Beverly Stephenson Duncan

Person

West Chester, OH, US

People

Patents Grantslast 30 patents

Information Patent Grant
Trapped vortex combustor for a gas turbine engine with a driver air...
- Patent number 11,788,725
- Issue date Oct 17, 2023
- General Electric Company
- Beverly Stephenson Duncan
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Fuel nozzle assembly for high fuel/air ratio and reduced combustion...
- Patent number 11,561,008
- Issue date Jan 24, 2023
- General Electric Company
- Eric John Stevens
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Trapped vortex combustor for a gas turbine engine with a driver air...
- Patent number 11,262,073
- Issue date Mar 1, 2022
- General Electric Company
- Beverly Stephenson Duncan
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Fuel nozzle centerbody and method of assembling the same
- Patent number 8,555,645
- Issue date Oct 15, 2013
- General Electric Company
- Beverly Stephenson Duncan
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Liner for a gas turbine engine combustor having trapped vortex cavity
- Patent number 6,851,263
- Issue date Feb 8, 2005
- General Electric Company
- James Anthony Stumpf
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Fuel nozzle assembly for reduced exhaust emissions
- Patent number 6,389,815
- Issue date May 21, 2002
- General Electric Company
- Harjit Singh Hura
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Multi-hole film cooled combuster liner
- Patent number 6,205,789
- Issue date Mar 27, 2001
- General Electric Company
- David B. Patterson
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Transitional multihole combustion liner
- Patent number 6,145,319
- Issue date Nov 14, 2000
- General Electric Company
- Craig P. Burns
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES

Patents Applicationslast 30 patents

Information Patent Application
TRAPPED VORTEX COMBUSTOR FOR A GAS TURBINE ENGINE WITH A DRIVER AIR...
- Publication number 20220090788
- Publication date Mar 24, 2022
- GENERAL ELECTRIC COMPANY
- Beverly Stephenson Duncan
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
FUEL NOZZLE ASSEMBLY FOR HIGH FUEL/AIR RATIO AND REDUCED COMBUSTION...
- Publication number 20190063753
- Publication date Feb 28, 2019
- GENERAL ELECTRIC COMPANY
- Eric John Stevens
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
TRAPPED VORTEX COMBUSTOR FOR A GAS TURBINE ENGINE WITH A DRIVER AIR...
- Publication number 20180320900
- Publication date Nov 8, 2018
- GENERAL ELECTRIC COMPANY
- Beverly Stephenson Duncan
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
FUEL NOZZLE CENTERBODY AND METHOD OF ASSEMBLING THE SAME
- Publication number 20100012750
- Publication date Jan 21, 2010
- GENERAL ELECTRIC COMPANY
- Beverly Stephenson Duncan
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Liner for a gas turbine engine combustor having trapped vortex cavity
- Publication number 20040079083
- Publication date Apr 29, 2004
- James Anthony Stumpf
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES

Beverly Stephenson Duncan

Person

Patents Grantslast 30 patents

Trapped vortex combustor for a gas turbine engine with a driver air...

Fuel nozzle assembly for high fuel/air ratio and reduced combustion...

Trapped vortex combustor for a gas turbine engine with a driver air...

Fuel nozzle centerbody and method of assembling the same

Liner for a gas turbine engine combustor having trapped vortex cavity

Fuel nozzle assembly for reduced exhaust emissions

Multi-hole film cooled combuster liner

Transitional multihole combustion liner

Patents Applicationslast 30 patents

TRAPPED VORTEX COMBUSTOR FOR A GAS TURBINE ENGINE WITH A DRIVER AIR...

FUEL NOZZLE ASSEMBLY FOR HIGH FUEL/AIR RATIO AND REDUCED COMBUSTION...

TRAPPED VORTEX COMBUSTOR FOR A GAS TURBINE ENGINE WITH A DRIVER AIR...

FUEL NOZZLE CENTERBODY AND METHOD OF ASSEMBLING THE SAME

Liner for a gas turbine engine combustor having trapped vortex cavity