Inventor
MCKINNEY RANDAL G
US15 patents
⚠️ This page may combine multiple inventors who share the name “MCKINNEY RANDAL G”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
12 patentsUS6412272B1Jul 2, 2002
Fuel nozzle guide for gas turbine engine and method of assembly/disassembly
UNITED TECHNOLOGIES CORP57 citations92
US6032457AMar 7, 2000
Fuel nozzle guide
UNITED TECHNOLOGIES CORP45 citations91
US9797601B2Oct 24, 2017
Bluff body fuel mixer
UNITED TECHNOLOGIES CORP6 citations83
US11143407B2Oct 12, 2021
Combustor with axial staging for a gas turbine engine
UNITED TECHNOLOGIES CORP3 citations72
US10794595B2Oct 6, 2020
Stepped heat shield for a turbine engine combustor
UNITED TECHNOLOGIES CORP4 citations72
US10697636B2Jun 30, 2020
Cooling a combustor heat shield proximate a quench aperture
UNITED TECHNOLOGIES CORP1 citations62
US11112115B2Sep 7, 2021
Contoured dilution passages for gas turbine engine combustor
UNITED TECHNOLOGIES CORP0 citations52
US10260748B2Apr 16, 2019
Gas turbine engine combustor with tailored temperature profile
UNITED TECHNOLOGIES CORP0 citations52
US10935243B2Mar 2, 2021
Regulated combustor liner panel for a gas turbine engine combustor
UNITED TECHNOLOGIES CORP0 citations51
US10816209B2Oct 27, 2020
Bluff body fuel mixer
UNITED TECHNOLOGIES CORP0 citations51
US10066836B2Sep 4, 2018
Gas turbine engine systems and methods involving enhanced fuel dispersion
UNITED TECHNOLOGIES CORP1 citations51
US10907833B2Feb 2, 2021
Axial staged combustor with restricted main fuel injector
UNITED TECHNOLOGIES CORP0 citations49