Inventor · disambiguated record
Christophe Chabaille
Also filed as: CHABAILLE CHRISTOPHE
10 granted patents·20 citations·filing 2014–2019
82Inventor score
Top patents by PatentIndex Score
10 records- 0189US10041411B2Compact dosing device for an injector with two fuel circuits for an aircraft turbomachineSNECMA·Filed 2014·Granted Aug 7, 2018·12 cites·10 claims
- 0281US11098648B2Chamber between an inlet nozzle and an obturator, for a turbomachine injectorSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Aug 24, 2021·2 cites·11 claims
- 0373US10495312B2Sealing device between an injection system and a fuel injection nozzle of an aircraft turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Dec 3, 2019·2 cites·9 claims
- 0470US11788727B2Injector nose for turbomachine comprising a primary fuel circuit arranged around a secondary fuel circuitSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Oct 17, 2023·1 cites·11 claims
- 0570US9857080B2Fuel injector for a turbine engineSNECMA·Filed 2014·Granted Jan 2, 2018·3 cites·4 claims
- 0664US11168886B2Injector nose for turbomachine including a secondary fuel swirler with changing sectionSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Nov 9, 2021·0 cites·9 claims
- 0749US10563586B2Fuel injector for a turbine engineSNECMA·Filed 2014·Granted Feb 18, 2020·0 cites·9 claims
- 0845US11002196B2Combustion chamber comprising two types of injectors in which the sealing members have a different opening thresholdSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted May 11, 2021·0 cites·15 claims
- 0939US11022312B2Connection device comprising several curved concentric tubesSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Jun 1, 2021·0 cites·15 claims
- 1033US10995671B2Housing of a gasket for a turbomachine injectorSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted May 4, 2021·0 cites·7 claims
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