TURBINE ROTOR BLADE
A turbine rotor blade (120) is additively manufactured and includes an airfoil body (122) with a radially extending chamber (134) for receiving a coolant (236) flow. A platform (150) (extends laterally outward relative to the airfoil body (122) and terminates at at least one slash face (230, 230PS,...
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| creator | SNIDER, Zachary John |
| description | A turbine rotor blade (120) is additively manufactured and includes an airfoil body (122) with a radially extending chamber (134) for receiving a coolant (236) flow. A platform (150) (extends laterally outward relative to the airfoil body (122) and terminates at at least one slash face (230, 230PS, 230SS). A cooling circuit (234) is within the platform (150) and is in fluid communication with a source of the coolant (236) flow. Cooling passage(s) (172, 240) are in the platform (150) and in fluid communication with the cooling circuit (234). The cooling passage(s) (172, 240) extend in a non-linear configuration from the cooling circuit (234) to exit through the at least one slash face (230, 230PS, 230SS) of the platform (150), providing improved cooling compared to linear cooling passages (172, 240). |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP4234130A3</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP4234130A3</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP4234130A33</originalsourceid><addsrcrecordid>eNrjZBAOCQ1y8vRzVQjyD_EPUnDycXRx5WFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BJkbGJobGBo7GxkQoAQAcZx3P</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>TURBINE ROTOR BLADE</title><source>esp@cenet</source><creator>SNIDER, Zachary John</creator><creatorcontrib>SNIDER, Zachary John</creatorcontrib><description>A turbine rotor blade (120) is additively manufactured and includes an airfoil body (122) with a radially extending chamber (134) for receiving a coolant (236) flow. A platform (150) (extends laterally outward relative to the airfoil body (122) and terminates at at least one slash face (230, 230PS, 230SS). A cooling circuit (234) is within the platform (150) and is in fluid communication with a source of the coolant (236) flow. Cooling passage(s) (172, 240) are in the platform (150) and in fluid communication with the cooling circuit (234). The cooling passage(s) (172, 240) extend in a non-linear configuration from the cooling circuit (234) to exit through the at least one slash face (230, 230PS, 230SS) of the platform (150), providing improved cooling compared to linear cooling passages (172, 240).</description><language>eng ; fre ; ger</language><subject>BLASTING ; CASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MAKING METALLIC POWDER ; MANUFACTURE OF ARTICLES FROM METALLIC POWDER ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PERFORMING OPERATIONS ; POWDER METALLURGY ; STEAM ENGINES ; TRANSPORTING ; WEAPONS ; WORKING METALLIC POWDER</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=20230906&DB=EPODOC&CC=EP&NR=4234130A3$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230906&DB=EPODOC&CC=EP&NR=4234130A3$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SNIDER, Zachary John</creatorcontrib><title>TURBINE ROTOR BLADE</title><description>A turbine rotor blade (120) is additively manufactured and includes an airfoil body (122) with a radially extending chamber (134) for receiving a coolant (236) flow. A platform (150) (extends laterally outward relative to the airfoil body (122) and terminates at at least one slash face (230, 230PS, 230SS). A cooling circuit (234) is within the platform (150) and is in fluid communication with a source of the coolant (236) flow. Cooling passage(s) (172, 240) are in the platform (150) and in fluid communication with the cooling circuit (234). The cooling passage(s) (172, 240) extend in a non-linear configuration from the cooling circuit (234) to exit through the at least one slash face (230, 230PS, 230SS) of the platform (150), providing improved cooling compared to linear cooling passages (172, 240).</description><subject>BLASTING</subject><subject>CASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MAKING METALLIC POWDER</subject><subject>MANUFACTURE OF ARTICLES FROM METALLIC POWDER</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><subject>WORKING METALLIC POWDER</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBAOCQ1y8vRzVQjyD_EPUnDycXRx5WFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BJkbGJobGBo7GxkQoAQAcZx3P</recordid><startdate>20230906</startdate><enddate>20230906</enddate><creator>SNIDER, Zachary John</creator><scope>EVB</scope></search><sort><creationdate>20230906</creationdate><title>TURBINE ROTOR BLADE</title><author>SNIDER, Zachary John</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4234130A33</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2023</creationdate><topic>BLASTING</topic><topic>CASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MAKING METALLIC POWDER</topic><topic>MANUFACTURE OF ARTICLES FROM METALLIC POWDER</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><topic>WORKING METALLIC POWDER</topic><toplevel>online_resources</toplevel><creatorcontrib>SNIDER, Zachary John</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SNIDER, Zachary John</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBINE ROTOR BLADE</title><date>2023-09-06</date><risdate>2023</risdate><abstract>A turbine rotor blade (120) is additively manufactured and includes an airfoil body (122) with a radially extending chamber (134) for receiving a coolant (236) flow. A platform (150) (extends laterally outward relative to the airfoil body (122) and terminates at at least one slash face (230, 230PS, 230SS). A cooling circuit (234) is within the platform (150) and is in fluid communication with a source of the coolant (236) flow. Cooling passage(s) (172, 240) are in the platform (150) and in fluid communication with the cooling circuit (234). The cooling passage(s) (172, 240) extend in a non-linear configuration from the cooling circuit (234) to exit through the at least one slash face (230, 230PS, 230SS) of the platform (150), providing improved cooling compared to linear cooling passages (172, 240).</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| source | esp@cenet |
| subjects | BLASTING CASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MAKING METALLIC POWDER MANUFACTURE OF ARTICLES FROM METALLIC POWDER MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS POWDER METALLURGY STEAM ENGINES TRANSPORTING WEAPONS WORKING METALLIC POWDER |
| title | TURBINE ROTOR BLADE |
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