Inventor · disambiguated record
Damien Joseph Cellier
Also filed as: CELLIER DAMIEN · CELLIER DAMIEN JOSEPH
12 granted patents·30 citations·filing 2012–2016
86Inventor score
Top patents by PatentIndex Score
12 records- 0183US9464526B2Airfoil and platform assembly for subsonic flowCELLIER DAMIEN·Filed 2012·Granted Oct 11, 2016·10 cites·14 claims
- 0272US10002209B2Method for modelling a part, in particular a bladingSNECMA·Filed 2014·Granted Jun 19, 2018·4 cites·13 claims
- 0371US9556740B2Turbine engine blade, in particular for a one-piece bladed diskSNECMA·Filed 2012·Granted Jan 31, 2017·5 cites·10 claims
- 0471US9458720B2Airfoil and platform assembly for supersonic flowCELLIER DAMIEN·Filed 2012·Granted Oct 4, 2016·5 cites·10 claims
- 0569US10301941B2Turbine engine rotor bladeSNECMA·Filed 2014·Granted May 28, 2019·4 cites·17 claims
- 0663US10352330B2Turbomachine part with a non-axisymmetric surfaceSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Jul 16, 2019·1 cites·13 claims
- 0761US10753371B2Stage of variable-pitch blades for a turbine engine, turbine engine and associated installation methodSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Aug 25, 2020·1 cites·8 claims
- 0852US10138897B2Blade and blade dihedral angleSNECMA·Filed 2014·Granted Nov 27, 2018·0 cites·7 claims
- 0946US10216867B2Method for modeling a non-axisymmetric surfaceSNECMA·Filed 2014·Granted Feb 26, 2019·0 cites·12 claims
- 1039US10330117B2Angular stator sector for a turbomachine compressor comprising a brush sealSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Jun 25, 2019·0 cites·7 claims
- 1137US11221020B2Dimensioning of the skeleton angle of the trailing edge of the arms crossing the by-pass flow of a turbofanSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jan 11, 2022·0 cites·10 claims
- 1237US10309419B2Turbomachine centre blade comprising a curved portionSAFRAN AIRCARFT ENGINES·Filed 2012·Granted Jun 4, 2019·0 cites·8 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →