Assignee
LEE CHING PANG
US·63 granted patents·6 pending applications·734 citations·filing 2006–2018
Top patents by PatentIndex Score
69 records- 0199US8667682B2Method of fabricating a nearwall nozzle impingement cooled component for an internal combustion engineLEE CHING-PANG·Filed 2011·Granted Mar 11, 2014·46 cites·20 claims
- 0297US8864438B1Flow control insert in cooling passage for turbine vaneLEE CHING-PANG·Filed 2013·Granted Oct 21, 2014·43 cites·11 claims
- 0397US8826668B2Two stage serial impingement cooling for isogrid structuresLEE CHING-PANG·Filed 2011·Granted Sep 9, 2014·30 cites·18 claims
- 0495US8939711B2Outer rim seal assembly in a turbine engineLEE CHING-PANG·Filed 2013·Granted Jan 27, 2015·15 cites·15 claims
- 0595US8936068B2Method of casting a component having interior passagewaysLEE CHING-PANG·Filed 2011·Granted Jan 20, 2015·22 cites·10 claims
- 0695US8920123B2Turbine blade with integrated serpentine and axial tip cooling circuitsLEE CHING-PANG·Filed 2012·Granted Dec 30, 2014·20 cites·14 claims
- 0795US8840363B2Trailing edge cooling system in a turbine airfoil assemblyLEE CHING-PANG·Filed 2011·Granted Sep 23, 2014·19 cites·20 claims
- 0895US8727704B2Ring segment with serpentine cooling passagesLEE CHING-PANG·Filed 2011·Granted May 20, 2014·33 cites·20 claims
- 0994US8944763B2Turbine blade cooling system with bifurcated mid-chord cooling chamberLEE CHING-PANG·Filed 2011·Granted Feb 3, 2015·19 cites·19 claims
- 1094US8684691B2Turbine blade with chamfered squealer tip and convective cooling holesLEE CHING-PANG·Filed 2011·Granted Apr 1, 2014·26 cites·20 claims
- 1193US9017025B2Serpentine cooling circuit with T-shaped partitions in a turbine airfoilLEE CHING-PANG·Filed 2011·Granted Apr 28, 2015·15 cites·8 claims
- 1293US8894367B2Compound cooling flow turbulator for turbine componentLEE CHING-PANG·Filed 2010·Granted Nov 25, 2014·15 cites·2 claims
- 1393US8827632B1Integrated TBC and cooling flow metering plate in turbine vaneLEE CHING-PANG·Filed 2013·Granted Sep 9, 2014·25 cites·16 claims
- 1492US9234438B2Turbine engine component wall having branched cooling passagesLEE CHING-PANG·Filed 2012·Granted Jan 12, 2016·15 cites·17 claims
- 1592US9039357B2Seal assembly including grooves in a radially outwardly facing side of a platform in a gas turbine engineLEE CHING-PANG·Filed 2013·Granted May 26, 2015·14 cites·20 claims
- 1692US8721291B2Flow directing member for gas turbine engineLEE CHING-PANG·Filed 2011·Granted May 13, 2014·18 cites·18 claims
- 1792US8714926B2Turbine component cooling channel mesh with intersection chambersLEE CHING-PANG·Filed 2010·Granted May 6, 2014·13 cites·19 claims
- 1891US8668453B2Cooling system having reduced mass pin fins for components in a gas turbine engineLEE CHING-PANG·Filed 2011·Granted Mar 11, 2014·13 cites·14 claims
- 1990US8884182B2Method of modifying the end wall contour in a turbine using laser consolidation and the turbines derived therefromLEE CHING-PANG·Filed 2006·Granted Nov 11, 2014·19 cites·17 claims
- 2089US9347324B2Turbine airfoil vane with an impingement insert having a plurality of impingement nozzlesLEE CHING-PANG·Filed 2013·Granted May 24, 2016·11 cites·19 claims
- 2188US9630277B2Airfoil having built-up surface with embedded cooling passageLEE CHING-PANG·Filed 2010·Granted Apr 25, 2017·12 cites·18 claims
- 2288US9132476B2Multi-wall gas turbine airfoil cast using a ceramic core formed with a fugitive insert and method of manufacturing sameLEE CHING-PANG·Filed 2013·Granted Sep 15, 2015·4 cites·7 claims
- 2388US9057276B2Twisted gas turbine engine airfoil having a twisted ribLEE CHING-PANG·Filed 2013·Granted Jun 16, 2015·10 cites·16 claims
- 2488US8920124B2Turbine blade with contoured chamfered squealer tipLEE CHING-PANG·Filed 2013·Granted Dec 30, 2014·10 cites·19 claims
- 2588US8764394B2Component cooling channelLEE CHING-PANG·Filed 2011·Granted Jul 1, 2014·10 cites·18 claims
- 2687US8608443B2Film cooled component wall in a turbine engineLEE CHING-PANG·Filed 2010·Granted Dec 17, 2013·11 cites·20 claims
- 2787US8535006B2Near-wall serpentine cooled turbine airfoilLEE CHING-PANG·Filed 2010·Granted Sep 17, 2013·9 cites·20 claims
- 2885US9022736B2Integrated axial and tangential serpentine cooling circuit in a turbine airfoilLEE CHING-PANG·Filed 2011·Granted May 5, 2015·10 cites·6 claims
- 2985US8985949B2Cooling system including wavy cooling chamber in a trailing edge portion of an airfoil assemblyLEE CHING-PANG·Filed 2013·Granted Mar 24, 2015·10 cites·18 claims
- 3085US8104292B2Duplex turbine shroudLEE CHING-PANG·Filed 2007·Granted Jan 31, 2012·31 cites·23 claims
- 3184US9091495B2Cooling passage including turbulator system in a turbine engine componentLEE CHING-PANG·Filed 2013·Granted Jul 28, 2015·8 cites·16 claims
- 3283US9181819B2Component wall having diffusion sections for cooling in a turbine engineLEE CHING-PANG·Filed 2010·Granted Nov 10, 2015·9 cites·18 claims
- 3383US9121298B2Finned seal assembly for gas turbine enginesLEE CHING-PANG·Filed 2012·Granted Sep 1, 2015·9 cites·20 claims
- 3483US8926283B2Turbine blade angel wing with pumping featuresLEE CHING-PANG·Filed 2012·Granted Jan 6, 2015·8 cites·18 claims
- 3583US8926267B2Ambient air cooling arrangement having a pre-swirler for gas turbine engine blade coolingLEE CHING-PANG·Filed 2013·Granted Jan 6, 2015·9 cites·18 claims
- 3683US8920122B2Turbine airfoil with an internal cooling system having vortex forming turbulatorsLEE CHING-PANG·Filed 2012·Granted Dec 30, 2014·8 cites·8 claims
- 3783US8413709B2Composite core die, methods of manufacture thereof and articles manufactured therefromLEE CHING-PANG·Filed 2006·Granted Apr 9, 2013·8 cites·11 claims
- 3883US8205458B2Duplex turbine nozzleLEE CHING-PANG·Filed 2007·Granted Jun 26, 2012·15 cites·24 claims
- 3981US8973372B2Combustor shell air recirculation system in a gas turbine engineLEE CHING-PANG·Filed 2012·Granted Mar 10, 2015·8 cites·18 claims
- 4081US8920111B2Airfoil incorporating tapered cooling structures defining cooling passagewaysLEE CHING-PANG·Filed 2010·Granted Dec 30, 2014·7 cites·18 claims
- 4181US8894363B2Cooling module design and method for cooling components of a gas turbine systemLEE CHING-PANG·Filed 2011·Granted Nov 25, 2014·7 cites·12 claims
- 4280US9004866B2Turbine blade incorporating trailing edge cooling designLEE CHING-PANG·Filed 2011·Granted Apr 14, 2015·7 cites·15 claims
- 4380US8820090B2Method for operating a gas turbine engine including a combustor shell air recirculation systemLEE CHING-PANG·Filed 2012·Granted Sep 2, 2014·8 cites·18 claims
- 4479US9120144B2Casting core for twisted gas turbine engine airfoil having a twisted ribLEE CHING-PANG·Filed 2013·Granted Sep 1, 2015·6 cites·20 claims
- 4578US9546558B2Damping resonator with impingement coolingLEE CHING-PANG·Filed 2010·Granted Jan 17, 2017·6 cites·20 claims
- 4678US9039371B2Trailing edge cooling using angled impingement on surface enhanced with cast chevron arrangementsLEE CHING-PANG·Filed 2013·Granted May 26, 2015·6 cites·18 claims
- 4778US8425183B2Triforial tip cavity airfoilLEE CHING-PANG·Filed 2006·Granted Apr 23, 2013·12 cites·28 claims
- 4877US8951004B2Cooling arrangement for a gas turbine componentLEE CHING-PANG·Filed 2012·Granted Feb 10, 2015·5 cites·15 claims
- 4976US8939717B1Vane outer support ring with no forward hook in a compressor section of a gas turbine engineLEE CHING-PANG·Filed 2013·Granted Jan 27, 2015·4 cites·15 claims
- 5076US8936067B2Casting core for a cooling arrangement for a gas turbine componentLEE CHING-PANG·Filed 2012·Granted Jan 20, 2015·5 cites·20 claims
Showing the top 50 of 69 patent records by PatentIndex Score.
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