TURBOFAN ENGINE WITH GEARED ARCHITECTURE AND LPC BLADES

A compressor airfoil of a turbine engine having a geared architecture includes pressure and suction sides that extend in a radial direction from a 0% span position to a 100% span position. The airfoil has a relationship between an axial stacking offset and span position that includes a curve with a...

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Bibliographische Detailangaben

Hauptverfasser:	HUDON, Kate, BRILLIANT, Lisa I, STEPHENS, Mark A, BALAMUCKI, Stanley J, STRACCIA, Joseph C, GALLAGHER, Edward J
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING HEATING LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS
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