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...
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 | 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&date=20220729&DB=EPODOC&CC=CN&NR=114802815A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220729&DB=EPODOC&CC=CN&NR=114802815A$$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 |