Inventor · disambiguated record
Kenneth K. Landis
Also filed as: LANDIS KENNETH · LANDIS KENNETH K
10 granted patents·4 pending applications·235 citations·filing 1987–2015
90Inventor score
Files withUNITED TECHNOLOGIES CORP4BRUNELLI MARCO CLAUDIO PIO2FLORIDA TURBINE TECH INC2SIEMENS POWER GENERATION INC2CHARRON RICHARD C1
Top patents by PatentIndex Score
14 records- 0189US4767268ATriple pass cooled airfoilUNITED TECHNOLOGIES CORP·Filed 1987·Granted Aug 30, 1988·83 cites·7 claims
- 0286US7500828B2Airfoil having porous metal filled cavitiesFLORIDA TURBINE TECH INC·Filed 2005·Granted Mar 10, 2009·28 cites·11 claims
- 0384US8061988B1Process for conjugate CFD analysis of a turbine airfoilRAWLINGS CHRISTOPHER K·Filed 2007·Granted Nov 22, 2011·16 cites·13 claims
- 0481US9017012B2Ring segment with cooling fluid supply trenchBRUNELLI MARCO CLAUDIO PIO·Filed 2011·Granted Apr 28, 2015·13 cites·19 claims
- 0569US8015817B2Cooling structure for gas turbine transition ductSIEMENS ENERGY INC·Filed 2009·Granted Sep 13, 2011·12 cites·18 claims
- 0668US4859147ACooled gas turbine bladeUNITED TECHNOLOGIES CORP·Filed 1988·Granted Aug 22, 1989·36 cites·5 claims
- 0761US7422417B2Airfoil with a porous fiber metal layerFLORIDA TURBINE TECH INC·Filed 2005·Granted Sep 9, 2008·7 cites·24 claims
- 0860US7118325B2Cooling passageway turnUNITED TECHNOLOGIES CORP·Filed 2004·Granted Oct 10, 2006·18 cites·30 claims
- 0958US4827587AMethod of fabricating an air cooled turbine bladeUNITED TECHNOLOGIES CORP·Filed 1988·Granted May 9, 1989·22 cites·12 claims
- 1040US9097117B2Turbine transition component formed from an air-cooled multi-layer outer panel for use in a gas turbine engineCHARRON RICHARD C·Filed 2010·Granted Aug 4, 2015·0 cites·14 claims
- 1134US2007258814A1Turbine airfoil with integral chordal support ribsSIEMENS POWER GENERATION INC·Filed 2006·Application pending·0 cites
- 1233US2007160475A1Tilted turbine vane with impingement coolingSIEMENS POWER GENERATION INC·Filed 2006·Application pending·0 cites
- 1331US2014286751A1Cooled turbine ring segments with intermediate pressure plenumsBRUNELLI MARCO CLAUDIO PIO·Filed 2013·Application pending·0 cites
- 1430US2018023404A1Ring segment system for gas turbine enginesSIEMENS AG·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →