Bowed compressor airfoil

Details Bowed compressor airfoil Bowed compressor airfoil

F - Mech Eng,Light,Heat,Weapons

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F04D 29/38 (2006.01) F01D 5/14 (2006.01) F04D 29/32 (2006.01)

Patent

CA 2321330

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 bowed stacking axis either tangentially, axially, or both, for improving performance.

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