Inventor · disambiguated record
Elric Georges André Fremont
Also filed as: FREMONT ELRIC · FREMONT ELRIC GEORGES ANDRE · FREMONT ELRIC GEORGES ANDRÉ
8 granted patents·92 citations·filing 2012–2021
86Inventor score
Top patents by PatentIndex Score
8 records- 0194US9045992B2Turbomachine blades or vanes having complementary even/odd geometryROUSSILLE CLÉMENT·Filed 2012·Granted Jun 2, 2015·26 cites·30 claims
- 0292US9062562B2Composite material turbomachine engine blade or vane, compressor stator segment or turbine nozzle segment incorporating such vanes and method for manufacturing sameCOUPE DOMINIQUE·Filed 2012·Granted Jun 23, 2015·21 cites·33 claims
- 0391US9033673B2Turbomachine blade or vane having complementary asymmetrical geometryROUSSILLE CLÉMENT·Filed 2012·Granted May 19, 2015·18 cites·31 claims
- 0490US9506355B2Turbine engine blade or vane made of composite material, turbine nozzle or compressor stator incorporating such vanes and method of fabricating sameNUNEZ ROMAIN·Filed 2012·Granted Nov 29, 2016·12 cites·32 claims
- 0586US10190426B2Stator sector for a turbine engine, and a method of fabricating itHERAKLES·Filed 2015·Granted Jan 29, 2019·8 cites·10 claims
- 0676US9822655B2Assembly formed by a turbine nozzle or a compressor diffuser made of CMC for a turbine engine and by an abradable material support ring, and a turbine or a compressor incorporating such an assemblyBEAUJARD ANTOINE JEAN-PHILIPPE·Filed 2012·Granted Nov 21, 2017·6 cites·16 claims
- 0756US9784122B2Method of fabricating a composite material casing for a gas turbine engine, and a casing obtained therebySNECMA·Filed 2013·Granted Oct 10, 2017·1 cites·18 claims
- 0845US12018628B2Turbojet engine rear part comprising a nozzle having flaps comprising levers that are movable by means of upstream and downstream bearing wallsSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Jun 25, 2024·0 cites·8 claims
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