Inventor · disambiguated record
Antoine Jean-Philippe Beaujard
Also filed as: BEAUJARD ANTOINE · BEAUJARD ANTOINE JEAN-PHILIPPE
28 granted patents·1 pending application·129 citations·filing 2011–2023
95Inventor score
Files withSAFRAN AIRCRAFT ENGINES13BEAUJARD ANTOINE JEAN-PHILIPPE4SNECMA4HERAKLES2ROUSSILLE CLÉMENT2
Top patents by PatentIndex Score
29 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
- 0587US10072508B2Turbomachine rotor with optimised bearing surfacesSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Sep 11, 2018·5 cites·7 claims
- 0683US9708918B2Hollow-blade turbine vane made from composite material, turbine or compressor including a nozzle or guide vane assembly formed by such blades, and turbomachine comprising sameHERAKLES·Filed 2012·Granted Jul 18, 2017·7 cites·20 claims
- 0782US9784113B2Method of fabricating a turbine or compressor guide vane sector made of composite material for a turbine engine, and a turbine or a compressor incorporating such guide vane sectorsHERAKLES·Filed 2012·Granted Oct 10, 2017·8 cites·22 claims
- 0876US10773813B2Aircraft with a propulsion unit comprising a fan at the rear of the fuselageSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Sep 15, 2020·3 cites·27 claims
- 0976US9822655B2Assembly 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
- 1073US11261754B2Shell for reducing overpressure in the vicinity of the upstream seal of a turbojet bearing housingSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Mar 1, 2022·2 cites·5 claims
- 1173US9518472B2Turbine engine stator wheel and a turbine or a compressor including such a stator wheelBELMONTE OLIVIER·Filed 2012·Granted Dec 13, 2016·4 cites·16 claims
- 1269US10351252B2Aircraft comprising a propulsion assembly including a pair of propellers at the rear of the fuselageSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jul 16, 2019·2 cites·9 claims
- 1369US9103219B2CMC turbine nozzle adapted to support a metallic turbine internal casing by an axial contactBEAUJARD ANTOINE JEAN-PHILIPPE·Filed 2012·Granted Aug 11, 2015·4 cites·9 claims
- 1466US9834312B2Method for holding an adapter piece on a tubular housing of a turbo engine, and corresponding adapter piece and holding systemSNECMA·Filed 2013·Granted Dec 5, 2017·3 cites·8 claims
- 1564US10036277B2Gas turbine engine comprising a composite component and a metal component which are connected by a flexible fixing deviceSNECMA·Filed 2013·Granted Jul 31, 2018·2 cites·13 claims
- 1662US9429030B2Device for locking a root of a rotor bladeBART JACQUES RENE·Filed 2011·Granted Aug 30, 2016·2 cites·12 claims
- 1760US9638042B2Turbine engine comprising a metal protection for a composite partBEAUJARD ANTOINE JEAN-PHILIPPE·Filed 2012·Granted May 2, 2017·2 cites·9 claims
- 1857US12025018B2Turbine arrangement incorporating an oil recovery circumferential troughSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Jul 2, 2024·0 cites·9 claims
- 1956US9784122B2Method 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
- 2054US9194241B2CMC turbine nozzle adapted to support a metallic turbine internal casing by a radial contactBEAUJARD ANTOINE JEAN-PHILIPPE·Filed 2012·Granted Nov 24, 2015·1 cites·9 claims
- 2151US11377978B2Device for evacuation of a ventilated lubricated chamber of a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Jul 5, 2022·0 cites·9 claims
- 2250US11371432B2Aircraft engine intake arrangement comprising a mechanical decouplerSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jun 28, 2022·0 cites·13 claims
- 2345US2020240641A1Turbomachine, such as an aircraft turbojet engineSAFRAN AIRCRAFT ENGINES·Filed 2020·Application pending·0 cites
- 2444US11499439B2Double flow turbojet including an intermediate flow path dedicated to supplying with air via radial arms an exhaust casing of this turbojetSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Nov 15, 2022·0 cites·6 claims
- 2543US11187107B2Turbojet with bearing architecture optimised for the support of a low pressure shaftSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Nov 30, 2021·0 cites·18 claims
- 2643US11136937B2Aircraft propulsion assembly comprising a thrust reverserSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Oct 5, 2021·0 cites·15 claims
- 2742US12359580B2Turbine engine for an aircraftSAFRAN AIRCRAFT ENGINES·Filed 2023·Granted Jul 15, 2025·0 cites·14 claims
- 2840US10450884B2Impeller having a radial seal for a turbine engine turbineSNECMA·Filed 2015·Granted Oct 22, 2019·0 cites·17 claims
- 2939US10138737B2Rotor for turbine engine comprising blades with added platformsSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Nov 27, 2018·0 cites·12 claims
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