HYBRID AIRFOIL FOR GAS TURBINE ENGINES

An airfoil (66, 166, 266) for a gas turbine engine includes an airfoil section (66A, 166A, 266A) that extends from a root section (66B, 266B). The airfoil section (66A, 166A, 266A) extends between a leading edge (LE) and a trailing edge (TE) in a chordwise direction (C) and extends between a tip por...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	HUSBAND, Jason, GLASPEY, James
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 STEAM ENGINES WEAPONS
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