TURBINE RING ASSEMBLY WITH CURVED RECTILINEAR SEATINGS
A turbine ring assembly including ring sectors forming a turbine ring and a ring support structure, each sector having, in a section plane defined by an axial direction and a radial direction of the ring, a first and a second attachment tabs extending in the radial direction, and the structure inclu...
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creator | QUENNEHEN, Lucien Henri Jacques CONGRATEL, Sébastien Serge Francis TABLEAU, Nicolas Paul DANIS, Antoine Claude Michel Etienne DUFFAU, Clément Jean Pierre |
description | A turbine ring assembly including ring sectors forming a turbine ring and a ring support structure, each sector having, in a section plane defined by an axial direction and a radial direction of the ring, a first and a second attachment tabs extending in the radial direction, and the structure including a central shell ring from which extend as projections a first and a second radial flanges between which are retained the first and second attachment tabs of each sector. Each sector includes rectilinear seatings mounted on the faces of the first and second attachment tabs in contact, respectively, with the second annular flange and the annular ring-flange and including, along a tangent to the circumferential direction, a variable thickness in the axial direction with a minimum thickness at the first and second ends of the sector and a maximum thickness in a median portion of the rectilinear seating. |
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Each sector includes rectilinear seatings mounted on the faces of the first and second attachment tabs in contact, respectively, with the second annular flange and the annular ring-flange and including, along a tangent to the circumferential direction, a variable thickness in the axial direction with a minimum thickness at the first and second ends of the sector and a maximum thickness in a median portion of the rectilinear seating.</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>2022</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=20220127&DB=EPODOC&CC=US&NR=2022025775A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220127&DB=EPODOC&CC=US&NR=2022025775A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>QUENNEHEN, Lucien Henri Jacques</creatorcontrib><creatorcontrib>CONGRATEL, Sébastien Serge Francis</creatorcontrib><creatorcontrib>TABLEAU, Nicolas Paul</creatorcontrib><creatorcontrib>DANIS, Antoine Claude Michel Etienne</creatorcontrib><creatorcontrib>DUFFAU, Clément Jean Pierre</creatorcontrib><title>TURBINE RING ASSEMBLY WITH CURVED RECTILINEAR SEATINGS</title><description>A turbine ring assembly including ring sectors forming a turbine ring and a ring support structure, each sector having, in a section plane defined by an axial direction and a radial direction of the ring, a first and a second attachment tabs extending in the radial direction, and the structure including a central shell ring from which extend as projections a first and a second radial flanges between which are retained the first and second attachment tabs of each sector. Each sector includes rectilinear seatings mounted on the faces of the first and second attachment tabs in contact, respectively, with the second annular flange and the annular ring-flange and including, along a tangent to the circumferential direction, a variable thickness in the axial direction with a minimum thickness at the first and second ends of the sector and a maximum thickness in a median portion of the rectilinear seating.</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>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDALCQ1y8vRzVQjy9HNXcAwOdvV18olUCPcM8VBwDg0Kc3VRCHJ1DvH0AapxDFIIdnUMASoM5mFgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8aHBRgZGQGRqbm7qaGhMnCoAy-gpDw</recordid><startdate>20220127</startdate><enddate>20220127</enddate><creator>QUENNEHEN, Lucien Henri Jacques</creator><creator>CONGRATEL, Sébastien Serge Francis</creator><creator>TABLEAU, Nicolas Paul</creator><creator>DANIS, Antoine Claude Michel Etienne</creator><creator>DUFFAU, Clément Jean Pierre</creator><scope>EVB</scope></search><sort><creationdate>20220127</creationdate><title>TURBINE RING ASSEMBLY WITH CURVED RECTILINEAR SEATINGS</title><author>QUENNEHEN, Lucien Henri Jacques ; CONGRATEL, Sébastien Serge Francis ; TABLEAU, Nicolas Paul ; DANIS, Antoine Claude Michel Etienne ; DUFFAU, Clément Jean Pierre</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2022025775A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2022</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>QUENNEHEN, Lucien Henri Jacques</creatorcontrib><creatorcontrib>CONGRATEL, Sébastien Serge Francis</creatorcontrib><creatorcontrib>TABLEAU, Nicolas Paul</creatorcontrib><creatorcontrib>DANIS, Antoine Claude Michel Etienne</creatorcontrib><creatorcontrib>DUFFAU, Clément Jean Pierre</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>QUENNEHEN, Lucien Henri Jacques</au><au>CONGRATEL, Sébastien Serge Francis</au><au>TABLEAU, Nicolas Paul</au><au>DANIS, Antoine Claude Michel Etienne</au><au>DUFFAU, Clément Jean Pierre</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBINE RING ASSEMBLY WITH CURVED RECTILINEAR SEATINGS</title><date>2022-01-27</date><risdate>2022</risdate><abstract>A turbine ring assembly including ring sectors forming a turbine ring and a ring support structure, each sector having, in a section plane defined by an axial direction and a radial direction of the ring, a first and a second attachment tabs extending in the radial direction, and the structure including a central shell ring from which extend as projections a first and a second radial flanges between which are retained the first and second attachment tabs of each sector. Each sector includes rectilinear seatings mounted on the faces of the first and second attachment tabs in contact, respectively, with the second annular flange and the annular ring-flange and including, along a tangent to the circumferential direction, a variable thickness in the axial direction with a minimum thickness at the first and second ends of the sector and a maximum thickness in a median portion of the rectilinear seating.</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 | TURBINE RING ASSEMBLY WITH CURVED RECTILINEAR SEATINGS |
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