Composite airfoil assembly and method of manufacturing same
A method of manufacturing an airfoil assembly includes forming an airfoil core including foam to define a pressure side and a suction side extending in a first direction and having a second direction extending between a leading edge and a trailing edge, the second direction being perpendicular to th...
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| creator | KUMAR, SANDEEP SURESH BALARAJU YADAV ABHIJIT JESSEGOWDA KRAY NICHOLAS JOSEPH JONNALAGADDA, GURU, VENKATA, DATTU JAIN, NITESH |
| description | A method of manufacturing an airfoil assembly includes forming an airfoil core including foam to define a pressure side and a suction side extending in a first direction and having a second direction extending between a leading edge and a trailing edge, the second direction being perpendicular to the first direction; and electroforming a metal alloy onto the outer surface of the airfoil core to define an outer airfoil shell.
制造翼型件组件的方法包括形成包括泡沫的翼型件核心，以限定在第一方向上延伸并且具有在前缘和后缘之间在第二方向上延伸的压力侧和吸力侧，第二方向垂直于第一方向；和将金属合金电铸到翼型件核心的外部表面上，以限定外部翼型件壳体。 |
| format | Patent |
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制造翼型件组件的方法包括形成包括泡沫的翼型件核心，以限定在第一方向上延伸并且具有在前缘和后缘之间在第二方向上延伸的压力侧和吸力侧，第二方向垂直于第一方向；和将金属合金电铸到翼型件核心的外部表面上，以限定外部翼型件壳体。</description><language>chi ; eng</language><subject>BLASTING ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT PUMPS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; 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=20240702&DB=EPODOC&CC=CN&NR=118273976A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240702&DB=EPODOC&CC=CN&NR=118273976A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KUMAR, SANDEEP</creatorcontrib><creatorcontrib>SURESH BALARAJU</creatorcontrib><creatorcontrib>YADAV ABHIJIT JESSEGOWDA</creatorcontrib><creatorcontrib>KRAY NICHOLAS JOSEPH</creatorcontrib><creatorcontrib>JONNALAGADDA, GURU, VENKATA, DATTU</creatorcontrib><creatorcontrib>JAIN, NITESH</creatorcontrib><title>Composite airfoil assembly and method of manufacturing same</title><description>A method of manufacturing an airfoil assembly includes forming an airfoil core including foam to define a pressure side and a suction side extending in a first direction and having a second direction extending between a leading edge and a trailing edge, the second direction being perpendicular to the first direction; and electroforming a metal alloy onto the outer surface of the airfoil core to define an outer airfoil shell.
制造翼型件组件的方法包括形成包括泡沫的翼型件核心，以限定在第一方向上延伸并且具有在前缘和后缘之间在第二方向上延伸的压力侧和吸力侧，第二方向垂直于第一方向；和将金属合金电铸到翼型件核心的外部表面上，以限定外部翼型件壳体。</description><subject>BLASTING</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT PUMPS</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLB2zs8tyC_OLElVSMwsSsvPzFFILC5OzU3KqVRIzEtRyE0tychPUchPU8hNzCtNS0wuKS3KzEtXKE7MTeVhYE1LzClO5YXS3AyKbq4hzh66qQX58anFBYnJqXmpJfHOfoaGFkbmxpbmZo7GxKgBAMtzL7Y</recordid><startdate>20240702</startdate><enddate>20240702</enddate><creator>KUMAR, SANDEEP</creator><creator>SURESH BALARAJU</creator><creator>YADAV ABHIJIT JESSEGOWDA</creator><creator>KRAY NICHOLAS JOSEPH</creator><creator>JONNALAGADDA, GURU, VENKATA, DATTU</creator><creator>JAIN, NITESH</creator><scope>EVB</scope></search><sort><creationdate>20240702</creationdate><title>Composite airfoil assembly and method of manufacturing same</title><author>KUMAR, SANDEEP ; SURESH BALARAJU ; YADAV ABHIJIT JESSEGOWDA ; KRAY NICHOLAS JOSEPH ; JONNALAGADDA, GURU, VENKATA, DATTU ; JAIN, NITESH</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN118273976A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2024</creationdate><topic>BLASTING</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT PUMPS</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>KUMAR, SANDEEP</creatorcontrib><creatorcontrib>SURESH BALARAJU</creatorcontrib><creatorcontrib>YADAV ABHIJIT JESSEGOWDA</creatorcontrib><creatorcontrib>KRAY NICHOLAS JOSEPH</creatorcontrib><creatorcontrib>JONNALAGADDA, GURU, VENKATA, DATTU</creatorcontrib><creatorcontrib>JAIN, NITESH</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KUMAR, SANDEEP</au><au>SURESH BALARAJU</au><au>YADAV ABHIJIT JESSEGOWDA</au><au>KRAY NICHOLAS JOSEPH</au><au>JONNALAGADDA, GURU, VENKATA, DATTU</au><au>JAIN, NITESH</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Composite airfoil assembly and method of manufacturing same</title><date>2024-07-02</date><risdate>2024</risdate><abstract>A method of manufacturing an airfoil assembly includes forming an airfoil core including foam to define a pressure side and a suction side extending in a first direction and having a second direction extending between a leading edge and a trailing edge, the second direction being perpendicular to the first direction; and electroforming a metal alloy onto the outer surface of the airfoil core to define an outer airfoil shell.
制造翼型件组件的方法包括形成包括泡沫的翼型件核心，以限定在第一方向上延伸并且具有在前缘和后缘之间在第二方向上延伸的压力侧和吸力侧，第二方向垂直于第一方向；和将金属合金电铸到翼型件核心的外部表面上，以限定外部翼型件壳体。</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN118273976A |
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| subjects | BLASTING HEATING LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS |
| title | Composite airfoil assembly and method of manufacturing same |
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