DB

David Louis Burrus

GE: 17 patents #1,712 of 36,430Top 5%
DC Deublin Company: 1 patents #11 of 20Top 60%
📍 Cincinnati, OH: #480 of 8,043 inventorsTop 6%
🗺 Ohio: #3,840 of 73,341 inventorsTop 6%
Overall (All Time): #253,113 of 4,157,543Top 7%
18
Patents All Time

Issued Patents All Time

Showing 1–18 of 18 patents

Patent #TitleCo-InventorsDate
11480338 Combustor system for high fuel/air ratio and reduced combustion dynamics Eric John Stevens, Mark David Durbin 2022-10-25
8453675 Rotary union with selectively controlled seal Graig Aaron LaCroix 2013-06-04
8272219 Gas turbine engine combustor having trapped dual vortex cavity Arthur Wesley Johnson 2012-09-25
7895841 Method and apparatus to facilitate reducing NOx emissions in turbine engines Arthur Wesley Johnson, Richard W. Stickles, Willard J. Dodds 2011-03-01
7716931 Method and apparatus for assembling gas turbine engine Alfred Albert Mancini, Steven Joseph Lohmueller 2010-05-18
6951108 Gas turbine engine combustor can with trapped vortex cavity Narendra Digamber Joshi, Joel Meier Haynes, Alan S. Feitelberg 2005-10-04
6851263 Liner for a gas turbine engine combustor having trapped vortex cavity James Anthony Stumpf, Beverly Stephenson Duncan, Clayton Stuart Cooper 2005-02-08
6843059 Combustor inlet diffuser with boundary layer blowing Jack R. Taylor 2005-01-18
6736338 Methods and apparatus for decreasing combustor emissions Arthur Wesley Johnson, Robert Andrew Wade 2004-05-18
6735949 Gas turbine engine combustor can with trapped vortex cavity Joel Meier Haynes, Alan S. Feitelberg, Narendra Digamber Joshi 2004-05-18
6540162 Methods and apparatus for decreasing combustor emissions with spray bar assembly Arthur Wesley Johnson, Robert Andrew Wade 2003-04-01
6497103 Methods for decreasing combustor emissions Arthur Wesley Johnson, Robert Andrew Wade, Hukam Chand Mongia 2002-12-24
6481209 Methods and apparatus for decreasing combustor emissions with swirl stabilized mixer Arthur Wesley Johnson, Robert Andrew Wade, Hukam Chand Mongia 2002-11-19
6295801 Fuel injector bar for gas turbine engine combustor having trapped vortex cavity Arthur Wesley Johnson 2001-10-02
6286317 Cooling nugget for a liner of a gas turbine engine combustor having trapped vortex cavity Arthur Wesley Johnson, George E. Moertle 2001-09-11
6286298 Apparatus and method for rich-quench-lean (RQL) concept in a gas turbine engine combustor having trapped vortex cavity Arthur Wesley Johnson, Hukam Chand Mongia 2001-09-11
5791148 Liner of a gas turbine engine combustor having trapped vortex cavity 1998-08-11
5619855 High inlet mach combustor for gas turbine engine 1997-04-15