Inventor

MCMAHAN KEVIN WESTON

US58 patents

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

MCMAHAN KEVIN WESTON

GEN ELECTRIC

Burner tube and method for mixing air and gas in a gas turbine engine

One-piece can combustor

System having layered structure and method of making the same

Articulated transition duct in turbomachine

Fuel nozzle for a combustor of a gas turbine engine

Segmented annular combustion system with axial fuel staging

Mounting of integrated combustor nozzles in a segmented annular combustion system

Combustor assembly for use in a turbine engine and methods of fabricating same

Curved seal for adjacent gas turbine components

Transition duct with divided upstream and downstream portions

Micro-mixer nozzle

Gas turbine burner

Clocked combustor can array

Integrated combustor nozzles with continuously curved liner segments

Aft frame assembly for gas turbine transition piece

System having layered structure and method of making the same

AFT frame assembly for gas turbine transition piece

Aft frame assembly for gas turbine transition piece

Curved seal for adjacent gas turbine components

Multi-premixer fuel nozzle support system

Transition duct assembly with late injection features

Transition duct assembly with late injection features

Transition duct assembly

MCMAHAN KEVIN WESTON

Spring loaded seal assembly for turbines

Systems and methods for reintroducing gas turbine combustion bypass flow

Segmented annular ring-manifold quaternary fuel distributor

Segmented combustor cap

Preferential cooling of gas turbine nozzles

Combustor liner helical cooling apparatus

Methods and systems for transferring heat from a transition nozzle

Methods and systems for inducing combustion dynamics

Methods and systems for cooling a transition nozzle

Methods and systems for cooling a transition nozzle

FLANAGAN JAMES SCOTT

Leaf seal for transition duct in turbine system

Flexible metallic seal for transition duct in turbine system

Convolution seal for transition duct in turbine system

LEBEGUE JEFFREY SCOTT

Transition duct with late injection in turbine system

Support assembly for transition duct in turbine system

Support assembly for transition duct in turbine system

CHILA RONALD JAMES

Effusion cooled one-piece can combustor

High temperature seal for a turbine engine

BERRY JONATHAN DWIGHT

Multi-premixer fuel nozzle support system

Impingement cooled transition piece aft frame

STRYAPUNIN SERGEY ALEKSANDROVICH

Gas turbine system having premixed injector vanes

CIHLAR DAVID WILLIAM

Aft frame and method for cooling aft frame

DAVIS JR LEWIS BERKLEY

Integrated combustor and stage 1 nozzle in a gas turbine and method

EDWARDS KARA JOHNSTON

System and method for thermal control in a cap of a gas turbine combustor

VENKATARAMAN KRISHNA KUMAR

Seals for a turbine engine, and methods of assembling a turbine engine

CHEN WEI

Injector seal for a gas turbomachine

KIM WON-WOOK

Combustor with non-circular head end