Inventor · disambiguated record
Philippe Pabion
Also filed as: PABION PHILIPPE · PABION PHILIPPE J · PABION PHILIPPE J-P · PABION PHILIPPE JEAN-PIERRE
22 granted patents·2 pending applications·377 citations·filing 1992–2009
96Inventor score
Files withSNECMA10SNECMA MOTEURS10GUIMBARD JEAN-MICHEL BERNARD2GIRARD PATRICK JOSEPH MARIE1MASSOT AURELIEN RENE-PIERRE1
Top patents by PatentIndex Score
24 records- 0193US7377749B2Device for balancing a rotating part, in particular a turbojet rotorSNECMA·Filed 2005·Granted May 27, 2008·38 cites·18 claims
- 0292US8162593B2Inter-turbine casing with cooling circuit, and turbofan comprising itGUIMBARD JEAN-MICHEL BERNARD·Filed 2008·Granted Apr 24, 2012·35 cites·12 claims
- 0389US7687021B2Method of fabricating a casing for turbine statorSNECMA·Filed 2005·Granted Mar 30, 2010·31 cites·16 claims
- 0485US7234920B2Turbine casing having refractory hooks and obtained by a powder metallurgy methodSNECMA MOTEURS·Filed 2005·Granted Jun 26, 2007·28 cites·24 claims
- 0580US7972107B2Device for cooling a turbomachine turbine casingSNECMA·Filed 2007·Granted Jul 5, 2011·18 cites·17 claims
- 0672US7527470B2Stator turbine vane with improved coolingSNECMA·Filed 2005·Granted May 5, 2009·14 cites·5 claims
- 0770US7794203B2Joining device for joining two assemblies, for example for a stator of a turbomachineSNECMA·Filed 2008·Granted Sep 14, 2010·6 cites·11 claims
- 0869US6699011B2Linking arrangement of a turbine stator ring to a support strutSNECMA MOTEURS·Filed 2001·Granted Mar 2, 2004·26 cites·4 claims
- 0968US5193982ASeparate inter-blade platform for a bladed rotor diskSNECMA·Filed 1992·Granted Mar 16, 1993·38 cites·4 claims
- 1064US7290982B2Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circleSNECMA MOTEURS·Filed 2004·Granted Nov 6, 2007·20 cites·24 claims
- 1162US8221061B2Gas turbine engine with valve for establishing communication between two enclosuresMASSOT AURELIEN RENE-PIERRE·Filed 2009·Granted Jul 17, 2012·9 cites·9 claims
- 1261US8162594B2Cooled blade for a turbomachineGUIMBARD JEAN-MICHEL BERNARD·Filed 2008·Granted Apr 24, 2012·8 cites·17 claims
- 1361US8011879B2Transition channel between two turbine stagesSNECMA·Filed 2007·Granted Sep 6, 2011·7 cites·12 claims
- 1460US8128375B2Turbomachine blade that is cast with a local fattening of the section of the airfoilGIRARD PATRICK JOSEPH MARIE·Filed 2008·Granted Mar 6, 2012·1 cites·15 claims
- 1554US5421704AInter-blade platform for a bladed disc of a turbomachine rotorSNECMA·Filed 1994·Granted Jun 6, 1995·31 cites·1 claims
- 1651US7004721B2Annular platform for a nozzle of a low-pressure turbine of a turbomachineSNECMA MOTEURS·Filed 2004·Granted Feb 28, 2006·11 cites·20 claims
- 1750US7025562B2Device for cooling turbine disksSNECMA MOTEURS·Filed 2004·Granted Apr 11, 2006·12 cites·20 claims
- 1848US7137783B2Cooled gas turbine bladesSNECMA MOTEURS·Filed 2004·Granted Nov 21, 2006·7 cites·11 claims
- 1945US6050522AThrust reverser for a high bypass turbofan engineSNECMA·Filed 1998·Granted Apr 18, 2000·16 cites·6 claims
- 2042US5520514ASealing lining between vanes and intermediate platformsSNECMA·Filed 1995·Granted May 28, 1996·18 cites·4 claims
- 2138US7351030B2Connection device for making a connection between a turbomachine nozzle and a feed enclosure for feeding cooling fluid to injectorsSNECMA MOTEURS·Filed 2004·Granted Apr 1, 2008·3 cites·20 claims
- 2238US7210901B2Assembly of sectors of a dispensing unit in a gas turbineSNECMA MOTEURS·Filed 2002·Granted May 1, 2007·0 cites·6 claims
- 2334US2003146578A1Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circleSNECMA MOTEURS·Filed 2003·Application pending·0 cites
- 2434US2004146398A1Assembly arrangement for blades with adjustable settingSNECMA MOTEURS·Filed 2004·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →