Inventor · disambiguated record
Jean-François Cortequisse
Also filed as: CORTEQUISSE JEAN-FRANCOIS · CORTEQUISSE JEAN-FRANCOIS GERARD JACQUES · CORTEQUISSE JEAN-FRANÇOIS
19 granted patents·76 citations·filing 2007–2019
92Inventor score
Files withTECHSPACE AERO SA11CORTEQUISSE JEAN-FRANCOIS4CORTEQUISSE JEAN-FRANCOIS GERARD JACQUES2SAFRAN AERO BOOSTERS SA2
Top patents by PatentIndex Score
19 records- 0195US10400625B2Lattice type blade of an axial turbine engine compressorTECHSPACE AERO SA·Filed 2015·Granted Sep 3, 2019·11 cites·13 claims
- 0292US10337340B2Mixed stator for an axial turbine engine compressorTECHSPACE AERO SA·Filed 2015·Granted Jul 2, 2019·9 cites·7 claims
- 0389US9816381B2Composite blade made by additive manufacturingTECHSPACE AERO SA·Filed 2014·Granted Nov 14, 2017·7 cites·20 claims
- 0483US10082038B2Axial turbomachine compressor outer casing with sealTECHSPACE AERO SA·Filed 2015·Granted Sep 25, 2018·4 cites·20 claims
- 0581US10113439B2Internal shroud for a compressor of an axial-flow turbomachineTECHSPACE AERO SA·Filed 2015·Granted Oct 30, 2018·3 cites·19 claims
- 0678US10428833B2Axial turbomachine compressor casingTECHSPACE AERO SA·Filed 2016·Granted Oct 1, 2019·2 cites·18 claims
- 0778US10392965B2Splitter nose of a low-pressure compressor of an axial turbomachine with annular deicing conduitSAFRAN AERO BOOSTERS SA·Filed 2016·Granted Aug 27, 2019·2 cites·19 claims
- 0878US8636466B2Segmented composite inner ferrule and segment of diffuser of axial compressorCORTEQUISSE JEAN-FRANCOIS·Filed 2009·Granted Jan 28, 2014·16 cites·17 claims
- 0973US11448095B2Turbine engine oil tank, method for measuring level, and computer programSAFRAN AERO BOOSTERS SA·Filed 2019·Granted Sep 20, 2022·1 cites·17 claims
- 1069US9670936B2Turbomachine stator internal shell with abradable materialTECHSPACE AERO SA·Filed 2014·Granted Jun 6, 2017·3 cites·20 claims
- 1167US8133011B2Device for stiffening the stator of a turbomachine and application to aircraft enginesCORTEQUISSE JEAN-FRANCOIS GERARD JACQUES·Filed 2008·Granted Mar 13, 2012·11 cites·10 claims
- 1264US9951654B2Stator blade sector for an axial turbomachine with a dual means of fixingTECHSPACE AERO SA·Filed 2014·Granted Apr 24, 2018·2 cites·8 claims
- 1363US9062687B2Segmented composite inner ferrule and segment of diffuser of axial compressorCORTEQUISSE JEAN-FRANCOIS·Filed 2014·Granted Jun 23, 2015·1 cites·13 claims
- 1463US8414256B2One-piece bladed drum of an axial turbomachine compressorCORTEQUISSE JEAN-FRANCOIS·Filed 2009·Granted Apr 9, 2013·4 cites·15 claims
- 1554US10280940B2Blade and shroud with socket for a compressor of an axial turbomachineTECHSPACE AERO SA·Filed 2016·Granted May 7, 2019·0 cites·14 claims
- 1653US10280758B2Composite compressor blade for an axial-flow turbomachineTECHSPACE AERO SA·Filed 2016·Granted May 7, 2019·0 cites·16 claims
- 1746US9739163B2Strip for abradable in a compressor turbineTECHSPACE AERO SA·Filed 2014·Granted Aug 22, 2017·0 cites·21 claims
- 1845US8939712B2External segmented shell capable of correcting for rotor misalignment in relation to the statorCORTEQUISSE JEAN-FRANCOIS·Filed 2012·Granted Jan 27, 2015·0 cites·16 claims
- 1926US8157519B2Connecting systemCORTEQUISSE JEAN-FRANCOIS GERARD JACQUES·Filed 2007·Granted Apr 17, 2012·0 cites·13 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →