Inventor · disambiguated record
Sarah Hamadi
Also filed as: HAMADI SARAH
7 granted patents·2 pending applications·1 citations·filing 2011–2021
69Inventor score
Top patents by PatentIndex Score
9 records- 0160US10745800B2Coating for protection against oxidation and against hot corrosion on a superalloy substrateSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Aug 18, 2020·0 cites·10 claims
- 0253US12241151B2Method for manufacturing a part made of a monocrystalline superalloySAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Mar 4, 2025·0 cites·14 claims
- 0351US12392256B2Superalloy turbomachine part with an optimized hafnium contentSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Aug 19, 2025·0 cites·9 claims
- 0449US9840914B2Method for localised repair of a damaged thermal barrierSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Dec 12, 2017·1 cites·20 claims
- 0546US9228264B2Process for depositing a coating for protection against oxidation and against hot corrosion on a superalloy substrateMENUEY JUSTINE·Filed 2011·Granted Jan 5, 2016·0 cites·16 claims
- 0644US2013115085A1Thermal barrier for turbine blades, having a columnar structure with spaced-apart columnsMENUEY JUSTINE·Filed 2011·Application pending·0 cites
- 0740US10539039B2Method of measuring the temperature reached by a part, in particular a turbine engine partSAFRAN AIRCRAFT ENGINES·Filed 2013·Granted Jan 21, 2020·0 cites·12 claims
- 0837US10445434B2Method and device for estimating a thickness of a ceramic thermal barrier coatingSAFRAN AIRCRAFT ENGINES·Filed 2012·Granted Oct 15, 2019·0 cites·20 claims
- 0933US2023065064A1Coated turbomachine part having a nickel-based substrate comprising hafniumSAFRAN AIRCRAFT ENGINES·Filed 2021·Application pending·0 cites
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