OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE BLADE, IN PARTICULAR FOR A ROTARY WHEEL OF A TURBINE
When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X, Y, Zadim given in Table 1, in which the coordinate Zadim is the quotient D/H where D is the distance of the point under consideration from a first...
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| creator | PINTAT, Ludovic MARCHE, Pierre Hervé Fernand LEONARDON, Vincent Nicolas MERVANT, Thomas Michel Julien ROYAN, Renaud Gabriel Constant |
| description | When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X, Y, Zadim given in Table 1, in which the coordinate Zadim is the quotient D/H where D is the distance of the point under consideration from a first reference plane P0 situated at the base of the nominal profile, and H is the height of said profile measured from the first reference plane to a second reference plane P1. The measurements D and H are taken radially relative to the axis of the turbine, while the X coordinate is measured in the axial direction of the turbine. |
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The measurements D and H are taken radially relative to the axis of the turbine, while the X coordinate is measured in the axial direction of the turbine.</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>2018</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=20181115&DB=EPODOC&CC=US&NR=2018328181A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20181115&DB=EPODOC&CC=US&NR=2018328181A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PINTAT, Ludovic</creatorcontrib><creatorcontrib>MARCHE, Pierre Hervé Fernand</creatorcontrib><creatorcontrib>LEONARDON, Vincent Nicolas</creatorcontrib><creatorcontrib>MERVANT, Thomas Michel Julien</creatorcontrib><creatorcontrib>ROYAN, Renaud Gabriel Constant</creatorcontrib><title>OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE BLADE, IN PARTICULAR FOR A ROTARY WHEEL OF A TURBINE</title><description>When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X, Y, Zadim given in Table 1, in which the coordinate Zadim is the quotient D/H where D is the distance of the point under consideration from a first reference plane P0 situated at the base of the nominal profile, and H is the height of said profile measured from the first reference plane to a second reference plane P1. The measurements D and H are taken radially relative to the axis of the turbine, while the X coordinate is measured in the axial direction of the turbine.</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>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNy7EKwjAQgOEuDqK-w4GrgmmXrtf0Qg_SpJwJUpdaJE6ihfr-uBRcnf7l-9fZzXeBW75SDUji695hyxo68YYtgfECCCFKxY6gsljTAdhBhxJYR4uyEPEBpYdLQ2TBm9-0zVaP8Tmn3dJNtjcUdHNM03tI8zTe0yt9hnjOT6os8lKVClXxn_oCEDcz0Q</recordid><startdate>20181115</startdate><enddate>20181115</enddate><creator>PINTAT, Ludovic</creator><creator>MARCHE, Pierre Hervé Fernand</creator><creator>LEONARDON, Vincent Nicolas</creator><creator>MERVANT, Thomas Michel Julien</creator><creator>ROYAN, Renaud Gabriel Constant</creator><scope>EVB</scope></search><sort><creationdate>20181115</creationdate><title>OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE BLADE, IN PARTICULAR FOR A ROTARY WHEEL OF A TURBINE</title><author>PINTAT, Ludovic ; MARCHE, Pierre Hervé Fernand ; LEONARDON, Vincent Nicolas ; MERVANT, Thomas Michel Julien ; ROYAN, Renaud Gabriel Constant</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2018328181A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2018</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>PINTAT, Ludovic</creatorcontrib><creatorcontrib>MARCHE, Pierre Hervé Fernand</creatorcontrib><creatorcontrib>LEONARDON, Vincent Nicolas</creatorcontrib><creatorcontrib>MERVANT, Thomas Michel Julien</creatorcontrib><creatorcontrib>ROYAN, Renaud Gabriel Constant</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PINTAT, Ludovic</au><au>MARCHE, Pierre Hervé Fernand</au><au>LEONARDON, Vincent Nicolas</au><au>MERVANT, Thomas Michel Julien</au><au>ROYAN, Renaud Gabriel Constant</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE BLADE, IN PARTICULAR FOR A ROTARY WHEEL OF A TURBINE</title><date>2018-11-15</date><risdate>2018</risdate><abstract>When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X, Y, Zadim given in Table 1, in which the coordinate Zadim is the quotient D/H where D is the distance of the point under consideration from a first reference plane P0 situated at the base of the nominal profile, and H is the height of said profile measured from the first reference plane to a second reference plane P1. The measurements D and H are taken radially relative to the axis of the turbine, while the X coordinate is measured in the axial direction of the turbine.</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 | OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE BLADE, IN PARTICULAR FOR A ROTARY WHEEL OF A TURBINE |
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