Inventor · disambiguated record
Thierry Fachat
Also filed as: FACHAT THIERRY
9 granted patents·1 pending application·154 citations·filing 2001–2023
88Inventor score
Files withSNECMA MOTEURS3FACHAT THIERRY2SAFRAN AIRCRAFT ENGINES2SNECMA2BLANCHARD STEPHANE PIERRE GUILLAUME1
Top patents by PatentIndex Score
10 records- 0193US7309209B2Device for tuning clearance in a gas turbine, while balancing air flowsSNECMA MOTEURS·Filed 2005·Granted Dec 18, 2007·48 cites·6 claims
- 0283US6896038B2Stator ring ventilation assemblySNECMA MOTEURS·Filed 2001·Granted May 24, 2005·44 cites·17 claims
- 0381US7287955B2Gas turbine clearance control devicesSNECMA MOTEURS·Filed 2005·Granted Oct 30, 2007·24 cites·19 claims
- 0480US7530788B2Hollow turbomachine bladeSNECMA·Filed 2006·Granted May 12, 2009·19 cites·8 claims
- 0576US9188014B2Vibration damper comprising a strip and jackets between outer platforms of adjacent composite-material blades of a turbine engine rotor wheelFACHAT THIERRY·Filed 2011·Granted Nov 17, 2015·6 cites·8 claims
- 0673US8662835B2Nozzle for a turbomachine turbineFACHAT THIERRY·Filed 2009·Granted Mar 4, 2014·10 cites·10 claims
- 0762US9194240B2Vibration damper comprising a peg between outer platforms of adjacent composite-material blades of a turbine engine rotor wheelBLANCHARD STEPHANE PIERRE GUILLAUME·Filed 2011·Granted Nov 24, 2015·2 cites·12 claims
- 0846US12276209B2Mounting of a sealing ring on an aeronautical turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Apr 15, 2025·0 cites·14 claims
- 0943US7360987B2Stator of a high-pressure turbine of a turbomachine, and a method of assembling itSNECMA·Filed 2005·Granted Apr 22, 2008·1 cites·10 claims
- 1043US2025389208A1Turbomachine having an improved oil-recovery deviceSAFRAN AIRCRAFT ENGINES·Filed 2023·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →