On-orbit assembly-oriented shear hinge type universal module based on edge lock butt joint

The invention discloses an on-orbit assembly-oriented shear-hinge type universal module based on corner lock butt joint, and belongs to the field of spacecraft structure design, the module comprises a corner triangular claw butt joint mechanism I, a corner locking mechanism II and a shear-hinge type...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: SUN HAO, ZHANG SIJI, SUN WEIFENG, WEN HAO, ZHANG WEI
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 SUN HAO
ZHANG SIJI
SUN WEIFENG
WEN HAO
ZHANG WEI
description The invention discloses an on-orbit assembly-oriented shear-hinge type universal module based on corner lock butt joint, and belongs to the field of spacecraft structure design, the module comprises a corner triangular claw butt joint mechanism I, a corner locking mechanism II and a shear-hinge type rotating rod mechanism III, the butt joint mechanism I contains a corner triangular claw for butt joint locking; the angular point locking mechanism II comprises a pre-tightening spring, and a groove is used for module self-locking; under limited conditions, a grabbing device can be conveniently assisted to quickly complete module assembly, meanwhile, the structure has the characteristics of standardization and modularization, interfaces are convenient to replace, on-orbit assembly of space structures of different specifications is met, therefore, the requirements of different aerospace tasks are met, the purposes of flexible function configuration and flexible task adaptation are achieved, and meanwhile the modul
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN114802815A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN114802815A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN114802815A3</originalsourceid><addsrcrecordid>eNqNyj0KwkAQhuE0FqLeYTxAwPgDaSUoVtpY2YTd5ItZ3cwumYmQ25vCA1i9vPDMk8eN09Bbp2RE0Fk_TuvAipqkhempdfwE6RhBA7sPejGeulAPHmSNTC4woZ6MD9Wb7KBKr-BYl8msMV6w-nWRrM-ne3FJEUMJiaYCQ8vimmX7fLPNs8Nx94_5AiHfOuo</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>On-orbit assembly-oriented shear hinge type universal module based on edge lock butt joint</title><source>esp@cenet</source><creator>SUN HAO ; ZHANG SIJI ; SUN WEIFENG ; WEN HAO ; ZHANG WEI</creator><creatorcontrib>SUN HAO ; ZHANG SIJI ; SUN WEIFENG ; WEN HAO ; ZHANG WEI</creatorcontrib><description>The invention discloses an on-orbit assembly-oriented shear-hinge type universal module based on corner lock butt joint, and belongs to the field of spacecraft structure design, the module comprises a corner triangular claw butt joint mechanism I, a corner locking mechanism II and a shear-hinge type rotating rod mechanism III, the butt joint mechanism I contains a corner triangular claw for butt joint locking; the angular point locking mechanism II comprises a pre-tightening spring, and a groove is used for module self-locking; under limited conditions, a grabbing device can be conveniently assisted to quickly complete module assembly, meanwhile, the structure has the characteristics of standardization and modularization, interfaces are convenient to replace, on-orbit assembly of space structures of different specifications is met, therefore, the requirements of different aerospace tasks are met, the purposes of flexible function configuration and flexible task adaptation are achieved, and meanwhile the modul</description><language>chi ; eng</language><subject>AIRCRAFT ; AVIATION ; COSMONAUTICS ; PERFORMING OPERATIONS ; TRANSPORTING ; VEHICLES OR EQUIPMENT THEREFOR</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=20220729&amp;DB=EPODOC&amp;CC=CN&amp;NR=114802815A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20220729&amp;DB=EPODOC&amp;CC=CN&amp;NR=114802815A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SUN HAO</creatorcontrib><creatorcontrib>ZHANG SIJI</creatorcontrib><creatorcontrib>SUN WEIFENG</creatorcontrib><creatorcontrib>WEN HAO</creatorcontrib><creatorcontrib>ZHANG WEI</creatorcontrib><title>On-orbit assembly-oriented shear hinge type universal module based on edge lock butt joint</title><description>The invention discloses an on-orbit assembly-oriented shear-hinge type universal module based on corner lock butt joint, and belongs to the field of spacecraft structure design, the module comprises a corner triangular claw butt joint mechanism I, a corner locking mechanism II and a shear-hinge type rotating rod mechanism III, the butt joint mechanism I contains a corner triangular claw for butt joint locking; the angular point locking mechanism II comprises a pre-tightening spring, and a groove is used for module self-locking; under limited conditions, a grabbing device can be conveniently assisted to quickly complete module assembly, meanwhile, the structure has the characteristics of standardization and modularization, interfaces are convenient to replace, on-orbit assembly of space structures of different specifications is met, therefore, the requirements of different aerospace tasks are met, the purposes of flexible function configuration and flexible task adaptation are achieved, and meanwhile the modul</description><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>VEHICLES OR EQUIPMENT THEREFOR</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyj0KwkAQhuE0FqLeYTxAwPgDaSUoVtpY2YTd5ItZ3cwumYmQ25vCA1i9vPDMk8eN09Bbp2RE0Fk_TuvAipqkhempdfwE6RhBA7sPejGeulAPHmSNTC4woZ6MD9Wb7KBKr-BYl8msMV6w-nWRrM-ne3FJEUMJiaYCQ8vimmX7fLPNs8Nx94_5AiHfOuo</recordid><startdate>20220729</startdate><enddate>20220729</enddate><creator>SUN HAO</creator><creator>ZHANG SIJI</creator><creator>SUN WEIFENG</creator><creator>WEN HAO</creator><creator>ZHANG WEI</creator><scope>EVB</scope></search><sort><creationdate>20220729</creationdate><title>On-orbit assembly-oriented shear hinge type universal module based on edge lock butt joint</title><author>SUN HAO ; ZHANG SIJI ; SUN WEIFENG ; WEN HAO ; ZHANG WEI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN114802815A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</creationdate><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>VEHICLES OR EQUIPMENT THEREFOR</topic><toplevel>online_resources</toplevel><creatorcontrib>SUN HAO</creatorcontrib><creatorcontrib>ZHANG SIJI</creatorcontrib><creatorcontrib>SUN WEIFENG</creatorcontrib><creatorcontrib>WEN HAO</creatorcontrib><creatorcontrib>ZHANG WEI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SUN HAO</au><au>ZHANG SIJI</au><au>SUN WEIFENG</au><au>WEN HAO</au><au>ZHANG WEI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>On-orbit assembly-oriented shear hinge type universal module based on edge lock butt joint</title><date>2022-07-29</date><risdate>2022</risdate><abstract>The invention discloses an on-orbit assembly-oriented shear-hinge type universal module based on corner lock butt joint, and belongs to the field of spacecraft structure design, the module comprises a corner triangular claw butt joint mechanism I, a corner locking mechanism II and a shear-hinge type rotating rod mechanism III, the butt joint mechanism I contains a corner triangular claw for butt joint locking; the angular point locking mechanism II comprises a pre-tightening spring, and a groove is used for module self-locking; under limited conditions, a grabbing device can be conveniently assisted to quickly complete module assembly, meanwhile, the structure has the characteristics of standardization and modularization, interfaces are convenient to replace, on-orbit assembly of space structures of different specifications is met, therefore, the requirements of different aerospace tasks are met, the purposes of flexible function configuration and flexible task adaptation are achieved, and meanwhile the modul</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN114802815A
source esp@cenet
subjects AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
title On-orbit assembly-oriented shear hinge type universal module based on edge lock butt joint
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-24T14%3A56%3A14IST&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=SUN%20HAO&rft.date=2022-07-29&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN114802815A%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