| Large eddy simulation of lithium-ion battery vent gases flame ignition and anchoring A Cellier, F Duchaine, T Poinsot, E Brodu, B Boust, M Bellenoue, G Okyay, ... Proceedings of the Combustion Institute 40 (1-4), 105632, 2024 | | 2024 |
| Constant volume combustion system PJB Metge, E Conete, G Mecuson, M Leyko US Patent 11,619,380, 2023 | | 2023 |
| An analytically reduced chemistry scheme for large eddy simulation of lithium-ion battery fires A Cellier, F Duchaine, T Poinsot, G Okyay, M Leyko, M Pallud Combustion and Flame 250, 112648, 2023 | 15 | 2023 |
| Constant-volume combustion system comprising a rotating closure element with segmented apertures M Leyko, PJB Metge, E Conete, G Mecuson US Patent 11,168,610, 2021 | | 2021 |
| Constant-volume combustion module for a turbine engine, comprising communication-based ignition M Leyko US Patent 11,066,990, 2021 | 4 | 2021 |
| Constant volume combustion chamber with counter rotating shutter valve PJB Metge, M Leyko US Patent 11,060,732, 2021 | 1 | 2021 |
| Flow deflector for a discharge valve system, discharge valve system and turbomachine comprising such a discharge valve system M Leyko, JAHJ Szydlowski US Patent 11,047,254, 2021 | 2 | 2021 |
| Heat-exchange and noise-reduction panel for a propulsion assembly M Leyko, I Ghazlane US Patent 10,794,246, 2020 | | 2020 |
| Constant-volume combustion module for a turbine engine M Leyko US Patent 10,662,874, 2020 | 2 | 2020 |
| Annular combustion chamber with continuous detonation wave M Leyko, MP Cazalens US Patent App. 16/097,732, 2020 | 2 | 2020 |
| Gyratory-effect flow deflector of a discharge valve system, discharge valve system and turbine engine comprising such a discharge valve system M Leyko, JAHJ Szydlowski US Patent 10,550,715, 2020 | 2 | 2020 |
| Fan rotor for a turbo machine such as a multiple flow turbojet engine driven by a reduction gear C Vessot, M Leyko US Patent 10,082,080, 2018 | 7 | 2018 |
| Air circulation device for turbomachine C Vessot, M Leyko US Patent 10,036,318, 2018 | | 2018 |
| Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method M Leyko, J Bertucchi, A Droit US Patent 9,915,227, 2018 | | 2018 |
| Convergent-divergent nozzle for a turbine engine M Leyko, J Bertucchi, M Gaillot US Patent 9,683,516, 2017 | | 2017 |
| Turbomachine comprising a device for the cooling of a pylon M Leyko, J Bertucchi, J Szydlowski US Patent 9,540,109, 2017 | 3 | 2017 |
| Assembly formed by a turbine engine and a system for attaching it to an aircraft structure M Gaillot, J Bertucchi, M Leyko US Patent 9,488,106, 2016 | 3 | 2016 |
| New combustion concepts to enhance the thermodynamic efficiency of propulsion engines M Bellenoue, B Boust, P Vidal, R Zitoun, T Gaillard, D Davidenko, ... Aerospace Lab, 13 pages, 2016 | 15 | 2016 |
| Method for defining the shape of a turbomachine convergent-divergent nozzle, and corresponding convergent-divergent nozzle J Szydlowski, G Bodard, M Leyko, J Langridge US Patent 9,249,755, 2016 | 4 | 2016 |
| Simulation and modelling of the waves transmission and generation in a stator blade row in a combustion-noise framework M Leyko, I Duran, S Moreau, F Nicoud, T Poinsot Journal of Sound and Vibration 333 (23), 6090-6106, 2014 | 43 | 2014 |
Thierry PoinsotCNRS
