Inventor · disambiguated record
Albert K. Cheung
Also filed as: CHEUNG ALBERT K
26 granted patents·4 pending applications·346 citations·filing 2003–2023
96Inventor score
Files withUNITED TECHNOLOGIES CORP21BURD STEVEN W2CHEUNG ALBERT K2EASTWOOD JONATHAN JEFFERY1ERBAS-SEN NURHAK1
Top patents by PatentIndex Score
30 records- 0193US7954325B2Gas turbine combustorUNITED TECHNOLOGIES CORP·Filed 2005·Granted Jun 7, 2011·43 cites·13 claims
- 0292US9797601B2Bluff body fuel mixerUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 24, 2017·6 cites·16 claims
- 0391US7631502B2Local cooling hole patternUNITED TECHNOLOGIES CORP·Filed 2005·Granted Dec 15, 2009·30 cites·21 claims
- 0491US7614235B2Combustor cooling hole patternUNITED TECHNOLOGIES CORP·Filed 2005·Granted Nov 10, 2009·30 cites·29 claims
- 0590US7093441B2Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volumeUNITED TECHNOLOGIES CORP·Filed 2003·Granted Aug 22, 2006·79 cites·20 claims
- 0689US8443610B2Low emission gas turbine combustorHOKE JAMES B·Filed 2009·Granted May 21, 2013·26 cites·23 claims
- 0788US9377198B2Heat shield for a combustorEASTWOOD JONATHAN JEFFERY·Filed 2012·Granted Jun 28, 2016·10 cites·27 claims
- 0884US9052111B2Turbine engine combustor wall with non-uniform distribution of effusion aperturesERBAS-SEN NURHAK·Filed 2012·Granted Jun 9, 2015·11 cites·14 claims
- 0984US7464554B2Gas turbine combustor heat shield panel or exhaust panel including a cooling deviceUNITED TECHNOLOGIES CORP·Filed 2004·Granted Dec 16, 2008·63 cites·16 claims
- 1081US8640463B2Swirler for gas turbine engine fuel injectorCHEUNG ALBERT K·Filed 2011·Granted Feb 4, 2014·7 cites·18 claims
- 1175US11391461B2Combustor bulkhead with circular impingement hole patternUNITED TECHNOLOGIES CORP·Filed 2020·Granted Jul 19, 2022·1 cites·15 claims
- 1273US8056342B2Hole pattern for gas turbine combustorSHELLEY JONATHAN K·Filed 2008·Granted Nov 15, 2011·19 cites·19 claims
- 1370US11143407B2Combustor with axial staging for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 12, 2021·3 cites·20 claims
- 1463US8850819B2Swirler, fuel and air assembly and combustorCHEUNG ALBERT K·Filed 2010·Granted Oct 7, 2014·2 cites·11 claims
- 1563US8800290B2CombustorBURD STEVEN W·Filed 2007·Granted Aug 12, 2014·7 cites·23 claims
- 1662US10816209B2Bluff body fuel mixerUNITED TECHNOLOGIES CORP·Filed 2017·Granted Oct 27, 2020·0 cites·9 claims
- 1762US8028528B2Annular gas turbine combustorUNITED TECHNOLOGIES CORP·Filed 2005·Granted Oct 4, 2011·6 cites·14 claims
- 1861US9068749B2Swirler for gas turbine engine fuel injectorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 30, 2015·1 cites·19 claims
- 1960US10677161B2Gas turbine engine diffuser cooling and mixing arrangementUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 9, 2020·1 cites·17 claims
- 2059US8671692B2Annular gas turbine combustor including converging and diverging segmentsBURD STEVEN W·Filed 2011·Granted Mar 18, 2014·1 cites·14 claims
- 2155US10551065B2Heat shield for a combustorUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 4, 2020·0 cites·15 claims
- 2254US9562690B2Swirler, fuel and air assembly and combustorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Feb 7, 2017·0 cites·5 claims
- 2352US10533502B2Combustor fuel manifoldUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jan 14, 2020·0 cites·13 claims
- 2451US12352441B2Reinforced film floatwall for a gas turbine engineRTX CORP·Filed 2023·Granted Jul 8, 2025·0 cites·19 claims
- 2546US10024538B2Apparatus and method for air extraction at a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 17, 2018·0 cites·14 claims
- 2643US2019063322A1Hybrid floatwall cooling featureUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 2742US10670267B2Combustor hole arrangement for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 2, 2020·0 cites·13 claims
- 2837US2016258627A1Low net-swirl configurations for gas turbine engine combustorsUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 2935US2017003027A1Gas turbine engine combustor liner panel with synergistic cooling featuresUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 3033US2017044979A1Pre-diffuser with high cant angleUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →