Turbine assembly and method for supporting turbine components
According to one aspect of the invention, a turbine assembly 10 includes a first static structure and a second static structure radially outward of the first static structure. The assembly 10 also includes a support member 40 placed in a recess 42 of the second static structure, wherein the support...
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| creator | KLINGLER, BRETT DARRICK |
| description | According to one aspect of the invention, a turbine assembly 10 includes a first static structure and a second static structure radially outward of the first static structure. The assembly 10 also includes a support member 40 placed in a recess 42 of the second static structure, wherein the support member 40 includes first and second curved surfaces 54,56 to contact the first and second static structures, respectively, and wherein the support member 40 includes a biasing structure 48,52 to retain the support member 40 in the recess 42. |
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The assembly 10 also includes a support member 40 placed in a recess 42 of the second static structure, wherein the support member 40 includes first and second curved surfaces 54,56 to contact the first and second static structures, respectively, and wherein the support member 40 includes a biasing structure 48,52 to retain the support member 40 in the recess 42.</description><language>eng ; fre ; ger</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>2014</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=20140101&DB=EPODOC&CC=EP&NR=2636851A3$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140101&DB=EPODOC&CC=EP&NR=2636851A3$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KLINGLER, BRETT DARRICK</creatorcontrib><title>Turbine assembly and method for supporting turbine components</title><description>According to one aspect of the invention, a turbine assembly 10 includes a first static structure and a second static structure radially outward of the first static structure. The assembly 10 also includes a support member 40 placed in a recess 42 of the second static structure, wherein the support member 40 includes first and second curved surfaces 54,56 to contact the first and second static structures, respectively, and wherein the support member 40 includes a biasing structure 48,52 to retain the support member 40 in the recess 42.</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>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLANKS1KysxLVUgsLk7NTcqpVEjMS1HITS3JyE9RSMsvUiguLSjILyrJzEtXKIEqTc7PLcjPS80rKeZhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAUZmxmYWpoaOxsZEKAEAB2kwfA</recordid><startdate>20140101</startdate><enddate>20140101</enddate><creator>KLINGLER, BRETT DARRICK</creator><scope>EVB</scope></search><sort><creationdate>20140101</creationdate><title>Turbine assembly and method for supporting turbine components</title><author>KLINGLER, BRETT DARRICK</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2636851A33</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2014</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>KLINGLER, BRETT DARRICK</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KLINGLER, BRETT DARRICK</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Turbine assembly and method for supporting turbine components</title><date>2014-01-01</date><risdate>2014</risdate><abstract>According to one aspect of the invention, a turbine assembly 10 includes a first static structure and a second static structure radially outward of the first static structure. The assembly 10 also includes a support member 40 placed in a recess 42 of the second static structure, wherein the support member 40 includes first and second curved surfaces 54,56 to contact the first and second static structures, respectively, and wherein the support member 40 includes a biasing structure 48,52 to retain the support member 40 in the recess 42.</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 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| title | Turbine assembly and method for supporting turbine components |
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