Inventor · disambiguated record
Serge Fargeas
Also filed as: FARGEAS SERGE · FARGEAS SERGE ALAIN
16 granted patents·10 citations·filing 2005–2020
86Inventor score
Top patents by PatentIndex Score
16 records- 0181US9643240B2Shell mould having a heat shieldSNECMA·Filed 2013·Granted May 9, 2017·2 cites·7 claims
- 0277US8201612B2Process for manufacturing directionally solidified bladesFARGEAS SERGE·Filed 2009·Granted Jun 19, 2012·4 cites·8 claims
- 0375US9744587B2Mould for monocrystalline castingSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Aug 29, 2017·1 cites·8 claims
- 0470US9381565B2Monocrystalline casting moldSNECMA·Filed 2014·Granted Jul 5, 2016·1 cites·9 claims
- 0562US7370688B2Lost wax moulding method with contact layerSNECMA·Filed 2005·Granted May 13, 2008·2 cites·18 claims
- 0659US11235379B2Foundry process with hot mold castingSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Feb 1, 2022·0 cites·8 claims
- 0758US11745254B2Foundry mold, method for manufacturing the mold and foundry methodSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Sep 5, 2023·0 cites·11 claims
- 0855US9796058B2Method for producing turbine engine parts, and resulting mould and blank compromising stacked partsSNECMA·Filed 2014·Granted Oct 24, 2017·0 cites·8 claims
- 0955US9616489B2Casting patternSNECMA·Filed 2013·Granted Apr 11, 2017·0 cites·11 claims
- 1053US11878338B2Mould for manufacturing a component by pouring metal and epitaxial growth, and associated manufacturing methodSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Jan 23, 2024·0 cites·9 claims
- 1153US10730108B2Directional solidification cooling furnace and cooling process using such a furnaceSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Aug 4, 2020·0 cites·9 claims
- 1250US9844843B2Method for producing turbine engine parts, and resulting blank and mouldSNECMA·Filed 2014·Granted Dec 19, 2017·0 cites·5 claims
- 1350US9764382B2Lined centrifugal mould with controlled thermal inertiaSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Sep 19, 2017·0 cites·4 claims
- 1447US9969035B2Method for producing a turbine engine part, and resulting mould and intermediate blankSNECMA·Filed 2014·Granted May 15, 2018·0 cites·14 claims
- 1545US11772155B2Method for manufacturing a metal workpiece limiting the appearance of recrystallized grains in said workpieceSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Oct 3, 2023·0 cites·12 claims
- 1638US10486230B2Method for manufacturing a two-component blade for a gas turbine engine and blade obtained by such a methodSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Nov 26, 2019·0 cites·7 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →