Inventor
ERBAS-SEN NURHAK
US16 patents
⚠️ This page may combine multiple inventors who share the name “ERBAS-SEN NURHAK”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
8 patentsUS9322560B2Apr 26, 2016
Combustor bulkhead assembly
UNITED TECHNOLOGIES CORP14 citations84
US9194585B2Nov 24, 2015
Cooling for combustor liners with accelerating channels
UNITED TECHNOLOGIES CORP10 citations82
US10488046B2Nov 26, 2019
Gas turbine engine combustor bulkhead assembly
UNITED TECHNOLOGIES CORP9 citations81
US10174949B2Jan 8, 2019
Gas turbine engine combustor liner assembly with convergent hyperbolic profile
UNITED TECHNOLOGIES CORP2 citations73
US10047958B2Aug 14, 2018
Combustor wall with tapered cooling cavity
UNITED TECHNOLOGIES CORP4 citations73
US10088159B2Oct 2, 2018
Active cooling of grommet bosses for a combustor panel of a gas turbine engine
UNITED TECHNOLOGIES CORP4 citations72
US10655855B2May 19, 2020
Gas turbine engine wall assembly with support shell contour regions
UNITED TECHNOLOGIES CORP0 citations51
US11326518B2May 10, 2022
Cooled component for a gas turbine engine
UNITED TECHNOLOGIES CORP0 citations46
CUNHA FRANK J
7 patentsUS9335050B2May 10, 2016
Gas turbine engine combustor
CUNHA FRANK J31 citations93
US9482432B2Nov 1, 2016
Gas turbine engine combustor with integrated combustor vane having swirler
CUNHA FRANK J9 citations83
US9404654B2Aug 2, 2016
Gas turbine engine combustor with integrated combustor vane
CUNHA FRANK J7 citations83
US9243801B2Jan 26, 2016
Combustor liner with improved film cooling
CUNHA FRANK J15 citations83
US9217568B2Dec 22, 2015
Combustor liner with decreased liner cooling
CUNHA FRANK J9 citations83
US9335049B2May 10, 2016
Combustor liner with reduced cooling dilution openings
CUNHA FRANK J6 citations72
US9239165B2Jan 19, 2016
Combustor liner with convergent cooling channel
CUNHA FRANK J4 citations72