Inventor · disambiguated record
Sebastien Christophe Chalaud
Also filed as: CHALAUD SEBASTIEN · CHALAUD SEBASTIEN CHRISTOPHE · CHALAUD SÉBASTIEN · CHALAUD SÉBASTIEN CHRISTOPHE
18 granted patents·3 pending applications·48 citations·filing 2013–2019
91Inventor score
Top patents by PatentIndex Score
21 records- 0193US10392952B2Output director vane for an aircraft turbine engine, with an improved lubricant cooling function using a heat conduction matrix housed in an inner duct of the vaneSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Aug 27, 2019·9 cites·11 claims
- 0292US10890117B2Fluid supply system for turbine engine, including an adjustable flow pump and a fluid metering deviceSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jan 12, 2021·8 cites·12 claims
- 0388US11156114B2Turbomachine provided with a vane sector and a cooling circuitSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Oct 26, 2021·6 cites·20 claims
- 0488US10378556B2Outlet guide vane for aircraft turbine engine, presenting an improved lubricant cooling functionSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Aug 13, 2019·6 cites·12 claims
- 0583US10683774B2Oil tank comprising an oil level control deviceSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Jun 16, 2020·6 cites·9 claims
- 0678US11199108B2Outlet of a hot-gas pipe of an aircraft engine passing through an engine wallSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Dec 14, 2021·2 cites·7 claims
- 0773US10072581B2Gas turbine engine comprising a starter engaged with a low-pressure bodySAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Sep 11, 2018·2 cites·8 claims
- 0872US9464595B2Optimising the availability of a thrust reverserSNECMA·Filed 2013·Granted Oct 11, 2016·2 cites·5 claims
- 0968US10072578B2Method and system for injecting fuel into an engine combustion chamberSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Sep 11, 2018·3 cites·9 claims
- 1067US9021869B2Method for managing the operation of a fuel metering unitSNECMA·Filed 2013·Granted May 5, 2015·3 cites·8 claims
- 1163US10823074B2Recirculation of fluid through a turbomachine centrifugal pumpSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Nov 3, 2020·1 cites·7 claims
- 1253US10465910B2Multi-point injection device for an aircraft engineSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Nov 5, 2019·0 cites·16 claims
- 1350US10934889B2System and method for supplying lubrication fluid to at least one member of an aircraft propulsion assemblySAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Mar 2, 2021·0 cites·12 claims
- 1448US10473032B2Multipoint fuel injection system for a turbomachine and associated regulation methodSNECMA·Filed 2014·Granted Nov 12, 2019·0 cites·11 claims
- 1544US11143462B2Panel for heat exchange and improved noise reduction for a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Oct 12, 2021·0 cites·10 claims
- 1644US10837317B2Turbofan comprising a simplified bearing lubrication assemblySAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Nov 17, 2020·0 cites·20 claims
- 1744US9909498B2Variable geometries fluid supply circuit for a turbomachine without volumetric pumpSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Mar 6, 2018·0 cites·12 claims
- 1843US11466625B2Method for controlling the supply of fuel to a combustion chamber of a turbine engine, fuel supply system and turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Oct 11, 2022·0 cites·12 claims
- 1940US2018094584A1Cooling of the oil circuit of a turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2016·Application pending·0 cites
- 2037US2015337734A1Variable geometries fluid supply circuit and injection system supply circuitSNECMA·Filed 2015·Application pending·0 cites
- 2134US2017009659A1Cooling of a main line in a multipoint fuel injection systemSAFRAN AIRCRAFT ENGINES·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →