Inventor · disambiguated record
Patrice Eneau
Also filed as: ENEAU PATRICE
24 granted patents·218 citations·filing 2002–2020
94Inventor score
Top patents by PatentIndex Score
24 records- 0190US9890644B2Foundry core assembly for manufacturing a turbomachine blade, associated method of manufacturing a blade and associated bladeSNECMA·Filed 2013·Granted Feb 13, 2018·19 cites·7 claims
- 0290US6705836B2Gas turbine blade cooling circuitsSNECMA MOTEURS·Filed 2002·Granted Mar 16, 2004·76 cites·10 claims
- 0382US7513739B2Cooling circuits for a turbomachine moving bladeSNECMA·Filed 2006·Granted Apr 7, 2009·25 cites·10 claims
- 0479US11035235B2Turbomachine blade with optimised coolingSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Jun 15, 2021·3 cites·10 claims
- 0579US7033136B2Cooling circuits for a gas turbine bladeSNECMA MOTEURS·Filed 2004·Granted Apr 25, 2006·37 cites·14 claims
- 0674US9981308B2Method for manufacturing a core for moulding a bladeSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted May 29, 2018·1 cites·9 claims
- 0774US6916155B2Cooling circuits for a gas turbine bladeSNECMA MOTEURS·Filed 2002·Granted Jul 12, 2005·30 cites·23 claims
- 0871US7670112B2Turbine blade with cooling and with improved service lifeSNECMA·Filed 2006·Granted Mar 2, 2010·15 cites·10 claims
- 0959US9869187B2Turbomachine turbine blade comprising a cooling circuit with improved homogeneitySAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Jan 16, 2018·1 cites·10 claims
- 1057US7661930B2Central cooling circuit for a moving blade of a turbomachineSNECMA·Filed 2006·Granted Feb 16, 2010·8 cites·14 claims
- 1151US11913354B2Turbomachine moving blade with cooling circuit having a double row of discharge slotsSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Feb 27, 2024·0 cites·10 claims
- 1250US11719102B2Blade provided with a cooling circuitSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Aug 8, 2023·0 cites·12 claims
- 1349US11499436B2Turbine engine blade with improved coolingSAFRAN·Filed 2019·Granted Nov 15, 2022·0 cites·14 claims
- 1447US7192251B1Air deflector for a cooling circuit for a gas turbine bladeSNECMA·Filed 2006·Granted Mar 20, 2007·3 cites·10 claims
- 1545US12146420B2Aircraft turbomachine blade and method for manufacturing same using lost-wax castingSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Nov 19, 2024·0 cites·9 claims
- 1645US10767491B2Blade comprising a trailing edge having three distinct cooling regionsSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Sep 8, 2020·0 cites·8 claims
- 1744US11286788B2Blade for a turbomachine turbine, comprising internal passages for circulating cooling airSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Mar 29, 2022·0 cites·10 claims
- 1844US11187088B2Turbomachine vane, including deflectors in an inner cooling cavitySAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Nov 30, 2021·0 cites·9 claims
- 1944US10961856B2Ceramic core for a multi-cavity turbine bladeSAFRAN·Filed 2016·Granted Mar 30, 2021·0 cites·8 claims
- 2040US12091989B2Turbomachine blade with improved coolingSAFRAN·Filed 2020·Granted Sep 17, 2024·0 cites·26 claims
- 2140US10337333B2Turbine blade comprising a central cooling duct and two side cavities connected downstream from the central ductSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Jul 2, 2019·0 cites·9 claims
- 2239US10662789B2Turbine blade with optimised cooling at the trailing edge of same comprising upstream and downstream ducts and inner side cavitiesSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted May 26, 2020·0 cites·5 claims
- 2338US10689985B2Turbine blade with optimised coolingSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Jun 23, 2020·0 cites·13 claims
- 2438US10493520B2Unit for moulding a turbomachine blade, comprising a raised portion with a large cross-sectionSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Dec 3, 2019·0 cites·9 claims
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →