Stress relieved blade support

Details Stress relieved blade support Stress relieved blade support

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/30 (2006.01)

Patent

CA 2306547

A rotor blade 16 having a dovetail 24 is mounted in a complementary slot 14 in a rotor disk 12, with radially engaging outer and inner pressure faces 38,40,42,44, respectively. Relief grooves 48,50 are provided for reducing stiffness at contact edges 46 between the pressure faces to reduce peak stress thereat.

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