Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Blade/disk dovetail backcut for blade/disk stress reduction (9FA+e, stage 1)

Blade/disk dovetail backcut for blade/disk stress reduction (9FA+e, stage 1)

US Patent 7419362 · Granted Sep 2, 2008

Estimated economic value: $59,543,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Control method for stoichiometric exhaust gas recirculation power plant2015
Clearance control system for a gas turbine2015
System and method for supporting a nozzle assembly2014
Method of operating a stoichiometric exhaust gas recirculation power plant2013
Power plant and method of operation2013
Power plant start-up method and method of venting the power plant2012
Power plant and method of use2012
Turbine blade cooling with a hollow airfoil configured to minimize a distance be2012
Methods and apparatus for reducing nozzle stress2012
Gas turbines having flexible chordal hinge seals2011
Fully contained retention pin for a turbine nozzle2011
Airfoil core shape for a turbine nozzle2011