Double bowed compressor airfoil

Details Double bowed compressor airfoil Double bowed compressor airfoil

F - Mech Eng,Light,Heat,Weapons

04

D

F04D 29/38 (2006.01) F04D 29/32 (2006.01)

Patent

CA 2326424

A compressor airfoil (12) includes pressure and suction sides (18,20) extending from root (22) to tip (24) and between leading and trailing edges (26,28). Transverse sections have respective chords and camber lines. Centers of gravity (34) of the sections are aligned along a double bowed stacking axis for improving performance.

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