Inventor · disambiguated record
David Louis Burrus
Also filed as: BURRUS DAVID · BURRUS DAVID L · BURRUS DAVID LOUIS
18 granted patents·4 pending applications·1,062 citations·filing 1995–2019
96Inventor score
Top patents by PatentIndex Score
22 records- 0196US6286298B1Apparatus and method for rich-quench-lean (RQL) concept in a gas turbine engine combustor having trapped vortex cavityGEN ELECTRIC·Filed 1998·Granted Sep 11, 2001·117 cites·14 claims
- 0296US5619855AHigh inlet mach combustor for gas turbine engineGEN ELECTRIC·Filed 1995·Granted Apr 15, 1997·194 cites·25 claims
- 0395US6481209B1Methods and apparatus for decreasing combustor emissions with swirl stabilized mixerGEN ELECTRIC·Filed 2000·Granted Nov 19, 2002·94 cites·14 claims
- 0494US6735949B1Gas turbine engine combustor can with trapped vortex cavityGEN ELECTRIC·Filed 2002·Granted May 18, 2004·84 cites·16 claims
- 0594US6295801B1Fuel injector bar for gas turbine engine combustor having trapped vortex cavityGEN ELECTRIC·Filed 1998·Granted Oct 2, 2001·95 cites·14 claims
- 0694US5791148ALiner of a gas turbine engine combustor having trapped vortex cavityGEN ELECTRIC·Filed 1995·Granted Aug 11, 1998·126 cites·9 claims
- 0791US7716931B2Method and apparatus for assembling gas turbine engineGEN ELECTRIC·Filed 2006·Granted May 18, 2010·30 cites·8 claims
- 0891US6951108B2Gas turbine engine combustor can with trapped vortex cavityGEN ELECTRIC·Filed 2004·Granted Oct 4, 2005·69 cites·9 claims
- 0981US6286317B1Cooling nugget for a liner of a gas turbine engine combustor having trapped vortex cavityGEN ELECTRIC·Filed 1998·Granted Sep 11, 2001·63 cites·18 claims
- 1080US6843059B2Combustor inlet diffuser with boundary layer blowingGEN ELECTRIC·Filed 2002·Granted Jan 18, 2005·26 cites·21 claims
- 1179US8272219B1Gas turbine engine combustor having trapped dual vortex cavityJOHNSON ARTHUR WESLEY·Filed 2000·Granted Sep 25, 2012·51 cites·23 claims
- 1278US6540162B1Methods and apparatus for decreasing combustor emissions with spray bar assemblyGEN ELECTRIC·Filed 2000·Granted Apr 1, 2003·18 cites·7 claims
- 1375US7895841B2Method and apparatus to facilitate reducing NOx emissions in turbine enginesGEN ELECTRIC·Filed 2006·Granted Mar 1, 2011·9 cites·17 claims
- 1471US6851263B2Liner for a gas turbine engine combustor having trapped vortex cavityGEN ELECTRIC·Filed 2002·Granted Feb 8, 2005·37 cites·20 claims
- 1566US8453675B2Rotary union with selectively controlled sealBURRUS DAVID·Filed 2009·Granted Jun 4, 2013·9 cites·19 claims
- 1664US6497103B2Methods for decreasing combustor emissionsGEN ELECTRIC·Filed 2002·Granted Dec 24, 2002·21 cites·6 claims
- 1762US6736338B2Methods and apparatus for decreasing combustor emissionsGEN ELECTRIC·Filed 2003·Granted May 18, 2004·19 cites·12 claims
- 1846US2020217437A1Rotary jointDEUBLIN CO·Filed 2019·Application pending·0 cites
- 1944US11480338B2Combustor system for high fuel/air ratio and reduced combustion dynamicsGEN ELECTRIC·Filed 2017·Granted Oct 25, 2022·0 cites·17 claims
- 2041US2019056108A1Non-uniform mixer for combustion dynamics attenuationGEN ELECTRIC·Filed 2017·Application pending·0 cites
- 2140US2008271457A1Cooling Holes For Gas Turbine Combustor Having A Non-Uniform Diameter TherethroughGEN ELECTRIC·Filed 2007·Application pending·0 cites
- 2237US2007028595A1High pressure gas turbine engine having reduced emissionsMONGIA HUKAM C·Filed 2005·Application pending·0 cites
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