Inventor · disambiguated record
Sebastien Alain Christophe Bourgois
Also filed as: BOURGOIS SEBASTIEN ALAIN CHRISTOPHE · BOURGOIS SÉBASTIEN ALAIN CHRISTOPHE
10 granted patents·1 pending application·24 citations·filing 2009–2019
84Inventor score
Files withSAFRAN AIRCRAFT ENGINES6BOURGOIS SEBASTIEN ALAIN CHRISTOPHE2SNECMA2BOURGOIS SÉBASTIEN ALAIN CHRISTOPHE1
Top patents by PatentIndex Score
11 records- 0183US8661829B2Aerodynamic shroud for the back of a combustion chamber of a turbomachineBOURGOIS SEBASTIEN ALAIN CHRISTOPHE·Filed 2011·Granted Mar 4, 2014·7 cites·14 claims
- 0279US10443850B2Turbomachine combustion chamber comprising an airflow guide device of specific shapeSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Oct 15, 2019·3 cites·10 claims
- 0369US11739936B2Injection system for turbomachine, comprising a swirler and mixing bowl vortex holesSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Aug 29, 2023·1 cites·15 claims
- 0469US11268699B2Injection system for a turbine engine annular combustion chamberSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Mar 8, 2022·1 cites·13 claims
- 0569US9581334B2Annular combustion chamber in a turbine engineSNECMA·Filed 2012·Granted Feb 28, 2017·3 cites·10 claims
- 0669US9127841B2Turbomachine combustion chamber comprising improved means of air supplyBOURGOIS SEBASTIEN ALAIN CHRISTOPHE·Filed 2010·Granted Sep 8, 2015·4 cites·6 claims
- 0765US9765970B2Aircraft turbomachine combustion chamber module and method for designing sameSAFRAN AIRCRAFT ENGINES·Filed 2012·Granted Sep 19, 2017·3 cites·8 claims
- 0856US10109985B2Semiconductor igniter plug for an aircraft turbomachine, comprising scoops for discharging possible fuel residuesSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Oct 23, 2018·1 cites·9 claims
- 0951US8955326B2Mixing screw for a fuel injector in a combustion chamber of a gas turbine, and corresponding combustion deviceBOURGOIS SÉBASTIEN ALAIN CHRISTOPHE·Filed 2010·Granted Feb 17, 2015·1 cites·15 claims
- 1050US11840994B2Multipoint fuel injection deviceSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Dec 12, 2023·0 cites·8 claims
- 1141US2011271678A1Turbomachine combustion chamber wall having a single annular row of inlet orifices for primary air and for dilution airSNECMA·Filed 2009·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →