Inventor
CHAN SZE BUN BRIAN
US7 patents
Patents
7 patentsUS7094025B2Aug 22, 2006
Apparatus and methods for removing and installing a selected nozzle segment of a gas turbine in an axial direction
GEN ELECTRIC22 citations90
US7029228B2Apr 18, 2006
Method and apparatus for convective cooling of side-walls of turbine nozzle segments
GEN ELECTRIC34 citations90
US7329093B2Feb 12, 2008
Nozzle blade airfoil profile for a turbine
GEN ELECTRIC43 citations88
US7988420B2Aug 2, 2011
Airfoil shape for a turbine bucket and turbine incorporating same
GEN ELECTRIC12 citations78
US7476084B1Jan 13, 2009
Blade/disk dovetail backcut for blade/disk stress reduction (6FA and 6FA+e, stage 1)
GEN ELECTRIC10 citations78
US8043061B2Oct 25, 2011
Turbine bucket tip shroud edge profile
GEN ELECTRIC13 citations77
US11156102B2Oct 26, 2021
Blade having a tip cooling cavity and method of making same
GEN ELECTRIC0 citations49