Inventor · disambiguated record
Corneil S. Paauwe
Also filed as: PAAUWE CORNEIL · PAAUWE CORNEIL S
9 granted patents·6 pending applications·88 citations·filing 2004–2019
87Inventor score
Top patents by PatentIndex Score
15 records- 0189US7220934B2Method of producing cooling holes in highly contoured airfoilsUNITED TECHNOLOGIES CORP·Filed 2005·Granted May 22, 2007·11 cites·11 claims
- 0278US8092179B2Blade tip cooling groovePAAUWE CORNEIL S·Filed 2009·Granted Jan 10, 2012·20 cites·20 claims
- 0375US7600966B2Turbine airfoil with improved coolingUNITED TECHNOLOGIES CORP·Filed 2006·Granted Oct 13, 2009·15 cites·22 claims
- 0470US8240981B2Turbine airfoil with platform coolingSPANGLER BRANDON W·Filed 2007·Granted Aug 14, 2012·13 cites·24 claims
- 0569US8206114B2Gas turbine engine systems involving turbine blade platforms with cooling holesSPANGLER BRANDON W·Filed 2008·Granted Jun 26, 2012·12 cites·16 claims
- 0666US7465154B2Gas turbine engine component suction side trailing edge cooling schemeUNITED TECHNOLOGIES CORP·Filed 2006·Granted Dec 16, 2008·11 cites·18 claims
- 0755US11149556B2Minicore cooling passage network having sloped impingement surfaceUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 19, 2021·0 cites·17 claims
- 0844US9322285B2Large fillet airfoil with fanned cooling hole arrayDEVORE MATTHEW A·Filed 2008·Granted Apr 26, 2016·1 cites·7 claims
- 0941US7431559B2Dirt separation for impingement cooled turbine componentsUNITED TECHNOLOGIES CORP·Filed 2004·Granted Oct 7, 2008·5 cites·21 claims
- 1040US2020348023A1Combustor liner panel with micro-circuit core coolingUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 1139US2009096174A1Blade outer air seal for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2007·Application pending·0 cites
- 1238US2008031739A1Airfoil with customized convective coolingUNITED TECHNOLOGIES CORP·Filed 2006·Application pending·0 cites
- 1337US2010310367A1Impingement cooling of a turbine airfoil with large platform to airfoil fillet radiusUNITED TECHNOLOGIES CORP·Filed 2006·Application pending·0 cites
- 1435US2016160652A1Cooled pocket in a turbine vane platformUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 1534US2007212214A1Segmented component sealUNITED TECHNOLOGIES CORP·Filed 2006·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →