Inventor

BUNKER RONALD SCOTT

US166 patents

⚠️ This page may combine multiple inventors who share the name “BUNKER RONALD SCOTT”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

BUNKER RONALD SCOTT

GEN ELECTRIC

Chevron film cooled wall

Method for improving the cooling effectiveness of a gaseous coolant stream, and related articles of manufacture

Cooling for double-wall structures

Combustor cooling with angled segmented surfaces

Method of forming concavities in the surface of a metal component, and related processes and articles

Hot gas path component with mesh and dimpled cooling

Hot gas path component with mesh and turbulated cooling

Combustor liner with ring turbulators and related method

Cooling passages and methods of fabrication

Film cooled blade tip

Turbine blade tip with offset squealer

Turbine engine with an airfoil having a tip shelf outlet

Film cooled slotted wall

Method and apparatus for cooling combustor liner and transition piece of a gas turbine

Scalloped surface turbine stage

Combustor liner with inverted turbulators

Thermal shield turbine airfoil

Double wall combustor liner segment with enhanced cooling

Generator stator cooling design with concavity surfaces

Shroud leakage flow discouragers

Airfoil with reduced heat load

Tandem airfoils

Turbine blade tip flow discouragers

Method of making double-walled turbine components from pre-consolidated assemblies

Film cooled wall

Method and apparatus for non-destructive thermal inspection

Components with multi-layered cooling features and methods of manufacture

Components with porous metal cooling and methods of manufacture

Component and methods of fabricating and coating a component

Stator-rotor assembly having surface feature for enhanced containment of gas flow and related processes

High expansion fuel injection slot jet and method for enhancing mixing in premixing devices

Film cooled slotted wall and method of making the same

Hot gas path component with mesh and impingement cooling

Component and turbine assembly with film cooling

Linear surface concavity enhancement

Turbine blade having a cooled tip shroud

Coolable airfoil

Shaped walls for enhancement of deflagration-to-detonation transition

System and method for thermal inspection of parts

Methods and apparatus for cooling gas turbine engine components

Converging pin cooled airfoil

Turbine blade cover cooling apparatus and method of fabrication

BUNKER RONALD SCOTT

Components with microchannel cooling

Articles which include chevron film cooling holes, and related processes

Turbine components with cooling features and methods of manufacturing the same

Components with conformal curved film holes and methods of manufacture

Cooling channel systems for high-temperature components covered by coatings, and related processes

Methods of fabricating and coating a component

Methods of manufacture for components with cooling channels

LACY BENJAMIN PAUL

Hot gas path component cooling system