2 Patents
- US120608092024Vane for a Turbine Engine with Optimized Heel and Method for Optimizing a Vane Profile
SAFRAN AIRCRAFT ENGINES
0 cites - US118670652024Blade for a Rotating Bladed Disk for an Aircraft Turbine Engine Comprising a Sealing Lip Having an Optimized Non-constant Cross Section
SAFRAN AIRCRAFT ENGINES
0 cites