Inventor · disambiguated record
Dominique Raulin
Also filed as: RAULIN DOMINIQUE
18 granted patents·187 citations·filing 1994–2019
94Inventor score
Files withSNECMA MOTEURS7SNECMA4SAFRAN AIRCRAFT ENGINES3PAPIN THIERRY GEORGES PAUL2BRETTES FRÉDÉRIC1
Top patents by PatentIndex Score
18 records- 0185US8740556B2Structural and aerodynamic module for a turbomachine casing and casing structure comprising a plurality of such a modulePAPIN THIERRY GEORGES PAUL·Filed 2011·Granted Jun 3, 2014·12 cites·13 claims
- 0281US9556745B2Turbine engine vane plate sealPAPIN THIERRY GEORGES PAUL·Filed 2012·Granted Jan 31, 2017·8 cites·5 claims
- 0379US8038387B2Bearing for variable pitch stator vaneSNECMA·Filed 2007·Granted Oct 18, 2011·14 cites·4 claims
- 0471US6799945B2Stator blade pivoting arrangement in a turbomachineSNECMA MOTEURS·Filed 2003·Granted Oct 5, 2004·29 cites·4 claims
- 0569US7037070B2Variable pitch device for two blade stages fixed onto a turbojetSNECMA MOTEURS·Filed 2004·Granted May 2, 2006·19 cites·1 claims
- 0668US7530784B2Device for controlling variable-pitch vanes in a turbomachineSNECMA·Filed 2006·Granted May 12, 2009·11 cites·12 claims
- 0767US8646744B2Structural frame for a turbomachineDUCHATELLE THIERRY FRANCOIS MAURICE·Filed 2009·Granted Feb 11, 2014·11 cites·16 claims
- 0862US10883374B2Blade comprising a folded leading edge shield and method of manufacturing the bladeSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jan 5, 2021·1 cites·11 claims
- 0960US7004723B2Device for controlling variable-pitch vanes in a turbomachineSNECMA MOTEURS·Filed 2004·Granted Feb 28, 2006·17 cites·6 claims
- 1059US10100859B2Riveted assembly and associated production methodSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Oct 16, 2018·1 cites·12 claims
- 1154US5421704AInter-blade platform for a bladed disc of a turbomachine rotorSNECMA·Filed 1994·Granted Jun 6, 1995·31 cites·1 claims
- 1252US6782702B2Compressor air drawing off systemSNECMA MOTEURS·Filed 2002·Granted Aug 31, 2004·15 cites·15 claims
- 1348US8052381B2Turbomachine module provided with a device to improve radial clearancesSNECMA·Filed 2008·Granted Nov 8, 2011·3 cites·14 claims
- 1442US11725822B2Combustion module for a gas turbo engine with chamber bottom stopSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Aug 15, 2023·0 cites·17 claims
- 1541US9879552B2Hydraulic device for changing the pitch of a propellerBRETTES FRÉDÉRIC·Filed 2011·Granted Jan 30, 2018·0 cites·9 claims
- 1638US7018173B2Device for stopping in rotation a fixed blade bearing sector in a gas turbine casingSNECMA MOTEURS·Filed 2002·Granted Mar 28, 2006·7 cites·13 claims
- 1737US7140838B2Control lever attachment with play compensation for blades with variable setting anglesSNECMA MOTEURS·Filed 2004·Granted Nov 28, 2006·3 cites·17 claims
- 1831US7048504B2Machine stator and mounting and dismounting methodsSNECMA MOTEURS·Filed 2003·Granted May 23, 2006·5 cites·6 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →