Inventor · disambiguated record
Antoine Robert Alain Brunet
Also filed as: BRUNET ANTOINE · BRUNET ANTOINE ROBERT ALAIN
21 granted patents·2 pending applications·119 citations·filing 2003–2022
93Inventor score
Files withSAFRAN AIRCRAFT ENGINES11SNECMA6BRUNET ANTOINE ROBERT ALAIN2SNECMA MOTEURS2ARGAUD THIERRY1
Top patents by PatentIndex Score
23 records- 0190US8777558B2Casing for a moving-blade wheel of turbomachineBRUNET ANTOINE ROBERT ALAIN·Filed 2009·Granted Jul 15, 2014·25 cites·16 claims
- 0276US10738650B2Device for deicing a splitter nose and inlet guide vanes of an aviation turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Aug 11, 2020·3 cites·6 claims
- 0375US11585230B2Assembly for a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Feb 21, 2023·2 cites·19 claims
- 0475US8029238B2System for cooling a downstream cavity of a centrifugal compressor impellerSNECMA·Filed 2007·Granted Oct 4, 2011·9 cites·11 claims
- 0573US7942630B2System for ventilating a downstream cavity of an impellor of a centrifugal compressorSNECMA·Filed 2007·Granted May 17, 2011·8 cites·11 claims
- 0672US8152460B2Device for bleeding air from a turbomachine compressorBRUNET ANTOINE ROBERT ALAIN·Filed 2008·Granted Apr 10, 2012·8 cites·14 claims
- 0770US9879607B2Sealing of turbine engine enclosures produced by brush seal and labyrinthSNECMA·Filed 2013·Granted Jan 30, 2018·5 cites·10 claims
- 0868US7937951B2System for cooling the impeller of a centrifugal compressorSNECMA·Filed 2007·Granted May 10, 2011·8 cites·11 claims
- 0966US6857851B2Axial compressor disk for a turbomachine with centripetal air bleedSNECMA MOTEURS·Filed 2003·Granted Feb 22, 2005·25 cites·22 claims
- 1059US12196504B2Heat exchanger comprising a baffle wall with hollow turbulence generatorsSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Jan 14, 2025·0 cites·9 claims
- 1158US8226353B2Ventilation of a downstream cavity of an impeller of a centrifugal compressorARGAUD THIERRY·Filed 2007·Granted Jul 24, 2012·9 cites·15 claims
- 1253US11753953B2Heat exchanger comprising an inter-vane wall provided with hollow turbulence generatorsSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Sep 12, 2023·0 cites·8 claims
- 1352US11225879B2Abradable turbomachine element provided with visual wear indicatorsSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Jan 18, 2022·0 cites·9 claims
- 1452US7937944B2System for ventilating a combustion chamber wallSNECMA·Filed 2007·Granted May 10, 2011·3 cites·15 claims
- 1548US8052381B2Turbomachine module provided with a device to improve radial clearancesSNECMA·Filed 2008·Granted Nov 8, 2011·3 cites·14 claims
- 1646US10273967B2Compressor shroud comprising a sealing element provided with a structure for entraining and diverting discharge airSANFRAN AIRCRAFT ENGINES·Filed 2014·Granted Apr 30, 2019·1 cites·10 claims
- 1744US6908278B2Device for straightening the flow of air fed to a centripetal bleed in a compressorSNECMA MOTEURS·Filed 2003·Granted Jun 21, 2005·10 cites·19 claims
- 1841US10975716B2Assembly forming a labyrinth seal for a turbomachine comprising an abradable material and inclined finsSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Apr 13, 2021·0 cites·9 claims
- 1940US2021207487A1Turbomachine blading angular sector with seal between sectorsSAFRAN AIRCRAFT ENGINES·Filed 2019·Application pending·0 cites
- 2040US2024418097A1Labyrinth sealing device for an aircraft turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2022·Application pending·0 cites
- 2139US10330117B2Angular stator sector for a turbomachine compressor comprising a brush sealSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Jun 25, 2019·0 cites·7 claims
- 2236US10683805B2Anti-icing system for a turbine engine vaneSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jun 16, 2020·0 cites·9 claims
- 2328US12031444B2Sealing assembly for a turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Jul 9, 2024·0 cites·15 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →