Aero-engine basic element construction and application method and basic element management device
The invention provides an aero-engine basic element construction and application method. The aero-engine basic element construction and application method comprises the steps that S10, a basic element range is determined; step S20, basic element classification is determined, wherein the basic elemen...
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 | NA LAN CUI WEIWEI NING HUAISONG WANG XIANGPING LIU XIAOSONG GU YANPING SUN XIAOHUAN XU KAICHI HE WEI ZHANG DEZHI ZHENG NING HAN QIUBING YANG LIN WANG FENG LIU HAINIAN |
| description | The invention provides an aero-engine basic element construction and application method. The aero-engine basic element construction and application method comprises the steps that S10, a basic element range is determined; step S20, basic element classification is determined, wherein the basic element classification comprises a specification/standard, a guide book, a template, a checklist, a software tool and an engineering database; s30, basic element composition elements are determined, and design requirements/criteria, a modeling method, a grid division method, a model analysis method, a calculation method and result output are included; step S40, establishing a basic element construction method based on a process; s50, forming an element template according to the basic element development plan and the basic elements, and completing basic element file development according to related regulations; step S60, establishing a basic element multi-dimensional access evaluation method based on technology maturity; |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN118627731A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN118627731A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN118627731A3</originalsourceid><addsrcrecordid>eNqNizEOwjAQBN1QIOAP5gEpTCRCG0WgVFT00XFegiX7bMWG90cKNHRUu7OaXStqMcUKMjqBvlN2rOERIEVzlFymFxcXRZNYTSl5x7RwQHlGu8y_r0BC46davB1jq1YP8hm7b27U_nK-dX2FFAfkRAxBGbqrMafjoWlq09b_ODMg3z3l</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Aero-engine basic element construction and application method and basic element management device</title><source>esp@cenet</source><creator>NA LAN ; CUI WEIWEI ; NING HUAISONG ; WANG XIANGPING ; LIU XIAOSONG ; GU YANPING ; SUN XIAOHUAN ; XU KAICHI ; HE WEI ; ZHANG DEZHI ; ZHENG NING ; HAN QIUBING ; YANG LIN ; WANG FENG ; LIU HAINIAN</creator><creatorcontrib>NA LAN ; CUI WEIWEI ; NING HUAISONG ; WANG XIANGPING ; LIU XIAOSONG ; GU YANPING ; SUN XIAOHUAN ; XU KAICHI ; HE WEI ; ZHANG DEZHI ; ZHENG NING ; HAN QIUBING ; YANG LIN ; WANG FENG ; LIU HAINIAN</creatorcontrib><description>The invention provides an aero-engine basic element construction and application method. The aero-engine basic element construction and application method comprises the steps that S10, a basic element range is determined; step S20, basic element classification is determined, wherein the basic element classification comprises a specification/standard, a guide book, a template, a checklist, a software tool and an engineering database; s30, basic element composition elements are determined, and design requirements/criteria, a modeling method, a grid division method, a model analysis method, a calculation method and result output are included; step S40, establishing a basic element construction method based on a process; s50, forming an element template according to the basic element development plan and the basic elements, and completing basic element file development according to related regulations; step S60, establishing a basic element multi-dimensional access evaluation method based on technology maturity;</description><language>chi ; eng</language><subject>CALCULATING ; COMPUTING ; COUNTING ; DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FORADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORYOR FORECASTING PURPOSES ; PHYSICS ; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE,COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTINGPURPOSES, NOT OTHERWISE PROVIDED FOR</subject><creationdate>2024</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=20240910&DB=EPODOC&CC=CN&NR=118627731A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240910&DB=EPODOC&CC=CN&NR=118627731A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>NA LAN</creatorcontrib><creatorcontrib>CUI WEIWEI</creatorcontrib><creatorcontrib>NING HUAISONG</creatorcontrib><creatorcontrib>WANG XIANGPING</creatorcontrib><creatorcontrib>LIU XIAOSONG</creatorcontrib><creatorcontrib>GU YANPING</creatorcontrib><creatorcontrib>SUN XIAOHUAN</creatorcontrib><creatorcontrib>XU KAICHI</creatorcontrib><creatorcontrib>HE WEI</creatorcontrib><creatorcontrib>ZHANG DEZHI</creatorcontrib><creatorcontrib>ZHENG NING</creatorcontrib><creatorcontrib>HAN QIUBING</creatorcontrib><creatorcontrib>YANG LIN</creatorcontrib><creatorcontrib>WANG FENG</creatorcontrib><creatorcontrib>LIU HAINIAN</creatorcontrib><title>Aero-engine basic element construction and application method and basic element management device</title><description>The invention provides an aero-engine basic element construction and application method. The aero-engine basic element construction and application method comprises the steps that S10, a basic element range is determined; step S20, basic element classification is determined, wherein the basic element classification comprises a specification/standard, a guide book, a template, a checklist, a software tool and an engineering database; s30, basic element composition elements are determined, and design requirements/criteria, a modeling method, a grid division method, a model analysis method, a calculation method and result output are included; step S40, establishing a basic element construction method based on a process; s50, forming an element template according to the basic element development plan and the basic elements, and completing basic element file development according to related regulations; step S60, establishing a basic element multi-dimensional access evaluation method based on technology maturity;</description><subject>CALCULATING</subject><subject>COMPUTING</subject><subject>COUNTING</subject><subject>DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FORADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORYOR FORECASTING PURPOSES</subject><subject>PHYSICS</subject><subject>SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE,COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTINGPURPOSES, NOT OTHERWISE PROVIDED FOR</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNizEOwjAQBN1QIOAP5gEpTCRCG0WgVFT00XFegiX7bMWG90cKNHRUu7OaXStqMcUKMjqBvlN2rOERIEVzlFymFxcXRZNYTSl5x7RwQHlGu8y_r0BC46davB1jq1YP8hm7b27U_nK-dX2FFAfkRAxBGbqrMafjoWlq09b_ODMg3z3l</recordid><startdate>20240910</startdate><enddate>20240910</enddate><creator>NA LAN</creator><creator>CUI WEIWEI</creator><creator>NING HUAISONG</creator><creator>WANG XIANGPING</creator><creator>LIU XIAOSONG</creator><creator>GU YANPING</creator><creator>SUN XIAOHUAN</creator><creator>XU KAICHI</creator><creator>HE WEI</creator><creator>ZHANG DEZHI</creator><creator>ZHENG NING</creator><creator>HAN QIUBING</creator><creator>YANG LIN</creator><creator>WANG FENG</creator><creator>LIU HAINIAN</creator><scope>EVB</scope></search><sort><creationdate>20240910</creationdate><title>Aero-engine basic element construction and application method and basic element management device</title><author>NA LAN ; CUI WEIWEI ; NING HUAISONG ; WANG XIANGPING ; LIU XIAOSONG ; GU YANPING ; SUN XIAOHUAN ; XU KAICHI ; HE WEI ; ZHANG DEZHI ; ZHENG NING ; HAN QIUBING ; YANG LIN ; WANG FENG ; LIU HAINIAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN118627731A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2024</creationdate><topic>CALCULATING</topic><topic>COMPUTING</topic><topic>COUNTING</topic><topic>DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FORADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORYOR FORECASTING PURPOSES</topic><topic>PHYSICS</topic><topic>SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE,COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTINGPURPOSES, NOT OTHERWISE PROVIDED FOR</topic><toplevel>online_resources</toplevel><creatorcontrib>NA LAN</creatorcontrib><creatorcontrib>CUI WEIWEI</creatorcontrib><creatorcontrib>NING HUAISONG</creatorcontrib><creatorcontrib>WANG XIANGPING</creatorcontrib><creatorcontrib>LIU XIAOSONG</creatorcontrib><creatorcontrib>GU YANPING</creatorcontrib><creatorcontrib>SUN XIAOHUAN</creatorcontrib><creatorcontrib>XU KAICHI</creatorcontrib><creatorcontrib>HE WEI</creatorcontrib><creatorcontrib>ZHANG DEZHI</creatorcontrib><creatorcontrib>ZHENG NING</creatorcontrib><creatorcontrib>HAN QIUBING</creatorcontrib><creatorcontrib>YANG LIN</creatorcontrib><creatorcontrib>WANG FENG</creatorcontrib><creatorcontrib>LIU HAINIAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>NA LAN</au><au>CUI WEIWEI</au><au>NING HUAISONG</au><au>WANG XIANGPING</au><au>LIU XIAOSONG</au><au>GU YANPING</au><au>SUN XIAOHUAN</au><au>XU KAICHI</au><au>HE WEI</au><au>ZHANG DEZHI</au><au>ZHENG NING</au><au>HAN QIUBING</au><au>YANG LIN</au><au>WANG FENG</au><au>LIU HAINIAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aero-engine basic element construction and application method and basic element management device</title><date>2024-09-10</date><risdate>2024</risdate><abstract>The invention provides an aero-engine basic element construction and application method. The aero-engine basic element construction and application method comprises the steps that S10, a basic element range is determined; step S20, basic element classification is determined, wherein the basic element classification comprises a specification/standard, a guide book, a template, a checklist, a software tool and an engineering database; s30, basic element composition elements are determined, and design requirements/criteria, a modeling method, a grid division method, a model analysis method, a calculation method and result output are included; step S40, establishing a basic element construction method based on a process; s50, forming an element template according to the basic element development plan and the basic elements, and completing basic element file development according to related regulations; step S60, establishing a basic element multi-dimensional access evaluation method based on technology maturity;</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN118627731A |
| source | esp@cenet |
| subjects | CALCULATING COMPUTING COUNTING DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FORADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORYOR FORECASTING PURPOSES PHYSICS SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE,COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTINGPURPOSES, NOT OTHERWISE PROVIDED FOR |
| title | Aero-engine basic element construction and application method and basic element management device |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-09T22%3A22%3A03IST&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=NA%20LAN&rft.date=2024-09-10&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN118627731A%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 |