Inventor · disambiguated record
Kari Heikurinen
Also filed as: HEIKURINEN KARI · HEIKURINEN KARI J
13 granted patents·140 citations·filing 1988–2019
91Inventor score
Top patents by PatentIndex Score
13 records- 0194US10865806B2Mistuned rotor for gas turbine enginePRATT & WHITNEY CANADA·Filed 2017·Granted Dec 15, 2020·10 cites·14 claims
- 0294US9303589B2Low hub-to-tip ratio fan for a turbofan gas turbine enginePRATT & WHITNEY CANADA·Filed 2012·Granted Apr 5, 2016·16 cites·15 claims
- 0392US8043063B2Intentionally mistuned integrally bladed rotorPRATT & WHITNEY CANADA·Filed 2009·Granted Oct 25, 2011·44 cites·13 claims
- 0484US8100655B2Method of machining airfoil root filletsSTONE PAUL·Filed 2008·Granted Jan 24, 2012·18 cites·10 claims
- 0582US10443411B2Compressor rotor with coated bladesPRATT & WHITNEY CANADA·Filed 2017·Granted Oct 15, 2019·3 cites·20 claims
- 0681US11002293B2Mistuned compressor rotor with hub scoopsPRATT & WHITNEY CANADA·Filed 2017·Granted May 11, 2021·3 cites·19 claims
- 0780US10689987B2Compressor rotor with coated bladesPRATT & WHITNEY CANADA·Filed 2019·Granted Jun 23, 2020·2 cites·20 claims
- 0879US10370973B2Compressor airfoil with compound leading edge profilePRATT & WHITNEY CANADA·Filed 2015·Granted Aug 6, 2019·5 cites·16 claims
- 0975US10837459B2Mistuned fan for gas turbine enginePRATT & WHITNEY CANADA·Filed 2017·Granted Nov 17, 2020·2 cites·33 claims
- 1075US10408231B2Rotor with non-uniform blade tip clearancePRATT & WHITNEY CANADA·Filed 2017·Granted Sep 10, 2019·2 cites·20 claims
- 1175US10408223B2Low hub-to-tip ratio fan for a turbofan gas turbine enginePRATT & WHITNEY CANADA·Filed 2017·Granted Sep 10, 2019·1 cites·19 claims
- 1274US4844695AVariable flow radial compressor inlet flow fencesPRATT & WHITNEY CANADA·Filed 1988·Granted Jul 4, 1989·33 cites·11 claims
- 1355US9759230B2Multistage axial flow compressorPRATT & WHITNEY CANADA·Filed 2014·Granted Sep 12, 2017·1 cites·21 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →