Compressor stator vane airfoils
A stator vane includes an airfoil having an airfoil shape. The airfoil shape has 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 coordin...
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| creator | Latimer, Jeremy Peter Dutka, Michael James Huskins, Steven Lynn DeJoris, Timothy E Malloy, Phillip Matthew S, Vasantharuban Williamson, Aaron David Chaudhary, Nancy Rajagopal, Sunil Blohm, Marc Edward Deivernois, Paul G A R, Nandakumar Rao, Narasimha K V Dalsania, Prakash B, Bala Muralidhar Singh Devangada, Siddaraja Mallikarjuna John, Joshy |
| description | A stator vane includes an airfoil having an airfoil shape. The airfoil shape has 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 are joined smoothly with one another to form a complete airfoil shape. |
| format | Patent |
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The airfoil shape has 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 are joined smoothly with one another to form a complete airfoil shape.</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=20221025&DB=EPODOC&CC=US&NR=11480062B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25546,76297</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20221025&DB=EPODOC&CC=US&NR=11480062B1$$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>DeJoris, Timothy E</creatorcontrib><creatorcontrib>Malloy, Phillip Matthew</creatorcontrib><creatorcontrib>S, Vasantharuban</creatorcontrib><creatorcontrib>Williamson, Aaron David</creatorcontrib><creatorcontrib>Chaudhary, Nancy</creatorcontrib><creatorcontrib>Rajagopal, Sunil</creatorcontrib><creatorcontrib>Blohm, Marc Edward</creatorcontrib><creatorcontrib>Deivernois, Paul G</creatorcontrib><creatorcontrib>A R, Nandakumar</creatorcontrib><creatorcontrib>Rao, Narasimha K V</creatorcontrib><creatorcontrib>Dalsania, Prakash</creatorcontrib><creatorcontrib>B, Bala Muralidhar Singh</creatorcontrib><creatorcontrib>Devangada, Siddaraja Mallikarjuna</creatorcontrib><creatorcontrib>John, Joshy</creatorcontrib><title>Compressor stator vane airfoils</title><description>A stator vane includes an airfoil having an airfoil shape. 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The airfoil shape has 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 are joined smoothly with one another to form a complete airfoil shape.</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 | Compressor stator vane airfoils |
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