Inventor · disambiguated record
Brice Marie Yves Emile Le Pannerer
Also filed as: LE PANNERER BRICE · LE PANNERER BRICE MARIE YVES EMILE
8 granted patents·2 citations·filing 2014–2023
73Inventor score
Top patents by PatentIndex Score
8 records- 0179US11686274B2Confluence structure of a primary stream and a secondary stream in a bypass turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Jun 27, 2023·2 cites·15 claims
- 0265US11873783B2Confluence structure of a primary stream and a secondary stream in a bypass turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2023·Granted Jan 16, 2024·0 cites·49 claims
- 0356US11373291B2Combustion chamber module for an aircraft turbine engine comprising marks facilitating identification during endoscopic inspection of the combustion chamberSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jun 28, 2022·0 cites·9 claims
- 0448US10337740B2Annular combustion chamber in a turbine engineSNECMA·Filed 2014·Granted Jul 2, 2019·0 cites·12 claims
- 0545US10458654B2Combustion chamber in a turbine engineSNECMA·Filed 2014·Granted Oct 29, 2019·0 cites·12 claims
- 0638US10060627B2Flame-holder deviceSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Aug 28, 2018·0 cites·19 claims
- 0733US11713730B2Convergent-divergent flap pair for a variable-geometry turbojet engine nozzle comprising cooling air circulation ducts connected through contact surfacesSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Aug 1, 2023·0 cites·9 claims
- 0831US10139110B2Bearing element to cushion axial displacements of a sliding traverse of an injection system for a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Nov 27, 2018·0 cites·17 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →