AIRFOIL ASSEMBLY WITH A TRUNNION AND SPAR
An airfoil assembly (130) and a method of forming the airfoil assembly (130), the airfoil assembly (130) having a trunnion (134), a spar (136), a skin (180), and an insert (172). The trunnion (134) having a flared socket (164) with an open top (170). The spar (136) extending from the flared socket (...
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; fre ; ger |
| 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 | DAVIS, Tod Winton XIE, Ming |
| description | An airfoil assembly (130) and a method of forming the airfoil assembly (130), the airfoil assembly (130) having a trunnion (134), a spar (136), a skin (180), and an insert (172). The trunnion (134) having a flared socket (164) with an open top (170). The spar (136) extending from the flared socket (164) and through the open top (170). The spar (136) having a first end (160) located within the flared socket (164). The skin (180) having a braided or woven fiber. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP4450385A2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP4450385A2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP4450385A23</originalsourceid><addsrcrecordid>eNrjZNB09Axy8_f0UXAMDnb1dfKJVAj3DPFQcFQICQr18_P091Nw9HNRCA5wDOJhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuASYmpgbGFqaORsZEKAEA21Ej3Q</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>AIRFOIL ASSEMBLY WITH A TRUNNION AND SPAR</title><source>esp@cenet</source><creator>DAVIS, Tod Winton ; XIE, Ming</creator><creatorcontrib>DAVIS, Tod Winton ; XIE, Ming</creatorcontrib><description>An airfoil assembly (130) and a method of forming the airfoil assembly (130), the airfoil assembly (130) having a trunnion (134), a spar (136), a skin (180), and an insert (172). The trunnion (134) having a flared socket (164) with an open top (170). The spar (136) extending from the flared socket (164) and through the open top (170). The spar (136) having a first end (160) located within the flared socket (164). The skin (180) having a braided or woven fiber.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; ENGINE PLANTS IN GENERAL ; HEATING ; HELICOPTERS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; NON-POSITIVE DISPLACEMENT PUMPS ; PERFORMING OPERATIONS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; STEAM ENGINES ; TRANSPORTING ; WEAPONS</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=20241023&DB=EPODOC&CC=EP&NR=4450385A2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25544,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20241023&DB=EPODOC&CC=EP&NR=4450385A2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DAVIS, Tod Winton</creatorcontrib><creatorcontrib>XIE, Ming</creatorcontrib><title>AIRFOIL ASSEMBLY WITH A TRUNNION AND SPAR</title><description>An airfoil assembly (130) and a method of forming the airfoil assembly (130), the airfoil assembly (130) having a trunnion (134), a spar (136), a skin (180), and an insert (172). The trunnion (134) having a flared socket (164) with an open top (170). The spar (136) extending from the flared socket (164) and through the open top (170). The spar (136) having a first end (160) located within the flared socket (164). The skin (180) having a braided or woven fiber.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>NON-POSITIVE DISPLACEMENT PUMPS</subject><subject>PERFORMING OPERATIONS</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>STEAM ENGINES</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNB09Axy8_f0UXAMDnb1dfKJVAj3DPFQcFQICQr18_P091Nw9HNRCA5wDOJhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuASYmpgbGFqaORsZEKAEA21Ej3Q</recordid><startdate>20241023</startdate><enddate>20241023</enddate><creator>DAVIS, Tod Winton</creator><creator>XIE, Ming</creator><scope>EVB</scope></search><sort><creationdate>20241023</creationdate><title>AIRFOIL ASSEMBLY WITH A TRUNNION AND SPAR</title><author>DAVIS, Tod Winton ; XIE, Ming</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4450385A23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2024</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>NON-POSITIVE DISPLACEMENT PUMPS</topic><topic>PERFORMING OPERATIONS</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>STEAM ENGINES</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>DAVIS, Tod Winton</creatorcontrib><creatorcontrib>XIE, Ming</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>DAVIS, Tod Winton</au><au>XIE, Ming</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRFOIL ASSEMBLY WITH A TRUNNION AND SPAR</title><date>2024-10-23</date><risdate>2024</risdate><abstract>An airfoil assembly (130) and a method of forming the airfoil assembly (130), the airfoil assembly (130) having a trunnion (134), a spar (136), a skin (180), and an insert (172). The trunnion (134) having a flared socket (164) with an open top (170). The spar (136) extending from the flared socket (164) and through the open top (170). The spar (136) having a first end (160) located within the flared socket (164). The skin (180) having a braided or woven fiber.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; fre ; ger |
| recordid | cdi_epo_espacenet_EP4450385A2 |
| source | esp@cenet |
| subjects | AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINE PLANTS IN GENERAL HEATING HELICOPTERS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS PERFORMING OPERATIONS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES TRANSPORTING WEAPONS |
| title | AIRFOIL ASSEMBLY WITH A TRUNNION AND SPAR |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-27T15%3A25%3A04IST&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=DAVIS,%20Tod%20Winton&rft.date=2024-10-23&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP4450385A2%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 |