Compressor stator vane airfoils
A stator vane includes an airfoil having an airfoil shape. The airfoil shape having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, Table IV, Table V, Table VI, Table VII, or Table VIII. The Cartesian coor...
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| creator | Latimer, Jeremy Peter Dutka, Michael James Huskins, Steven Lynn Hubbert, Corey Lynn Chaluvadi, Venkata Siva Prasad Deivernois, Paul G Blohm, Marcus Edward Williamson, Aaron David Bush, Brandon Lamar Hart, Andrew Clifford |
| description | A stator vane includes an airfoil having an airfoil shape. The airfoil shape having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, Table IV, Table V, Table VI, Table VII, or Table VIII. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a scaling factor of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each Z value. The airfoil profile sections at Z values being joined smoothly with one another to form a complete airfoil shape. |
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The airfoil shape having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, Table IV, Table V, Table VI, Table VII, or Table VIII. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a scaling factor of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each Z value. The airfoil profile sections at Z values being joined smoothly with one another to form a complete airfoil shape.</description><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT PUMPS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; 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=20220405&DB=EPODOC&CC=US&NR=11293454B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220405&DB=EPODOC&CC=US&NR=11293454B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Latimer, Jeremy Peter</creatorcontrib><creatorcontrib>Dutka, Michael James</creatorcontrib><creatorcontrib>Huskins, Steven Lynn</creatorcontrib><creatorcontrib>Hubbert, Corey Lynn</creatorcontrib><creatorcontrib>Chaluvadi, Venkata Siva Prasad</creatorcontrib><creatorcontrib>Deivernois, Paul G</creatorcontrib><creatorcontrib>Blohm, Marcus Edward</creatorcontrib><creatorcontrib>Williamson, Aaron David</creatorcontrib><creatorcontrib>Bush, Brandon Lamar</creatorcontrib><creatorcontrib>Hart, Andrew Clifford</creatorcontrib><title>Compressor stator vane airfoils</title><description>A stator vane includes an airfoil having an airfoil shape. The airfoil shape having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, Table IV, Table V, Table VI, Table VII, or Table VIII. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a scaling factor of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each Z value. The airfoil profile sections at Z values being joined smoothly with one another to form a complete airfoil shape.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT PUMPS</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJB3zs8tKEotLs4vUiguSSwBUmWJeakKiZlFafmZOcU8DKxpiTnFqbxQmptB0c01xNlDN7UgPz61uCAxOTUvtSQ-NNjQ0MjS2MTUxMnQmBg1AE6oJV8</recordid><startdate>20220405</startdate><enddate>20220405</enddate><creator>Latimer, Jeremy Peter</creator><creator>Dutka, Michael James</creator><creator>Huskins, Steven Lynn</creator><creator>Hubbert, Corey Lynn</creator><creator>Chaluvadi, Venkata Siva Prasad</creator><creator>Deivernois, Paul G</creator><creator>Blohm, Marcus Edward</creator><creator>Williamson, Aaron David</creator><creator>Bush, Brandon Lamar</creator><creator>Hart, Andrew Clifford</creator><scope>EVB</scope></search><sort><creationdate>20220405</creationdate><title>Compressor stator vane airfoils</title><author>Latimer, Jeremy Peter ; Dutka, Michael James ; Huskins, Steven Lynn ; Hubbert, Corey Lynn ; Chaluvadi, Venkata Siva Prasad ; Deivernois, Paul G ; Blohm, Marcus Edward ; Williamson, Aaron David ; Bush, Brandon Lamar ; Hart, Andrew Clifford</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US11293454B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2022</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT PUMPS</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Latimer, Jeremy Peter</creatorcontrib><creatorcontrib>Dutka, Michael James</creatorcontrib><creatorcontrib>Huskins, Steven Lynn</creatorcontrib><creatorcontrib>Hubbert, Corey Lynn</creatorcontrib><creatorcontrib>Chaluvadi, Venkata Siva Prasad</creatorcontrib><creatorcontrib>Deivernois, Paul G</creatorcontrib><creatorcontrib>Blohm, Marcus Edward</creatorcontrib><creatorcontrib>Williamson, Aaron David</creatorcontrib><creatorcontrib>Bush, Brandon Lamar</creatorcontrib><creatorcontrib>Hart, Andrew Clifford</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Latimer, Jeremy Peter</au><au>Dutka, Michael James</au><au>Huskins, Steven Lynn</au><au>Hubbert, Corey Lynn</au><au>Chaluvadi, Venkata Siva Prasad</au><au>Deivernois, Paul G</au><au>Blohm, Marcus Edward</au><au>Williamson, Aaron David</au><au>Bush, Brandon Lamar</au><au>Hart, Andrew Clifford</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Compressor stator vane airfoils</title><date>2022-04-05</date><risdate>2022</risdate><abstract>A stator vane includes an airfoil having an airfoil shape. The airfoil shape having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, Table IV, Table V, Table VI, Table VII, or Table VIII. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a scaling factor of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each Z value. The airfoil profile sections at Z values being joined smoothly with one another to form a complete airfoil shape.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS |
| title | Compressor stator vane airfoils |
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