Inventor · disambiguated record
Franco Di Paola
Also filed as: DI PAOLA FRANCO
21 granted patents·4 pending applications·217 citations·filing 2002–2024
94Inventor score
Files withPRATT & WHITNEY CANADA18DI PAOLA FRANCO3LECUYER DANIEL2MARTIN YVES1PRATT & WHITNEY CANADA CCORP1
Top patents by PatentIndex Score
25 records- 0195US11629596B1Rotor assembly for a gas turbine engine and method for assembling samePRATT & WHITNEY CANADA·Filed 2021·Granted Apr 18, 2023·7 cites·17 claims
- 0290US8684680B2Sealing and cooling at the joint between shroud segmentsMARTIN YVES·Filed 2009·Granted Apr 1, 2014·36 cites·14 claims
- 0390US8246305B2Gas turbine engine balancingLECUYER DANIEL·Filed 2009·Granted Aug 21, 2012·32 cites·9 claims
- 0488US11414993B1Retaining assembly with anti-rotation featurePRATT & WHITNEY CANADA·Filed 2021·Granted Aug 16, 2022·4 cites·20 claims
- 0587US6837686B2Blade retention scheme using a retention tabPRATT & WHITNEY CANADA·Filed 2002·Granted Jan 4, 2005·52 cites·8 claims
- 0682US8740551B2Blade outer air seal coolingDI PAOLA FRANCO·Filed 2010·Granted Jun 3, 2014·8 cites·9 claims
- 0781US8622693B2Blade outer air seal support cooling air distribution systemDI PAOLA FRANCO·Filed 2010·Granted Jan 7, 2014·7 cites·12 claims
- 0880US8568085B2High pressure turbine vane cooling hole distrubutionDI PAOLA FRANCO·Filed 2010·Granted Oct 29, 2013·8 cites·20 claims
- 0978US7806662B2Blade retention system for use in a gas turbine enginePRATT & WHITNEY CANADA·Filed 2007·Granted Oct 5, 2010·17 cites·14 claims
- 1077US9745919B2Gas turbine engine exhaust ejector/mixerPRATT & WHITNEY CANADA·Filed 2014·Granted Aug 29, 2017·6 cites·8 claims
- 1174US11105204B2Turbine assemblyPRATT & WHITNEY CANADA·Filed 2019·Granted Aug 31, 2021·1 cites·18 claims
- 1270US10633992B2Rim sealPRATT & WHITNEY CANADA·Filed 2017·Granted Apr 28, 2020·1 cites·14 claims
- 1369US10197009B2Gas turbine engine ejectorPRATT & WHITNEY CANADA·Filed 2014·Granted Feb 5, 2019·3 cites·9 claims
- 1468US10876416B2Vane segment with ribsPRATT & WHITNEY CANADA·Filed 2018·Granted Dec 29, 2020·2 cites·20 claims
- 1567US8186939B2Turbine disc and retaining nut arrangementLECUYER DANIEL·Filed 2009·Granted May 29, 2012·11 cites·12 claims
- 1661US6918743B2Sheet metal turbine or compressor static shroudPRATT & WHITNEY CANADA CCORP·Filed 2002·Granted Jul 19, 2005·22 cites·2 claims
- 1757US11415079B2Turbo-shaft ejector with flow guide ringPRATT & WHITNEY CANADA·Filed 2018·Granted Aug 16, 2022·0 cites·8 claims
- 1853US10619596B2Gas turbine engine exhaust ejector/mixerPRATT & WHITNEY CANADA·Filed 2017·Granted Apr 14, 2020·0 cites·7 claims
- 1953US2020217214A1Rim sealPRATT & WHITNEY CANADA·Filed 2020·Application pending·0 cites
- 2049US2025354498A1Stator vane with multi-access cooling air feed passagePRATT & WHITNEY CANADA·Filed 2024·Application pending·0 cites
- 2143US11598265B2Tangential on-board injectorPRATT & WHITNEY CANADA·Filed 2021·Granted Mar 7, 2023·0 cites·19 claims
- 2242US2018347399A1Turbine shroud with integrated heat shieldPRATT & WHITNEY CANADA·Filed 2017·Application pending·0 cites
- 2341US11578599B2Rotor balance assemblyPRATT & WHITNEY CANADA·Filed 2021·Granted Feb 14, 2023·0 cites·14 claims
- 2440US11674394B2Gas turbine engine rotor assembly and method of using samePRATT & WHITNEY CANADA·Filed 2021·Granted Jun 13, 2023·0 cites·16 claims
- 2539US2018106161A1Turbine shroud segmentPRATT & WHITNEY CANADA·Filed 2016·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →