Inventor · disambiguated record
James Harvey Laflen
Also filed as: LAFLEN JAMES H · LAFLEN JAMES HARVEY
11 granted patents·187 citations·filing 1999–2008
92Inventor score
Top patents by PatentIndex Score
11 records- 0182US7604453B2Methods and system for recuperated circumferential cooling of integral turbine nozzle and shroud assembliesGEN ELECTRIC·Filed 2006·Granted Oct 20, 2009·22 cites·20 claims
- 0281US7740444B2Methods and system for cooling integral turbine shround assembliesGEN ELECTRIC·Filed 2006·Granted Jun 22, 2010·23 cites·20 claims
- 0378US7785067B2Method and system to facilitate cooling turbine enginesGEN ELECTRIC·Filed 2006·Granted Aug 31, 2010·19 cites·15 claims
- 0476US8147192B2Dual stage turbine shroudJONES DANIEL VERN·Filed 2008·Granted Apr 3, 2012·19 cites·21 claims
- 0576US7722315B2Method and system to facilitate preferentially distributed recuperated film cooling of turbine shroud assemblyGEN ELECTRIC·Filed 2006·Granted May 25, 2010·12 cites·17 claims
- 0673US7665953B2Methods and system for recuperated cooling of integral turbine nozzle and shroud assembliesGEN ELECTRIC·Filed 2006·Granted Feb 23, 2010·10 cites·17 claims
- 0772US7740442B2Methods and system for cooling integral turbine nozzle and shroud assembliesGEN ELECTRIC·Filed 2006·Granted Jun 22, 2010·12 cites·20 claims
- 0869US8226360B2Crenelated turbine nozzleSCOGGINS PATRICK JARVIS·Filed 2008·Granted Jul 24, 2012·15 cites·26 claims
- 0965US7690885B2Methods and system for shielding cooling air to facilitate cooling integral turbine nozzle and shroud assembliesGEN ELECTRIC·Filed 2006·Granted Apr 6, 2010·10 cites·20 claims
- 1064US6158962ATurbine blade with ribbed platformGEN ELECTRIC·Filed 1999·Granted Dec 12, 2000·37 cites·12 claims
- 1163US7611324B2Method and system to facilitate enhanced local cooling of turbine enginesGEN ELECTRIC·Filed 2006·Granted Nov 3, 2009·8 cites·20 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →