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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Hauptverfasser: 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
Format: Patent
Sprache:eng
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Zusammenfassung: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.