4 Patents
- US123663582025Flame-holder Device for a Turbojet Afterburner, Comprising Three-branched Arms
SAFRAN AIRCRAFT ENGINES
0 cites - US121636612024Diffusion Cone for the Rear Part of a Jet Engine Incorporating a Flame-holder Ring at the Trailing Edge
SAFRAN AIRCRAFT ENGINES
0 cites - 0 cites
- US117397122023Convergent-divergent Flap Pair for a Variable-geometry Turbojet Engine Nozzle, the Flaps of Which Each Comprise a Cooling Air Circulation Duct
SAFRAN AIRCRAFT ENGINES
0 cites