Inventor · disambiguated record
David Allen Flodman
Also filed as: FLODMAN DAVID ALLEN
11 granted patents·1 pending application·121 citations·filing 2001–2022
88Inventor score
Top patents by PatentIndex Score
12 records- 0195US11536149B1Cooling method and structure of vane of gas turbineMITSUBISHI HEAVY IND LTD·Filed 2022·Granted Dec 27, 2022·3 cites·20 claims
- 0287US6595748B2Trichannel airfoil leading edge coolingGEN ELECTRIC·Filed 2001·Granted Jul 22, 2003·58 cites·29 claims
- 0376US10724391B2Engine component with flow enhancerGEN ELECTRIC·Filed 2017·Granted Jul 28, 2020·2 cites·27 claims
- 0476US7377743B2Countercooled turbine nozzleGEN ELECTRIC·Filed 2005·Granted May 27, 2008·16 cites·25 claims
- 0574US7946801B2Multi-source gas turbine coolingGEN ELECTRIC·Filed 2007·Granted May 24, 2011·11 cites·19 claims
- 0663US8172504B2Hybrid impingement cooled airfoilFLODMAN DAVID ALLEN·Filed 2008·Granted May 8, 2012·11 cites·16 claims
- 0758US12331662B2Structure of cooling turbine vane shroud and manufacturing method thereofMITSUBISHI HEAVY IND LTD·Filed 2022·Granted Jun 17, 2025·0 cites·16 claims
- 0856US7246999B2Stepped outlet turbine airfoilGEN ELECTRIC·Filed 2004·Granted Jul 24, 2007·15 cites·23 claims
- 0947US12305532B2Cooling method and structure of vane of gas turbineMITSUBISHI HEAVY IND LTD·Filed 2022·Granted May 20, 2025·0 cites·12 claims
- 1046US11982206B2Cooling method and structure of vane of gas turbineMITSUBISHI HEAVY IND LTD·Filed 2022·Granted May 14, 2024·0 cites·18 claims
- 1141US6694742B2Gas turbine system operation based on estimated stressGEN ELECTRIC·Filed 2002·Granted Feb 24, 2004·5 cites·16 claims
- 1240US2009220331A1Turbine nozzle with integral impingement blanketGEN ELECTRIC·Filed 2008·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →