Inventor · disambiguated record
Jae Y. Um
Also filed as: UM JAE · UM JAE Y · UM JAE YONG
13 granted patents·7 pending applications·110 citations·filing 2002–2018
90Inventor score
Files withSIEMENS AG8LEE CHING PANG5SIEMENS ENERGY INC3GEN ELECTRIC2SIEMENS ENERGY GLOBAL GMBH & CO KG1
Top patents by PatentIndex Score
20 records- 0192US9840930B2Internal cooling system with insert forming nearwall cooling channels in midchord cooling cavities of a gas turbine airfoilSIEMENS AG·Filed 2014·Granted Dec 12, 2017·25 cites·14 claims
- 0288US9630277B2Airfoil having built-up surface with embedded cooling passageLEE CHING-PANG·Filed 2010·Granted Apr 25, 2017·12 cites·18 claims
- 0387US8608443B2Film cooled component wall in a turbine engineLEE CHING-PANG·Filed 2010·Granted Dec 17, 2013·11 cites·20 claims
- 0483US9863256B2Internal cooling system with insert forming nearwall cooling channels in an aft cooling cavity of an airfoil usable in a gas turbine engineSIEMENS AG·Filed 2014·Granted Jan 9, 2018·9 cites·12 claims
- 0583US9181819B2Component wall having diffusion sections for cooling in a turbine engineLEE CHING-PANG·Filed 2010·Granted Nov 10, 2015·9 cites·18 claims
- 0677US9745853B2Integrated circuit cooled turbine bladeSIEMENS ENERGY INC·Filed 2015·Granted Aug 29, 2017·3 cites·19 claims
- 0775US9963996B2Shroud cooling system for shrouds adjacent to airfoils within gas turbine enginesSIEMENS AG·Filed 2014·Granted May 8, 2018·5 cites·10 claims
- 0875US6679680B2Built-up gas turbine component and its fabricationGEN ELECTRIC·Filed 2002·Granted Jan 20, 2004·33 cites·19 claims
- 0974US9061349B2Investment casting method for gas turbine engine vane segmentLEE CHING-PANG·Filed 2013·Granted Jun 23, 2015·1 cites·16 claims
- 1052US10697306B2Gas turbine airfoil including integrated leading edge and tip cooling fluid passage and core structure used for forming such an airfoilSIEMENS AG·Filed 2014·Granted Jun 30, 2020·1 cites·5 claims
- 1151US6679757B2Shaping tool and method for shaping curved surfaces on workpiecesGEN ELECTRIC·Filed 2002·Granted Jan 20, 2004·1 cites·26 claims
- 1249US2015122450A1Ceramic casting core having an integral vane internal core and shroud backside shell for vane segment castingLEE CHING-PANG·Filed 2013·Application pending·0 cites
- 1347US2015239043A1Cast Features for Location and InspectionSIEMENS ENERGY INC·Filed 2014·Application pending·0 cites
- 1443US11415000B2Turbine airfoil with trailing edge features and casting coreSIEMENS ENERGY GLOBAL GMBH & CO KG·Filed 2018·Granted Aug 16, 2022·0 cites·11 claims
- 1543US2015198050A1Internal cooling system with corrugated insert forming nearwall cooling channels for airfoil usable in a gas turbine engineSIEMENS ENERGY INC·Filed 2014·Application pending·0 cites
- 1642US11111795B2Turbine rotor airfoil and corresponding method for reducing pressure loss in a cavity within a bladeSIEMENS AG·Filed 2018·Granted Sep 7, 2021·0 cites·9 claims
- 1740US2015204197A1Airfoil leading edge chamber cooling with angled impingementSIEMENS AG·Filed 2014·Application pending·0 cites
- 1840US2018298763A1Turbine blade with axial tip cooling circuitSIEMENS AG·Filed 2014·Application pending·0 cites
- 1934US2018045059A1Internal cooling system with insert forming nearwall cooling channels in an aft cooling cavity of a gas turbine airfoil including heat dissipating ribsSIEMENS AG·Filed 2015·Application pending·0 cites
- 2034US2007258814A1Turbine airfoil with integral chordal support ribsSIEMENS POWER GENERATION INC·Filed 2006·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →