Inventor · disambiguated record
Ghislain Plante
Also filed as: PLANTE GHISLAIN
27 granted patents·4 pending applications·80 citations·filing 2005–2023
94Inventor score
Top patents by PatentIndex Score
31 records- 0194US10533559B2Reverse flow engine architecturePRATT & WHITNEY CANADA·Filed 2016·Granted Jan 14, 2020·9 cites·18 claims
- 0291US10961919B2Corrected parameters control logic for variable geometry mechanismsPRATT & WHITNEY CANADA·Filed 2018·Granted Mar 30, 2021·5 cites·18 claims
- 0388US11408352B2Reverse-flow gas turbine enginePRATT & WHITNEY CANADA·Filed 2020·Granted Aug 9, 2022·2 cites·17 claims
- 0484US9376921B2Internally cooled gas turbine engine airfoilPRATT & WHITNEY CANADA·Filed 2012·Granted Jun 28, 2016·7 cites·14 claims
- 0582US9121289B2High pressure turbine blade cooling hole distributionPRATT & WHITNEY CANADA·Filed 2012·Granted Sep 1, 2015·9 cites·20 claims
- 0680US11199096B1Turbomachine bladeUNITED TECHNOLOGIES CORP·Filed 2018·Granted Dec 14, 2021·3 cites·13 claims
- 0777US8267663B2Multi-cast turbine airfoils and method for making sameLAROSE JOEL·Filed 2008·Granted Sep 18, 2012·21 cites·16 claims
- 0875US10808624B2Turbine rotor with low over-speed requirementsPRATT & WHITNEY CANADA·Filed 2017·Granted Oct 20, 2020·2 cites·12 claims
- 0975US10190423B2Shrouded blade for a gas turbine enginePRATT & WHITNEY CANADA·Filed 2016·Granted Jan 29, 2019·2 cites·14 claims
- 1074US11668245B2Gas turbine engine with clutch system between low-pressure compressor and low-pressure turbinePRATT & WHITNEY CANADA·Filed 2020·Granted Jun 6, 2023·1 cites·13 claims
- 1173US11773785B2Reverse-flow gas turbine enginePRATT & WHITNEY CANADA·Filed 2023·Granted Oct 3, 2023·0 cites·16 claims
- 1273US11415063B2Reverse-flow gas turbine enginePRATT & WHITNEY CANADA·Filed 2016·Granted Aug 16, 2022·1 cites·20 claims
- 1372US11555453B2Reverse-flow gas turbine enginePRATT & WHITNEY CANADA·Filed 2021·Granted Jan 17, 2023·0 cites·19 claims
- 1472US10473038B2Power plant thrust management system for turboprop enginesPRATT & WHITNEY CANADA·Filed 2017·Granted Nov 12, 2019·2 cites·20 claims
- 1571US12467412B2Gas turbine engine with clutch system between low-pressure compressor and low-pressure turbinePRATT & WHITNEY CANADA·Filed 2023·Granted Nov 11, 2025·0 cites·7 claims
- 1670US11719247B2Reverse flow engine architecturePRATT & WHITNEY CANADA·Filed 2021·Granted Aug 8, 2023·0 cites·8 claims
- 1769US9879550B2Outer shroud with gussetPRATT & WHITNEY CANADA·Filed 2014·Granted Jan 30, 2018·3 cites·20 claims
- 1868US9638046B2Airfoil with variable land width at trailing edgePRATT & WHITNEY CANADA·Filed 2014·Granted May 2, 2017·3 cites·20 claims
- 1965US12116940B2Corrected parameters control logic for variable geometry mechanismsPRATT & WHITNEY CANADA·Filed 2021·Granted Oct 15, 2024·0 cites·19 claims
- 2064US11125239B2Reverse flow engine architecturePRATT & WHITNEY CANADA·Filed 2019·Granted Sep 21, 2021·0 cites·9 claims
- 2161US7357623B2Angled cooling divider wall in blade attachmentPRATT & WHITNEY CANADA·Filed 2005·Granted Apr 15, 2008·9 cites·15 claims
- 2257US9556741B2Shrouded blade for a gas turbine enginePRATT & WHITNEY CANADA·Filed 2014·Granted Jan 31, 2017·1 cites·9 claims
- 2354US10221695B2Internally cooled gas turbine engine airfoilPRATT & WHITNEY CANADA·Filed 2016·Granted Mar 5, 2019·0 cites·16 claims
- 2452US11578663B2Engine family platform designPRATT & WHITNEY CANADA·Filed 2019·Granted Feb 14, 2023·0 cites·9 claims
- 2548US11629665B2Gas turbine engine and method of creating classes of samePRATT & WHITNEY CANADA·Filed 2019·Granted Apr 18, 2023·0 cites·32 claims
- 2647US10598023B2Power turbine blade airfoil profilePRATT & WHITNEY CANADA·Filed 2017·Granted Mar 24, 2020·0 cites·8 claims
- 2747US2022074349A1Split compressor gas turbine enginePRATT & WHITNEY CANADA·Filed 2020·Application pending·0 cites
- 2844US11994034B2Gas turbine engine with low pressure compressor stagesPRATT & WHITNEY CANADA·Filed 2018·Granted May 28, 2024·0 cites·11 claims
- 2943US2018135525A1Gas turbine engine tangential orifice bleed configurationPRATT & WHITNEY CANADA·Filed 2016·Application pending·0 cites
- 3043US2020080476A1Spilt compressor system on multi-spool enginePRATT & WHITNEY CANADA·Filed 2018·Application pending·0 cites
- 3141US2018216525A1Gas turbine engine architecture with split compressor systemPRATT & WHITNEY CANADA·Filed 2017·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →