in the central axis of the six-component balance, and the through hole is the gas supply pipeline for jetting medium gas; the measuring section is provided with a resistance element strain cavity, and a resistance strain beam is arranged in the resistance element strain cavity. The application mode comprises a middle resistance element strain cavity six-component balance and a front resistance element strain cavity six-component balance. The six-component balance ado</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN115077853A
source esp@cenet
subjects MEASURING
PHYSICS
TESTING
TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES
TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
title Six-component balance for wind tunnel jet flow experiment and application mode thereof
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-31T00%3A19%3A05IST&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=ZHANG%20LIBO&rft.date=2022-09-20&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN115077853A%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