Satellite support type structure design method based on topological optimization and dot matrix filling
The invention discloses a satellite support type structure design method based on topological optimization and dot matrix filling, and belongs to the field of satellite effective load supporting structure design. Firstly, an initial model is established, and finite element mesh generation is carried...
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 | GENG DONGLING BU YUFENG YAN JUN DU HONGZE WANG FUHAO ZHAO CHUNYU XU QI JIANG LIZHE |
| description | The invention discloses a satellite support type structure design method based on topological optimization and dot matrix filling, and belongs to the field of satellite effective load supporting structure design. Firstly, an initial model is established, and finite element mesh generation is carried out on the initial model to obtain a finite element model; secondly, dividing the finite element model into a designable domain and a non-designable domain, and performing macroscopic topological optimization design on the designable domain to obtain a topological optimization configuration; thirdly, geometric repair is conducted on the topological optimization configuration, fuzzy boundaries in the topological configuration are reduced, and manufacturability of the designed support is improved. And finally, performing mesoscopic lattice filling on the geometric repair configuration of the satellite support. On the basis that the high stability of the support type structure is guaranteed, the structural mass can b |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN116432483A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN116432483A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN116432483A3</originalsourceid><addsrcrecordid>eNqNjDEKwkAQRdNYiHqH8QAWMUFsJShWNtqHMTvZDGx2ht0JqKc3hQew-jze4y8Lf0ejENgI8qQqycDeOoOlqbMpETjK7COMZIM4eGImBxLBRCWI5w4DiBqP_EHjWWB04MRgREv8gp7n9-jXxaLHkGnz21WxvZwfzXVHKi1lxY4iWdvcyvJQV_v6WJ2qf5ovU01A9A</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Satellite support type structure design method based on topological optimization and dot matrix filling</title><source>esp@cenet</source><creator>GENG DONGLING ; BU YUFENG ; YAN JUN ; DU HONGZE ; WANG FUHAO ; ZHAO CHUNYU ; XU QI ; JIANG LIZHE</creator><creatorcontrib>GENG DONGLING ; BU YUFENG ; YAN JUN ; DU HONGZE ; WANG FUHAO ; ZHAO CHUNYU ; XU QI ; JIANG LIZHE</creatorcontrib><description>The invention discloses a satellite support type structure design method based on topological optimization and dot matrix filling, and belongs to the field of satellite effective load supporting structure design. Firstly, an initial model is established, and finite element mesh generation is carried out on the initial model to obtain a finite element model; secondly, dividing the finite element model into a designable domain and a non-designable domain, and performing macroscopic topological optimization design on the designable domain to obtain a topological optimization configuration; thirdly, geometric repair is conducted on the topological optimization configuration, fuzzy boundaries in the topological configuration are reduced, and manufacturability of the designed support is improved. And finally, performing mesoscopic lattice filling on the geometric repair configuration of the satellite support. On the basis that the high stability of the support type structure is guaranteed, the structural mass can b</description><language>chi ; eng</language><subject>CALCULATING ; COMPUTING ; COUNTING ; ELECTRIC DIGITAL DATA PROCESSING ; PHYSICS</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=20230714&DB=EPODOC&CC=CN&NR=116432483A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,309,781,886,25566,76549</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230714&DB=EPODOC&CC=CN&NR=116432483A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GENG DONGLING</creatorcontrib><creatorcontrib>BU YUFENG</creatorcontrib><creatorcontrib>YAN JUN</creatorcontrib><creatorcontrib>DU HONGZE</creatorcontrib><creatorcontrib>WANG FUHAO</creatorcontrib><creatorcontrib>ZHAO CHUNYU</creatorcontrib><creatorcontrib>XU QI</creatorcontrib><creatorcontrib>JIANG LIZHE</creatorcontrib><title>Satellite support type structure design method based on topological optimization and dot matrix filling</title><description>The invention discloses a satellite support type structure design method based on topological optimization and dot matrix filling, and belongs to the field of satellite effective load supporting structure design. Firstly, an initial model is established, and finite element mesh generation is carried out on the initial model to obtain a finite element model; secondly, dividing the finite element model into a designable domain and a non-designable domain, and performing macroscopic topological optimization design on the designable domain to obtain a topological optimization configuration; thirdly, geometric repair is conducted on the topological optimization configuration, fuzzy boundaries in the topological configuration are reduced, and manufacturability of the designed support is improved. And finally, performing mesoscopic lattice filling on the geometric repair configuration of the satellite support. On the basis that the high stability of the support type structure is guaranteed, the structural mass can b</description><subject>CALCULATING</subject><subject>COMPUTING</subject><subject>COUNTING</subject><subject>ELECTRIC DIGITAL DATA PROCESSING</subject><subject>PHYSICS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjDEKwkAQRdNYiHqH8QAWMUFsJShWNtqHMTvZDGx2ht0JqKc3hQew-jze4y8Lf0ejENgI8qQqycDeOoOlqbMpETjK7COMZIM4eGImBxLBRCWI5w4DiBqP_EHjWWB04MRgREv8gp7n9-jXxaLHkGnz21WxvZwfzXVHKi1lxY4iWdvcyvJQV_v6WJ2qf5ovU01A9A</recordid><startdate>20230714</startdate><enddate>20230714</enddate><creator>GENG DONGLING</creator><creator>BU YUFENG</creator><creator>YAN JUN</creator><creator>DU HONGZE</creator><creator>WANG FUHAO</creator><creator>ZHAO CHUNYU</creator><creator>XU QI</creator><creator>JIANG LIZHE</creator><scope>EVB</scope></search><sort><creationdate>20230714</creationdate><title>Satellite support type structure design method based on topological optimization and dot matrix filling</title><author>GENG DONGLING ; BU YUFENG ; YAN JUN ; DU HONGZE ; WANG FUHAO ; ZHAO CHUNYU ; XU QI ; JIANG LIZHE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN116432483A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</creationdate><topic>CALCULATING</topic><topic>COMPUTING</topic><topic>COUNTING</topic><topic>ELECTRIC DIGITAL DATA PROCESSING</topic><topic>PHYSICS</topic><toplevel>online_resources</toplevel><creatorcontrib>GENG DONGLING</creatorcontrib><creatorcontrib>BU YUFENG</creatorcontrib><creatorcontrib>YAN JUN</creatorcontrib><creatorcontrib>DU HONGZE</creatorcontrib><creatorcontrib>WANG FUHAO</creatorcontrib><creatorcontrib>ZHAO CHUNYU</creatorcontrib><creatorcontrib>XU QI</creatorcontrib><creatorcontrib>JIANG LIZHE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GENG DONGLING</au><au>BU YUFENG</au><au>YAN JUN</au><au>DU HONGZE</au><au>WANG FUHAO</au><au>ZHAO CHUNYU</au><au>XU QI</au><au>JIANG LIZHE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Satellite support type structure design method based on topological optimization and dot matrix filling</title><date>2023-07-14</date><risdate>2023</risdate><abstract>The invention discloses a satellite support type structure design method based on topological optimization and dot matrix filling, and belongs to the field of satellite effective load supporting structure design. Firstly, an initial model is established, and finite element mesh generation is carried out on the initial model to obtain a finite element model; secondly, dividing the finite element model into a designable domain and a non-designable domain, and performing macroscopic topological optimization design on the designable domain to obtain a topological optimization configuration; thirdly, geometric repair is conducted on the topological optimization configuration, fuzzy boundaries in the topological configuration are reduced, and manufacturability of the designed support is improved. And finally, performing mesoscopic lattice filling on the geometric repair configuration of the satellite support. On the basis that the high stability of the support type structure is guaranteed, the structural mass can b</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN116432483A |
| source | esp@cenet |
| subjects | CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING PHYSICS |
| title | Satellite support type structure design method based on topological optimization and dot matrix filling |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-18T00%3A46%3A35IST&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=GENG%20DONGLING&rft.date=2023-07-14&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN116432483A%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 |