WIRE SCREEN PARTICLE FILTER FOR TURBOMACHINE AIRFOIL
A filter for an airfoil of a vane of a turbomachine is disclosed. The filter includes a mounting member for mounting to an endwall of the vane. The mounting member has a first flow exit opening defined therethrough for fluid communication with a cooling circuit of the airfoil. A screen frame is coup...
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creator | ROBERTS, JR., Frederic Woodrow KOTAY, Kathen Thomas |
description | A filter for an airfoil of a vane of a turbomachine is disclosed. The filter includes a mounting member for mounting to an endwall of the vane. The mounting member has a first flow exit opening defined therethrough for fluid communication with a cooling circuit of the airfoil. A screen frame is coupled to the mounting member to support a wire screen around the first flow exit opening, and a first wire screen is positioned over the screen frame. The screen frame has an exterior shape supporting the wire screen in a manner incapable of having a horizontal surface regardless of a circumferential position of the airfoil around an axis of the turbomachine. A related turbine vane and turbine system are also provided. |
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The filter includes a mounting member for mounting to an endwall of the vane. The mounting member has a first flow exit opening defined therethrough for fluid communication with a cooling circuit of the airfoil. A screen frame is coupled to the mounting member to support a wire screen around the first flow exit opening, and a first wire screen is positioned over the screen frame. The screen frame has an exterior shape supporting the wire screen in a manner incapable of having a horizontal surface regardless of a circumferential position of the airfoil around an axis of the turbomachine. A related turbine vane and turbine system are also provided.</description><language>eng</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</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=20230622&DB=EPODOC&CC=US&NR=2023193765A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230622&DB=EPODOC&CC=US&NR=2023193765A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ROBERTS, JR., Frederic Woodrow</creatorcontrib><creatorcontrib>KOTAY, Kathen Thomas</creatorcontrib><title>WIRE SCREEN PARTICLE FILTER FOR TURBOMACHINE AIRFOIL</title><description>A filter for an airfoil of a vane of a turbomachine is disclosed. The filter includes a mounting member for mounting to an endwall of the vane. The mounting member has a first flow exit opening defined therethrough for fluid communication with a cooling circuit of the airfoil. A screen frame is coupled to the mounting member to support a wire screen around the first flow exit opening, and a first wire screen is positioned over the screen frame. The screen frame has an exterior shape supporting the wire screen in a manner incapable of having a horizontal surface regardless of a circumferential position of the airfoil around an axis of the turbomachine. A related turbine vane and turbine system are also provided.</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</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>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAJ9wxyVQh2DnJ19VMIcAwK8XT2cVVw8_QJcQ1ScPMPUggJDXLy93V09vD0c1Vw9Axy8_f04WFgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8aHBRgZGxoaWxuZmpo6GxsSpAgBkNyha</recordid><startdate>20230622</startdate><enddate>20230622</enddate><creator>ROBERTS, JR., Frederic Woodrow</creator><creator>KOTAY, Kathen Thomas</creator><scope>EVB</scope></search><sort><creationdate>20230622</creationdate><title>WIRE SCREEN PARTICLE FILTER FOR TURBOMACHINE AIRFOIL</title><author>ROBERTS, JR., Frederic Woodrow ; KOTAY, Kathen Thomas</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2023193765A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2023</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</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>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>ROBERTS, JR., Frederic Woodrow</creatorcontrib><creatorcontrib>KOTAY, Kathen Thomas</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ROBERTS, JR., Frederic Woodrow</au><au>KOTAY, Kathen Thomas</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>WIRE SCREEN PARTICLE FILTER FOR TURBOMACHINE AIRFOIL</title><date>2023-06-22</date><risdate>2023</risdate><abstract>A filter for an airfoil of a vane of a turbomachine is disclosed. The filter includes a mounting member for mounting to an endwall of the vane. The mounting member has a first flow exit opening defined therethrough for fluid communication with a cooling circuit of the airfoil. A screen frame is coupled to the mounting member to support a wire screen around the first flow exit opening, and a first wire screen is positioned over the screen frame. The screen frame has an exterior shape supporting the wire screen in a manner incapable of having a horizontal surface regardless of a circumferential position of the airfoil around an axis of the turbomachine. A related turbine vane and turbine system are also provided.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
title | WIRE SCREEN PARTICLE FILTER FOR TURBOMACHINE AIRFOIL |
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