Safran Aircraft Engines

Michel Gilbert Rolland Brault

Arnaud Nicolas Negri

Nathalie Nowakowski

Romain Guillaume Cuvillier

Guillaume Patrice Kubiak

Nils Edouard Romain Bordoni

Aircraft turbine engine, including at least one first compressor, an annular combustion chamber and at least one first turbine, which define a first flow duct for a primary flow. Between the combustion chamber and the first turbine is a device for discharging at least part of the primary flow.

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Quincy Sous Senart, France

Michel Gilbert Rolland Brault