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Inventor
RICKERT CHRIS A
US
2 patents
Patents
2 patents
US7121803B2
Oct 17, 2006
Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge
GEN ELECTRIC
28 citations
89
US7165944B2
Jan 23, 2007
Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge
GEN ELECTRIC
15 citations
80