Inventor · disambiguated record
Kevin Joseph Low
Also filed as: LOW KEVIN J · LOW KEVIN JOSEPH
18 granted patents·7 pending applications·90 citations·filing 2002–2018
91Inventor score
Top patents by PatentIndex Score
25 records- 0190US9400104B2Flow modifier for combustor fuel nozzle tipLOW KEVIN JOSEPH·Filed 2012·Granted Jul 26, 2016·20 cites·27 claims
- 0289US9587831B2Cooled combustor sealUNITED TECHNOLOGIES CORP·Filed 2012·Granted Mar 7, 2017·15 cites·20 claims
- 0387US10488046B2Gas turbine engine combustor bulkhead assemblyUNITED TECHNOLOGIES CORP·Filed 2014·Granted Nov 26, 2019·9 cites·14 claims
- 0481US8800298B2Washer with cooling passage for a turbine engine combustorLADD SCOTT A·Filed 2009·Granted Aug 12, 2014·22 cites·20 claims
- 0579US8689563B2Fuel nozzle guide plate mistake proofingLOW KEVIN JOSEPH·Filed 2009·Granted Apr 8, 2014·18 cites·14 claims
- 0666US9511388B2Method and system for holding a combustor panel during coating processUNITED TECHNOLOGIES CORP·Filed 2012·Granted Dec 6, 2016·2 cites·12 claims
- 0763US9297536B2Gas turbine engine combustor surge retentionEASTWOOD JONATHAN JEFFERY·Filed 2012·Granted Mar 29, 2016·2 cites·22 claims
- 0858US10088162B2Combustor with grommet having projecting lipUNITED TECHNOLOGIES CORP·Filed 2013·Granted Oct 2, 2018·1 cites·23 claims
- 0955US11226102B2Fuel nozzle for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jan 18, 2022·0 cites·16 claims
- 1055US10197285B2Gas turbine engine wall assembly interfaceUNITED TECHNOLOGIES CORP·Filed 2014·Granted Feb 5, 2019·0 cites·20 claims
- 1154US8733800B1Tube having an integral, spring-loaded, spherical jointUNITED TECHNOLOGIES CORP·Filed 2012·Granted May 27, 2014·1 cites·8 claims
- 1253US10655855B2Gas turbine engine wall assembly with support shell contour regionsUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 19, 2020·0 cites·20 claims
- 1352US2016033130A1Fuel nozzle for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 1449US10808937B2Gas turbine engine wall assembly with offset railUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 20, 2020·0 cites·11 claims
- 1549US10473330B2Swept combustor liner panels for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Nov 12, 2019·0 cites·8 claims
- 1649US10240793B2Single-fitting, dual-circuit fuel nozzleUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 26, 2019·0 cites·15 claims
- 1749US10041416B2Combustor seal system for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2013·Granted Aug 7, 2018·0 cites·18 claims
- 1846US10190504B2Combustor seal mistake-proofing for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jan 29, 2019·0 cites·13 claims
- 1946US2005074373A1Retainer for buttressing an element and a method for producing the retainerFiled 2004·Application pending·0 cites
- 2046US2015260399A1Combustor section of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2013·Application pending·0 cites
- 2143US2010242483A1Combustor for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2009·Application pending·0 cites
- 2242US2003124036A1Retainer for buttressing an element and a method for producing the retainerFiled 2002·Application pending·0 cites
- 2340US10260750B2Combustor panels having angled railUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 16, 2019·0 cites·12 claims
- 2440US2016017755A1Common joint for a combustor, diffuser, and tobi of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2013·Application pending·0 cites
- 2539US2015241067A1Fastened joint for a tangential on board injectorUNITED TECHNOLOGIES CORP·Filed 2013·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →