Inventor · disambiguated record
Leissner Ferdinand Poth, Iii
Also filed as: POTH III LEISSNER F · POTH III LEISSNER FERDINAND · POTH LEISSNER F
9 granted patents·1 pending application·17 citations·filing 2009–2023
79Inventor score
Files withMECH DYNAMICS & ANALYSIS LLC4MECH DYNAMICS AND ANALYSIS LLC2MCGOVERN KEVIN T1PW POWER SYSTEMS INC1SCHLEIF KURT KRAMER1
Top patents by PatentIndex Score
10 records- 0170US8133016B2Airfoil profile for a second stage turbine nozzleMCGOVERN KEVIN T·Filed 2009·Granted Mar 13, 2012·15 cites·10 claims
- 0263US12359569B2Turbine blade tip cooling hole supply plenumMECH DYNAMICS AND ANALYSIS LLC·Filed 2023·Granted Jul 15, 2025·0 cites·18 claims
- 0359US9828857B2Repaired or remanufactured blade platform for a gas turbine enginePW POWER SYSTEMS INC·Filed 2014·Granted Nov 28, 2017·2 cites·20 claims
- 0457US10875131B2Repair or remanufacture of blade platform for a gas turbine engineMECH DYNAMICS & ANALYSIS LLC·Filed 2019·Granted Dec 29, 2020·0 cites·20 claims
- 0552US11840940B2Turbine blade tip cooling hole supply plenumMECH DYNAMICS AND ANALYSIS LLC·Filed 2021·Granted Dec 12, 2023·0 cites·21 claims
- 0652US10252380B2Repair or remanufacture of blade platform for a gas turbine engineMECH DYNAMICS & ANALYSIS LLC·Filed 2014·Granted Apr 9, 2019·0 cites·23 claims
- 0745US8690530B2System and method for supporting a nozzle assemblySNOOK DANIEL DAVID·Filed 2011·Granted Apr 8, 2014·0 cites·16 claims
- 0843US11506061B2Ram air turbine blade platform coolingMECH DYNAMICS & ANALYSIS LLC·Filed 2020·Granted Nov 22, 2022·0 cites·24 claims
- 0934US2012128468A1Sensor assembly for use with a turbomachine and methods of assembling sameSCHLEIF KURT KRAMER·Filed 2010·Application pending·0 cites
- 1032US10145249B2Turbine bucket lockwire anti-rotation device for gas turbine engineMECH DYNAMICS & ANALYSIS LLC·Filed 2016·Granted Dec 4, 2018·0 cites·19 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →