Inventor · disambiguated record
Aurelien Rene-Pierre Massot
Also filed as: MASSOT AURELIEN RENE-PIERRE · MASSOT AURÉLIEN RENÉ-PIERRE
7 granted patents·62 citations·filing 2008–2016
82Inventor score
Files withSNECMA2GIRARD PATRICK JOSEPH MARIE1HAZEVIS PHILIPPE GERARD MARIE1LESCURE XAVIER FIRMIN CAMILLE JEAN1MASSOT AURELIEN RENE-PIERRE1
Top patents by PatentIndex Score
7 records- 0181US8172526B2Sealing a hub cavity of an exhaust casing in a turbomachineLESCURE XAVIER FIRMIN CAMILLE JEAN·Filed 2008·Granted May 8, 2012·26 cites·10 claims
- 0276US8100644B2Sealing a rotor ring in a turbine stageHAZEVIS PHILIPPE GERARD MARIE·Filed 2008·Granted Jan 24, 2012·22 cites·8 claims
- 0364US10605106B2Turbine of gas turbine engine, comprising a labyrinth seal elementSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Mar 31, 2020·1 cites·11 claims
- 0462US8221061B2Gas turbine engine with valve for establishing communication between two enclosuresMASSOT AURELIEN RENE-PIERRE·Filed 2009·Granted Jul 17, 2012·9 cites·9 claims
- 0550US8147189B2Sectorized nozzle for a turbomachineGIRARD PATRICK JOSEPH MARIE·Filed 2008·Granted Apr 3, 2012·4 cites·13 claims
- 0643US9732885B2Cooling device for the casing of an aircraft jet engine comprising a supporting deviceSNECMA·Filed 2014·Granted Aug 15, 2017·0 cites·16 claims
- 0737US9677413B2Interface device between two turbomachine elementsSNECMA·Filed 2014·Granted Jun 13, 2017·0 cites·11 claims
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