TURBINE NOZZLE SEGMENT AND ASSEMBLY
A turbine nozzle segment includes a band (122, 124) having a plurality of circumferentially spaced apart tabs (130) and a single airfoil (120) extending from the band. L'invention concerne un segment de buse de turbine comprenant une bande (122, 124) composée d'une pluralité de languettes...
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| creator | HEFFRON, TODD, STEPHEN MORGAN, CLIVE, ANDREW FONSEKA, SANJEEWA, THUSITHA |
| description | A turbine nozzle segment includes a band (122, 124) having a plurality of circumferentially spaced apart tabs (130) and a single airfoil (120) extending from the band.
L'invention concerne un segment de buse de turbine comprenant une bande (122, 124) composée d'une pluralité de languettes circonférentiellement espacées (130) et une surface portante unique (120) s'étendant depuis la bande. |
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L'invention concerne un segment de buse de turbine comprenant une bande (122, 124) composée d'une pluralité de languettes circonférentiellement espacées (130) et une surface portante unique (120) s'étendant depuis la bande.</description><language>eng ; fre</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>2009</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=20090709&DB=EPODOC&CC=WO&NR=2009085620A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20090709&DB=EPODOC&CC=WO&NR=2009085620A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HEFFRON, TODD, STEPHEN</creatorcontrib><creatorcontrib>MORGAN, CLIVE, ANDREW</creatorcontrib><creatorcontrib>FONSEKA, SANJEEWA, THUSITHA</creatorcontrib><title>TURBINE NOZZLE SEGMENT AND ASSEMBLY</title><description>A turbine nozzle segment includes a band (122, 124) having a plurality of circumferentially spaced apart tabs (130) and a single airfoil (120) extending from the band.
L'invention concerne un segment de buse de turbine comprenant une bande (122, 124) composée d'une pluralité de languettes circonférentiellement espacées (130) et une surface portante unique (120) s'étendant depuis la bande.</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>2009</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFAOCQ1y8vRzVfDzj4rycVUIdnX3dfULUXD0c1FwDA529XXyieRhYE1LzClO5YXS3AzKbq4hzh66qQX58anFBYnJqXmpJfHh_kYGBpYGFqZmRgaOhsbEqQIA8QMjuw</recordid><startdate>20090709</startdate><enddate>20090709</enddate><creator>HEFFRON, TODD, STEPHEN</creator><creator>MORGAN, CLIVE, ANDREW</creator><creator>FONSEKA, SANJEEWA, THUSITHA</creator><scope>EVB</scope></search><sort><creationdate>20090709</creationdate><title>TURBINE NOZZLE SEGMENT AND ASSEMBLY</title><author>HEFFRON, TODD, STEPHEN ; MORGAN, CLIVE, ANDREW ; FONSEKA, SANJEEWA, THUSITHA</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2009085620A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2009</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>HEFFRON, TODD, STEPHEN</creatorcontrib><creatorcontrib>MORGAN, CLIVE, ANDREW</creatorcontrib><creatorcontrib>FONSEKA, SANJEEWA, THUSITHA</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HEFFRON, TODD, STEPHEN</au><au>MORGAN, CLIVE, ANDREW</au><au>FONSEKA, SANJEEWA, THUSITHA</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBINE NOZZLE SEGMENT AND ASSEMBLY</title><date>2009-07-09</date><risdate>2009</risdate><abstract>A turbine nozzle segment includes a band (122, 124) having a plurality of circumferentially spaced apart tabs (130) and a single airfoil (120) extending from the band.
L'invention concerne un segment de buse de turbine comprenant une bande (122, 124) composée d'une pluralité de languettes circonférentiellement espacées (130) et une surface portante unique (120) s'étendant depuis la bande.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre |
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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 | TURBINE NOZZLE SEGMENT AND ASSEMBLY |
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