4 Patents
- US124290122025Turbojet Engine Rear Portion Having an Augmented A9/A8 Nozzle Area Ratio
SAFRAN AIRCRAFT ENGINES
0 cites - US120186282024Turbojet Engine Rear Part Comprising a Nozzle Having Flaps Comprising Levers That Are Movable by Means of Upstream and Downstream Bearing Walls
SAFRAN AIRCRAFT ENGINES
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 - US117137302023Convergent-divergent Flap Pair for a Variable-geometry Turbojet Engine Nozzle Comprising Cooling Air Circulation Ducts Connected Through Contact Surfaces
SAFRAN AIRCRAFT ENGINES
0 cites