Inventor
GAUTREAU JAMES CHARLES
US4 patents
Patents
4 patentsUS6769877B2Aug 3, 2004
Undercut leading edge for compressor blades and related method
GEN ELECTRIC25 citations90
US7121803B2Oct 17, 2006
Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge
GEN ELECTRIC28 citations89
US6902376B2Jun 7, 2005
Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge
GEN ELECTRIC20 citations87
US7165944B2Jan 23, 2007
Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge
GEN ELECTRIC15 citations80