Inventor · disambiguated record
Randal G. Mckinney
Also filed as: MCKINNEY RANDAL G
15 granted patents·1 pending application·158 citations·filing 1996–2019
91Inventor score
Top patents by PatentIndex Score
16 records- 0192US9797601B2Bluff body fuel mixerUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 24, 2017·6 cites·16 claims
- 0286US8966877B2Gas turbine combustor with variable airflowMCKINNEY RANDAL G·Filed 2010·Granted Mar 3, 2015·12 cites·10 claims
- 0386US6412272B1Fuel nozzle guide for gas turbine engine and method of assembly/disassemblyUNITED TECHNOLOGIES CORP·Filed 1999·Granted Jul 2, 2002·57 cites·19 claims
- 0484US10794595B2Stepped heat shield for a turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 6, 2020·4 cites·16 claims
- 0581US6032457AFuel nozzle guideUNITED TECHNOLOGIES CORP·Filed 1996·Granted Mar 7, 2000·45 cites·15 claims
- 0679US8109099B2Flow sleeve with tabbed direct combustion liner cooling airTU JOHN S·Filed 2008·Granted Feb 7, 2012·21 cites·5 claims
- 0770US11143407B2Combustor with axial staging for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 12, 2021·3 cites·20 claims
- 0867US9115897B2Gas turbine engine systems and methods involving enhanced fuel dispersionSNYDER TIMOTHY S·Filed 2008·Granted Aug 25, 2015·8 cites·16 claims
- 0965US10066836B2Gas turbine engine systems and methods involving enhanced fuel dispersionUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 4, 2018·1 cites·8 claims
- 1062US10816209B2Bluff body fuel mixerUNITED TECHNOLOGIES CORP·Filed 2017·Granted Oct 27, 2020·0 cites·9 claims
- 1161US2020025376A1Gas turbine engine combustor with tailored temperature profileUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 1260US10697636B2Cooling a combustor heat shield proximate a quench apertureUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 30, 2020·1 cites·10 claims
- 1352US10260748B2Gas turbine engine combustor with tailored temperature profileUNITED TECHNOLOGIES CORP·Filed 2012·Granted Apr 16, 2019·0 cites·1 claims
- 1450US10935243B2Regulated combustor liner panel for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2016·Granted Mar 2, 2021·0 cites·10 claims
- 1549US11112115B2Contoured dilution passages for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 7, 2021·0 cites·14 claims
- 1645US10907833B2Axial staged combustor with restricted main fuel injectorUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 2, 2021·0 cites·20 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →