AN OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE BLADE, IN PARTICULAR FOR A ROTARY WHEEL OF THE FIRST STAGE OF A TURBINE

An aerodynamic airfoil profile for a blade of a turbine, which, when cold and in a non-coated state, is substantially identical to a nominal profile determined by Cartesian coordinates X,Y,Z', in which the coordinate Z' is the quotient D/H, where D is the distance of the point under consid...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ROYAN, RENAUD, ROUTIER, PASCAL, MARTET, RENAUD, BLEUZEN, JEAN
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	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
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