Inventor · disambiguated record
Francois Pierre Georges Maurice Ribassin
Also filed as: RIBASSIN FRANCOIS · RIBASSIN FRANCOIS PIERRE GEORG · RIBASSIN FRANCOIS PIERRE GEORGES MAURICE · RIBASSIN FRANÇOIS PIERRE
7 granted patents·111 citations·filing 2001–2020
85Inventor score
Top patents by PatentIndex Score
7 records- 0191US6676373B2Assembly formed by at least one blade and a blade-fixing platform for a turbomachine, and a method of manufacturing itSNECMA MOTEURS·Filed 2001·Granted Jan 13, 2004·49 cites·35 claims
- 0285US11441779B2Configuring and positioning air passage holes in a combustion chamber wallSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Sep 13, 2022·2 cites·9 claims
- 0377US7147434B2Nozzle ring with adhesive bonded blading for aircraft engine compressorSNECMA MOTEURS·Filed 2004·Granted Dec 12, 2006·32 cites·12 claims
- 0471US7553130B1Nozzle ring adhesive bonded blading for aircraft engine compressorSNECMA·Filed 2006·Granted Jun 30, 2009·6 cites·19 claims
- 0568US7530784B2Device for controlling variable-pitch vanes in a turbomachineSNECMA·Filed 2006·Granted May 12, 2009·11 cites·12 claims
- 0665US10883718B2Air intake swirler for a turbomachine injection system comprising an aerodynamic deflector at its inletSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Jan 5, 2021·1 cites·12 claims
- 0763US9512733B2Diffuser/rectifier assembly for a turbine engine with corrugated downstream wallsLOMBARD JEAN-PIERRE FRANCOIS·Filed 2009·Granted Dec 6, 2016·10 cites·11 claims
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