CAST-IN FILM COOLING HOLE STRUCTURES
A core element (10, 10A-C) of an investment core for use in a casting process used to produce an airfoil (32, 32A-E) includes an investment core body (12, 12A-C), an extension (16, 16A-C) connected to and protruding from the investment core body (12, 12A-C), and a connection portion (14, 14A-C) conn...
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creator | WAGNER, Joel H PAULUS, John DAVIS, Dustin W |
description | A core element (10, 10A-C) of an investment core for use in a casting process used to produce an airfoil (32, 32A-E) includes an investment core body (12, 12A-C), an extension (16, 16A-C) connected to and protruding from the investment core body (12, 12A-C), and a connection portion (14, 14A-C) connected to the investment core body (12, 12A-C) and to the extension (16, 16A-C). The investment core body (12, 12A-C) comprises a ceramic material. A shape of the extension (16, 16A-C) comprises a tube with a centerline axis (CLE) passing through a center of the extension (16, 16A-C). A shape of a cross-section of the extension (16, 16A-C) taken along a plane perpendicular to the extension centerline axis (CLE) comprises an ellipse. The extension (16, 16A-C) is connected to the investment core body (12, 12A-C) by the connection portion (14, 14A-C). |
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The investment core body (12, 12A-C) comprises a ceramic material. A shape of the extension (16, 16A-C) comprises a tube with a centerline axis (CLE) passing through a center of the extension (16, 16A-C). A shape of a cross-section of the extension (16, 16A-C) taken along a plane perpendicular to the extension centerline axis (CLE) comprises an ellipse. The extension (16, 16A-C) is connected to the investment core body (12, 12A-C) by the connection portion (14, 14A-C).</description><language>eng ; fre ; ger</language><subject>BLASTING ; CASTING ; ENGINE PLANTS IN GENERAL ; FOUNDRY MOULDING ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PERFORMING OPERATIONS ; POWDER METALLURGY ; STEAM ENGINES ; TRANSPORTING ; WEAPONS</subject><creationdate>2021</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=20210428&DB=EPODOC&CC=EP&NR=3623072B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210428&DB=EPODOC&CC=EP&NR=3623072B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WAGNER, Joel H</creatorcontrib><creatorcontrib>PAULUS, John</creatorcontrib><creatorcontrib>DAVIS, Dustin W</creatorcontrib><title>CAST-IN FILM COOLING HOLE STRUCTURES</title><description>A core element (10, 10A-C) of an investment core for use in a casting process used to produce an airfoil (32, 32A-E) includes an investment core body (12, 12A-C), an extension (16, 16A-C) connected to and protruding from the investment core body (12, 12A-C), and a connection portion (14, 14A-C) connected to the investment core body (12, 12A-C) and to the extension (16, 16A-C). The investment core body (12, 12A-C) comprises a ceramic material. A shape of the extension (16, 16A-C) comprises a tube with a centerline axis (CLE) passing through a center of the extension (16, 16A-C). A shape of a cross-section of the extension (16, 16A-C) taken along a plane perpendicular to the extension centerline axis (CLE) comprises an ellipse. The extension (16, 16A-C) is connected to the investment core body (12, 12A-C) by the connection portion (14, 14A-C).</description><subject>BLASTING</subject><subject>CASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>FOUNDRY MOULDING</subject><subject>HEATING</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>PERFORMING OPERATIONS</subject><subject>POWDER METALLURGY</subject><subject>STEAM ENGINES</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFBxdgwO0fX0U3Dz9PFVcPb39_H0c1fw8PdxVQgOCQp1DgkNcg3mYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgHGZkbGBuZGTobGRCgBADOKIpE</recordid><startdate>20210428</startdate><enddate>20210428</enddate><creator>WAGNER, Joel H</creator><creator>PAULUS, John</creator><creator>DAVIS, Dustin W</creator><scope>EVB</scope></search><sort><creationdate>20210428</creationdate><title>CAST-IN FILM COOLING HOLE STRUCTURES</title><author>WAGNER, Joel H ; PAULUS, John ; DAVIS, Dustin W</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3623072B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2021</creationdate><topic>BLASTING</topic><topic>CASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>FOUNDRY MOULDING</topic><topic>HEATING</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>PERFORMING OPERATIONS</topic><topic>POWDER METALLURGY</topic><topic>STEAM ENGINES</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>WAGNER, Joel H</creatorcontrib><creatorcontrib>PAULUS, John</creatorcontrib><creatorcontrib>DAVIS, Dustin W</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WAGNER, Joel H</au><au>PAULUS, John</au><au>DAVIS, Dustin W</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>CAST-IN FILM COOLING HOLE STRUCTURES</title><date>2021-04-28</date><risdate>2021</risdate><abstract>A core element (10, 10A-C) of an investment core for use in a casting process used to produce an airfoil (32, 32A-E) includes an investment core body (12, 12A-C), an extension (16, 16A-C) connected to and protruding from the investment core body (12, 12A-C), and a connection portion (14, 14A-C) connected to the investment core body (12, 12A-C) and to the extension (16, 16A-C). The investment core body (12, 12A-C) comprises a ceramic material. A shape of the extension (16, 16A-C) comprises a tube with a centerline axis (CLE) passing through a center of the extension (16, 16A-C). A shape of a cross-section of the extension (16, 16A-C) taken along a plane perpendicular to the extension centerline axis (CLE) comprises an ellipse. The extension (16, 16A-C) is connected to the investment core body (12, 12A-C) by the connection portion (14, 14A-C).</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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subjects | BLASTING CASTING ENGINE PLANTS IN GENERAL FOUNDRY MOULDING HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS POWDER METALLURGY STEAM ENGINES TRANSPORTING WEAPONS |
title | CAST-IN FILM COOLING HOLE STRUCTURES |
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