COOLING CIRCUIT FOR A MULTI-WALL BLADE
A turbine blade cooling system according to an embodiment includes: a first arcuate turn for redirecting a first flow of gas flowing through a first channel of a turbine blade (6) into a central plenum (44) of the turbine blade (6); and a second arcuate turn (70) for redirecting a second flow of gas...
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creator | WEBER, David Wayne WILLETT, Fred Thomas Jr |
description | A turbine blade cooling system according to an embodiment includes: a first arcuate turn for redirecting a first flow of gas flowing through a first channel of a turbine blade (6) into a central plenum (44) of the turbine blade (6); and a second arcuate turn (70) for redirecting a second flow of gas flowing through a second channel of the turbine blade (6) into the central plenum (44) of the turbine blade (6), wherein the first and second arcuate turns (60, 70) reduce impingement of the first flow of gas and the second flow of gas in the central plenum (44) of the turbine blade (6). |
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fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3184738A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3184738A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3184738A13</originalsourceid><addsrcrecordid>eNrjZFBz9vf38fRzV3D2DHIO9QxRcPMPUnBU8A31CfHUDXf08VFw8nF0ceVhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcaGFibmxhaOhsZEKAEAX7Ai3w</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>COOLING CIRCUIT FOR A MULTI-WALL BLADE</title><source>esp@cenet</source><creator>WEBER, David Wayne ; WILLETT, Fred Thomas Jr</creator><creatorcontrib>WEBER, David Wayne ; WILLETT, Fred Thomas Jr</creatorcontrib><description>A turbine blade cooling system according to an embodiment includes: a first arcuate turn for redirecting a first flow of gas flowing through a first channel of a turbine blade (6) into a central plenum (44) of the turbine blade (6); and a second arcuate turn (70) for redirecting a second flow of gas flowing through a second channel of the turbine blade (6) into the central plenum (44) of the turbine blade (6), wherein the first and second arcuate turns (60, 70) reduce impingement of the first flow of gas and the second flow of gas in the central plenum (44) of the turbine blade (6).</description><language>eng ; fre ; ger</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS ; INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2017</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=20170628&DB=EPODOC&CC=EP&NR=3184738A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170628&DB=EPODOC&CC=EP&NR=3184738A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WEBER, David Wayne</creatorcontrib><creatorcontrib>WILLETT, Fred Thomas Jr</creatorcontrib><title>COOLING CIRCUIT FOR A MULTI-WALL BLADE</title><description>A turbine blade cooling system according to an embodiment includes: a first arcuate turn for redirecting a first flow of gas flowing through a first channel of a turbine blade (6) into a central plenum (44) of the turbine blade (6); and a second arcuate turn (70) for redirecting a second flow of gas flowing through a second channel of the turbine blade (6) into the central plenum (44) of the turbine blade (6), wherein the first and second arcuate turns (60, 70) reduce impingement of the first flow of gas and the second flow of gas in the central plenum (44) of the turbine blade (6).</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</subject><subject>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</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>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFBz9vf38fRzV3D2DHIO9QxRcPMPUnBU8A31CfHUDXf08VFw8nF0ceVhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcaGFibmxhaOhsZEKAEAX7Ai3w</recordid><startdate>20170628</startdate><enddate>20170628</enddate><creator>WEBER, David Wayne</creator><creator>WILLETT, Fred Thomas Jr</creator><scope>EVB</scope></search><sort><creationdate>20170628</creationdate><title>COOLING CIRCUIT FOR A MULTI-WALL BLADE</title><author>WEBER, David Wayne ; WILLETT, Fred Thomas Jr</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3184738A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2017</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</topic><topic>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</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>WEBER, David Wayne</creatorcontrib><creatorcontrib>WILLETT, Fred Thomas Jr</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WEBER, David Wayne</au><au>WILLETT, Fred Thomas Jr</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COOLING CIRCUIT FOR A MULTI-WALL BLADE</title><date>2017-06-28</date><risdate>2017</risdate><abstract>A turbine blade cooling system according to an embodiment includes: a first arcuate turn for redirecting a first flow of gas flowing through a first channel of a turbine blade (6) into a central plenum (44) of the turbine blade (6); and a second arcuate turn (70) for redirecting a second flow of gas flowing through a second channel of the turbine blade (6) into the central plenum (44) of the turbine blade (6), wherein the first and second arcuate turns (60, 70) reduce impingement of the first flow of gas and the second flow of gas in the central plenum (44) of the turbine blade (6).</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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subjects | BLASTING ENGINE PLANTS IN GENERAL HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
title | COOLING CIRCUIT FOR A MULTI-WALL BLADE |
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