David L. Burrus

Person

Cincinnati, OH, US

People

Patents Grantslast 30 patents

Information Patent Grant
Combustor system for high fuel/air ratio and reduced combustion dyn...
- Patent number 11,480,338
- Issue date Oct 25, 2022
- General Electric Company
- Eric John Stevens
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Gas turbine engine combustor having trapped dual vortex cavity
- Patent number 8,272,219
- Issue date Sep 25, 2012
- General Electric Company
- Arthur Wesley Johnson
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Method and apparatus to facilitate reducing NOx emissions in turbin...
- Patent number 7,895,841
- Issue date Mar 1, 2011
- General Electric Company
- Arthur Wesley Johnson
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Method and apparatus for assembling gas turbine engine
- Patent number 7,716,931
- Issue date May 18, 2010
- General Electric Company
- Alfred A. Mancini
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Gas turbine engine combustor can with trapped vortex cavity
- Patent number 6,951,108
- Issue date Oct 4, 2005
- General Electric Company
- David Louis Burrus
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
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
Combustor inlet diffuser with boundary layer blowing
- Patent number 6,843,059
- Issue date Jan 18, 2005
- General Electric Company
- David Louis Burrus
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Gas turbine engine combustor can with trapped vortex cavity
- Patent number 6,735,949
- Issue date May 18, 2004
- General Electric Company
- Joel Meier Haynes
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Methods and apparatus for decreasing combustor emissions
- Patent number 6,736,338
- Issue date May 18, 2004
- General Electric Company
- Arthur Wesley Johnson
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Methods and apparatus for decreasing combustor emissions with spray...
- Patent number 6,540,162
- Issue date Apr 1, 2003
- General Electric Company
- Arthur Wesley Johnson
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Methods for decreasing combustor emissions
- Patent number 6,497,103
- Issue date Dec 24, 2002
- General Electric Company
- Arthur Wesley Johnson
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Methods and apparatus for decreasing combustor emissions with swirl...
- Patent number 6,481,209
- Issue date Nov 19, 2002
- General Electric Company
- Arthur Wesley Johnson
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Fuel injector bar for gas turbine engine combustor having trapped v...
- Patent number 6,295,801
- Issue date Oct 2, 2001
- General Electric Company
- David L. Burrus
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Cooling nugget for a liner of a gas turbine engine combustor having...
- Patent number 6,286,317
- Issue date Sep 11, 2001
- General Electric Company
- David L. Burrus
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Apparatus and method for rich-quench-lean (RQL) concept in a gas tu...
- Patent number 6,286,298
- Issue date Sep 11, 2001
- General Electric Company
- David L. Burrus
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Liner of a gas turbine engine combustor having trapped vortex cavity
- Patent number 5,791,148
- Issue date Aug 11, 1998
- General Electric Company
- David L. Burrus
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
High inlet mach combustor for gas turbine engine
- Patent number 5,619,855
- Issue date Apr 15, 1997
- General Electric Company
- David L. Burrus
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES

Patents Applicationslast 30 patents

Information Patent Application
COMBUSTOR SYSTEM FOR HIGH FUEL/AIR RATIO AND REDUCED COMBUSTION DYN...
- Publication number 20190063752
- Publication date Feb 28, 2019
- GENERAL ELECTRIC COMPANY
- Eric John Stevens
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
NON-UNIFORM MIXER FOR COMBUSTION DYNAMICS ATTENUATION
- Publication number 20190056108
- Publication date Feb 21, 2019
- GENERAL ELECTRIC COMPANY
- Hejie Li
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD AND APPARATUS FOR ASSEMBLING GAS TURBINE ENGINE
- Publication number 20100083664
- Publication date Apr 8, 2010
- General Electric Company
- Alfred A. Mancini
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Cooling Holes For Gas Turbine Combustor Having A Non-Uniform Diamet...
- Publication number 20080271457
- Publication date Nov 6, 2008
- GENERAL ELECTRIC COMPANY
- Marie Ann McMasters
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Method and apparatus to facilitate reducing NOx emissions in turbin...
- Publication number 20080010991
- Publication date Jan 17, 2008
- General Electric Company
- Arthur Wesley Johnson
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
High pressure gas turbine engine having reduced emissions
- Publication number 20070028595
- Publication date Feb 8, 2007
- Hukam Chand Mongia
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
GAS TURBINE ENGINE COMBUSTOR CAN WITH TRAPPED VORTEX CAVITY
- Publication number 20050034458
- Publication date Feb 17, 2005
- David Louis Burrus
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
GAS TURBINE ENGINE COMBUSTOR CAN WITH TRAPPED VORTEX CAVITY
- Publication number 20040103663
- Publication date Jun 3, 2004
- Joel Meier Haynes
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Combustor inlet diffuser with boundary layer blowing
- Publication number 20040093871
- Publication date May 20, 2004
- David Louis Burrus
- 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
Information Patent Application
Methods and apparatus for decreasing combustor emissions
- Publication number 20030141388
- Publication date Jul 31, 2003
- Arthur Wesley Johnson
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Methods for decreasing combustor emissions
- Publication number 20020112482
- Publication date Aug 22, 2002
- Arthur Wesley Johnson
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES

David L. Burrus

Person

Patents Grantslast 30 patents

Combustor system for high fuel/air ratio and reduced combustion dyn...

Gas turbine engine combustor having trapped dual vortex cavity

Method and apparatus to facilitate reducing NOx emissions in turbin...

Method and apparatus for assembling gas turbine engine

Gas turbine engine combustor can with trapped vortex cavity

Liner for a gas turbine engine combustor having trapped vortex cavity

Combustor inlet diffuser with boundary layer blowing

Gas turbine engine combustor can with trapped vortex cavity

Methods and apparatus for decreasing combustor emissions

Methods and apparatus for decreasing combustor emissions with spray...

Methods for decreasing combustor emissions

Methods and apparatus for decreasing combustor emissions with swirl...

Fuel injector bar for gas turbine engine combustor having trapped v...

Cooling nugget for a liner of a gas turbine engine combustor having...

Apparatus and method for rich-quench-lean (RQL) concept in a gas tu...

Liner of a gas turbine engine combustor having trapped vortex cavity

High inlet mach combustor for gas turbine engine

Patents Applicationslast 30 patents

COMBUSTOR SYSTEM FOR HIGH FUEL/AIR RATIO AND REDUCED COMBUSTION DYN...

NON-UNIFORM MIXER FOR COMBUSTION DYNAMICS ATTENUATION

METHOD AND APPARATUS FOR ASSEMBLING GAS TURBINE ENGINE

Cooling Holes For Gas Turbine Combustor Having A Non-Uniform Diamet...

Method and apparatus to facilitate reducing NOx emissions in turbin...

High pressure gas turbine engine having reduced emissions

GAS TURBINE ENGINE COMBUSTOR CAN WITH TRAPPED VORTEX CAVITY

GAS TURBINE ENGINE COMBUSTOR CAN WITH TRAPPED VORTEX CAVITY

Combustor inlet diffuser with boundary layer blowing

Liner for a gas turbine engine combustor having trapped vortex cavity

Methods and apparatus for decreasing combustor emissions

Methods for decreasing combustor emissions