Inventor · disambiguated record
Nurhak Erbas-Sen
Also filed as: ERBAS-SEN NURHAK
16 granted patents·3 pending applications·135 citations·filing 2012–2020
93Inventor score
Top patents by PatentIndex Score
19 records- 0197US9335050B2Gas turbine engine combustorCUNHA FRANK J·Filed 2012·Granted May 10, 2016·31 cites·19 claims
- 0293US9243801B2Combustor liner with improved film coolingCUNHA FRANK J·Filed 2012·Granted Jan 26, 2016·15 cites·16 claims
- 0392US9322560B2Combustor bulkhead assemblyUNITED TECHNOLOGIES CORP·Filed 2012·Granted Apr 26, 2016·14 cites·18 claims
- 0487US10488046B2Gas turbine engine combustor bulkhead assemblyUNITED TECHNOLOGIES CORP·Filed 2014·Granted Nov 26, 2019·9 cites·14 claims
- 0587US9217568B2Combustor liner with decreased liner coolingCUNHA FRANK J·Filed 2012·Granted Dec 22, 2015·9 cites·20 claims
- 0686US9482432B2Gas turbine engine combustor with integrated combustor vane having swirlerCUNHA FRANK J·Filed 2012·Granted Nov 1, 2016·9 cites·17 claims
- 0786US9194585B2Cooling for combustor liners with accelerating channelsUNITED TECHNOLOGIES CORP·Filed 2012·Granted Nov 24, 2015·10 cites·20 claims
- 0884US9052111B2Turbine engine combustor wall with non-uniform distribution of effusion aperturesERBAS-SEN NURHAK·Filed 2012·Granted Jun 9, 2015·11 cites·14 claims
- 0983US9404654B2Gas turbine engine combustor with integrated combustor vaneCUNHA FRANK J·Filed 2012·Granted Aug 2, 2016·7 cites·19 claims
- 1080US9335049B2Combustor liner with reduced cooling dilution openingsCUNHA FRANK J·Filed 2012·Granted May 10, 2016·6 cites·15 claims
- 1175US10047958B2Combustor wall with tapered cooling cavityUNITED TECHNOLOGIES CORP·Filed 2014·Granted Aug 14, 2018·4 cites·22 claims
- 1274US10088159B2Active cooling of grommet bosses for a combustor panel of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 2, 2018·4 cites·15 claims
- 1374US9239165B2Combustor liner with convergent cooling channelCUNHA FRANK J·Filed 2012·Granted Jan 19, 2016·4 cites·19 claims
- 1467US10174949B2Gas turbine engine combustor liner assembly with convergent hyperbolic profileUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jan 8, 2019·2 cites·14 claims
- 1553US10655855B2Gas turbine engine wall assembly with support shell contour regionsUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 19, 2020·0 cites·20 claims
- 1648US11326518B2Cooled component for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2020·Granted May 10, 2022·0 cites·20 claims
- 1748US2016040881A1Gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 1847US2015362192A1Gas turbine engine combustor liner assembly with convergent hyperbolic profileUNITED TECHNOLOGIES CORP·Filed 2013·Application pending·0 cites
- 1947US2014216044A1Gas turbine engine combustor heat shield with increased film cooling effectivenessUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
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