2 Patents
- US125957392026Gas Turbine Engine Blading Comprising a Blade and a Platform Which Has an Internal Flow-intake and Flow-ejection Canal
SAFRAN AIRCRAFT ENGINES
0 cites - US120185822024Turbine Blade for an Aircraft Turbine Engine, Comprising a Platform Provided with a Channel for Primary Flow Rejection Towards a Purge Cavity
SAFRAN AIRCRAFT ENGINES
0 cites