SC

Sebastien Christophe Chalaud

SE Safran Aircraft Engines: 16 patents #40 of 1,821Top 3%
SN Snecma: 2 patents #478 of 1,717Top 30%
Overall (All Time): #253,074 of 4,157,543Top 7%
18
Patents All Time

Issued Patents All Time

Showing 1–18 of 18 patents

Patent #TitleCo-InventorsDate
11466625 Method for controlling the supply of fuel to a combustion chamber of a turbine engine, fuel supply system and turbine engine Mohammed-Lamine BOUTALEB, Gwenole Yann LE PACHE 2022-10-11
11199108 Outlet of a hot-gas pipe of an aircraft engine passing through an engine wall Romain Jean-Claude Ferrier, Philippe Gerard Chanez, Lauren Davis, Bastien Pierre Verdier, Christian Sylvain Vessot 2021-12-14
11156114 Turbomachine provided with a vane sector and a cooling circuit Christian Sylvain Vessot 2021-10-26
11143462 Panel for heat exchange and improved noise reduction for a turbomachine Bellal Waissi, Lancelot Guillou, Jacky Novi Mardjono, Guillaume Mathon-Margueritte, Georges Jean Xavier Riou +1 more 2021-10-12
10934889 System and method for supplying lubrication fluid to at least one member of an aircraft propulsion assembly 2021-03-02
10890117 Fluid supply system for turbine engine, including an adjustable flow pump and a fluid metering device Pierre C. Mouton 2021-01-12
10837317 Turbofan comprising a simplified bearing lubrication assembly Romain Guillaume Cuvillier, Nils Edouard Romain Bordoni, Michel Gilbert Roland Brault, Guillaume Patrice Kubiak, Arnaud Nicolas Negri +1 more 2020-11-17
10823074 Recirculation of fluid through a turbomachine centrifugal pump 2020-11-03
10683774 Oil tank comprising an oil level control device Lise Jeanine Léonie Domecq, Yves Emprin 2020-06-16
10473032 Multipoint fuel injection system for a turbomachine and associated regulation method Clement Bernard, Loic Pora 2019-11-12
10465910 Multi-point injection device for an aircraft engine 2019-11-05
10392952 Output 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 vane Cédric Zaccardi, Mohamed-Lamine Boutaleb, Eric Pierre Georges Lemarechal, Thierry Georges Paul Papin 2019-08-27
10378556 Outlet guide vane for aircraft turbine engine, presenting an improved lubricant cooling function Cédric Zaccardi, Mohamed-Lamine Boutaleb, Eric Pierre Georges Lemarechal, Thierry Georges Paul Papin 2019-08-13
10072578 Method and system for injecting fuel into an engine combustion chamber 2018-09-11
10072581 Gas turbine engine comprising a starter engaged with a low-pressure body Bellal Waissi, Alain Pierre Garassino 2018-09-11
9909498 Variable geometries fluid supply circuit for a turbomachine without volumetric pump 2018-03-06
9464595 Optimising the availability of a thrust reverser 2016-10-11
9021869 Method for managing the operation of a fuel metering unit 2015-05-05