TURBOMACHINE COMPRESSOR BLADE COMPRISING A CURVED PORTION

A turbomachine compressor blade of main radial orientation with respect to a main axis of the turbomachine. The blade includes a radially internal root portion, a radially external tip portion, a radially intermediate portion, a curved portion tangentially in a direction, and at least one straight p...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	CELLIER, Damien, PELLETRAU, Philippe, Pierre, Marcel, Marie, PERROT, Vincent, Paul, Gabriel, DUFRESNE, Alicia, Lise, Julia, RIOS, Jean-François, Antoine, Christian, VILLAINES, Laurent, Christophe, Francis
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A turbomachine compressor blade of main radial orientation with respect to a main axis of the turbomachine. The blade includes a radially internal root portion, a radially external tip portion, a radially intermediate portion, a curved portion tangentially in a direction, and at least one straight portion on the root portion and/or on the tip portion.