Inventor · disambiguated record
Christophe Nicolas Henri Viguier
Also filed as: VIGUIER CHRISTOPHE · VIGUIER CHRISTOPHE NICOLAS HENRI
5 granted patents·5 pending applications·48 citations·filing 2002–2022
75Inventor score
Top patents by PatentIndex Score
10 records- 0167US9677505B2Method for injecting fuel into a combustion chamber of a gas turbine, and injection system for implementing sameSAVARY NICOLAS·Filed 2012·Granted Jun 13, 2017·4 cites·7 claims
- 0266US6799427B2Multimode system for injecting an air/fuel mixture into a combustion chamberSNECMA MOTEURS·Filed 2003·Granted Oct 5, 2004·33 cites·11 claims
- 0351US12385440B2Fire safety system for a turbomachine comprising means for maintaining a cooling air speed and corresponding turbomachineSAFRAN HELICOPTER ENGINES·Filed 2022·Granted Aug 12, 2025·0 cites·13 claims
- 0445US2024328617A1Device for injecting dihydrogen and airCENTRE NAT RECH SCIENT·Filed 2022·Application pending·0 cites
- 0542US6959551B2Aeromechanical injection system with a primary anti-return swirlerSNECMA MOTEURS·Filed 2002·Granted Nov 1, 2005·11 cites·4 claims
- 0633US2018149365A1Turbine engine cvc combustion chamber module comprising a pre-combustion chamberSAFRAN HELICOPTER ENGINES·Filed 2016·Application pending·0 cites
- 0733US2018038278A1Constant-volume combustion system for a turbine engine of an aircraft engineSAFRAN HELICOPTER ENGINES·Filed 2016·Application pending·0 cites
- 0829US12168955B2Constant-volume combustion system with synchronized injectionSAFRAN·Filed 2020·Granted Dec 17, 2024·0 cites·6 claims
- 0929US2004011058A1Annular combustion chamber with two offset headsSNECMA MOTEURS·Filed 2002·Application pending·0 cites
- 1028US2017038075A1Aircraft engine comprising azimuth setting of the diffuser with respect to the combustion chamberTURBOMECA·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →